Tuesday, 21 January 2014

HYDROSTATIC LOCK

Hydrolock (a shorthand notation for hydrostatic lock) is an abnormal condition of any device which is designed to compress a gas by mechanically restraining it; most commonly the reciprocating internal combustion engine, the case this article refers to unless otherwise noted. Hydrolock occurs when a volume of liquid greater than the volume of the cylinder at its minimum (end of the piston's stroke) enters the cylinder. Since most common liquids are incompressible the piston cannot complete its travel; either the engine must stop rotating or a mechanical failure must occur.

 

Bend Connecting Rod due to Hydrolock

 

Symptoms and damage :-

If an engine hydrolocks while at speed, a mechanical failure is likely. Common damage modes include bent or broken connecting rods, a fractured head, a fractured block, crankcase damage, damaged bearings, or any combination of these. Forces absorbed by other interconnected components may cause additional damage. Physical damage to metal parts can manifest as a "crashing" or "screeching" sound and usually requires replacement of the engine or a substantial rebuild of its major components.
If an internal combustion engine hydrolocks while idling or under low power conditions, the engine may stop suddenly with no immediate damage. In this case the engine can often be purged by unscrewing the spark plugs or injectors and spinning the engine to expel the liquid from the combustion chambers and then restarted. Depending on how the liquid was introduced to the engine, it possibly can be restarted and dried out with normal combustion heat, or it may require more work, such as flushing out corrupted operating fluids and replacing damaged gaskets.
If a cylinder fills with liquid while the engine is turned off, the engine will refuse to turn when a starting cycle is attempted. Since the starter mechanism's torque is normally much lower than the engine's operating torque and momentum this will usually not damage the engine but may burn out the starter. The engine can be drained as above and restarted. If a corrosive substance such as water has been in the engine long enough to cause rusting, more extensive repairs will be required.
Amounts of water significant enough to cause hydrolock tend to upset the air/fuel mixture in gasoline engines. If water is introduced slowly enough, this effect can cut power and speed in an engine to a point that when hydrolock actually occurs it does not cause catastrophic engine damage.

 

Automotive

Hydrolock most commonly occurs in automobiles when driving through floods, either where the water is above the level of the air intake or the vehicle's speed is excessive, creating a tall bow wave. A vehicle fitted with a cold air intake mounted low on the vehicle will be especially vulnerable to hydrolocking when being driven through standing water or heavy precipitation. Engine coolant entering the cylinders through various means (such as a blown head gasket) is another common cause. Excessive fuel entering (flooding) one or more cylinders in liquid form due to or other abnormal operating conditions can also cause hydrolock.

 

Sunday, 19 January 2014

DRDO - NISHANT

 The DRDO Nishant is an Unmanned Aerial Vehicle (UAV) developed by India's ADE (Aeronautical Development Establishment) a branch of DRDO for the Indian Armed Forces. The Nishant UAV is primarily tasked with intelligence gathering over enemy territory and also for reconnaissance, training, surveillance, target designation, artillery fire correction, damage assessment, ELINT and SIGINT. The UAV has an endurance of 4 h 30 min. Nishant has completed development phase and user trials. 

DRDO - NISHANT

 

 

The 380 kg (840 lb) Nishant UAV requires rail-launching from a hydro-pneumatic launcher and recovered by a Parachute System. Launches at a velocity of 45 m/s are carried out in 0.6 second with 100 kW power and subsequent launches can be carried out in intervals of 20 minutes. The Mobile Hydro-Pneumatic Launcher (MHPL) system mounted on a Tatra truck weighs 14,000 kg (31,000 lb) and boasts of a life cycle of 1000 launches before requiring overhaul. Nishant is one of the few UAVs in the world in its weight-class capable of being catapult-launched and recovered by using parachute, thus eliminating the need for a runway as in case of conventional take-off and landing with wheels.

On 3rd Feb 2011 Nishant UAV has successfully completed confirmatory trials conducted by the Indian Army at Pokhran ,Rajasthan.

 

Features

  • Day/night capability training vehicle

  • Battlefield reconnaissance & surveillance,

  • Target tracking and localization

  • Artillery fire correction

  • All terrain mobility

  • Target designation (using integral laser target designator)

  • Endurance: 4 h 30 min

Ground support systems

  • Mobile hydropneumatic launcher (MHPL)

  • Ground control station (GCS)

  • Antenna vehicle/Ground Data Terminal(GDT)

  • Avionics preparation vehicle(APV)

  • Mechanical maintenance vehicle

  • UAV transportation vehicle

  • Power supply vehicle

General characteristics

  • Crew: None

  • Payload: 45 kg

  • Length: 4.63 m (15.2 ft)

  • Wingspan: 6.57 m (21.6 ft)

  • Empty weight: 380 kg (840 lb)

  • Powerplant: 1 × RE-2-21-P or RE-4-37-P

Performance:

  • Maximum speed: 185 km/h

  • Cruise speed: 125 km/h to 150 km/h

  • Range: 160 km (100 mi)

  • Service ceiling: 3,600 m (up to 11,800 ft)

Launch & recovery

  • Launch: Mobile hydropneumatic launcher (MHPL) system

  • Recovery: Parachute + landing bags

Saturday, 18 January 2014

DRDO DRONES- AURA(Autonomous Unmanned Research Aircraft)

AURA

The AURA will be a stealth UCAV, capable of releasing missiles, bombs and precision-guided munitions. The programme is in its project definition stage. The design is in line with what former DRDO chief controller for Aeronautics said in 2007, that India's combat drone would be a stealthy flying-wing concept aircraft with internal weapons and a turbofan engine.The UCAV's design is similar to Northrop Grumman's B-2 Spirit.The ADA describes the AURA as a "self-defending high-speed reconnaissance UAV with weapon firing capability". The first images released as part of a presentation shows the UAV as having a stealth design.The AURA will cruise at medium altitude and will be capable of carrying two or more guided strike weapons with on-board sensors for targeting and weapon guidance. The flight control system and data link packages of Aura (unmanned combat aerial vehicle) will be designed and developed jointly by ADA and Defense Electronic Application Laboratory. DRDO's Chief Controller, R&D (aeronautics), Dr Prahlada said, "Capable of flying at altitudes of 30,000 feet and weighing less than 15 tonnes, the UCAVs will have rail-launching for the missiles, bombs and PGMs (precision-guided munitions) they will carry.". The DRDO is going to use a Kaveri engine to power this unmanned vehicle. The AURA will be approximtely 15 tonnes aircraft with a range of 300+ km.

AURA

(Autonomous Unmanned Research Aircraft)
Role
Unmanned Stealth Bomber
Manufacturer
DRDO
Designer
DRDO
First flight
2015
Introduction
2019-2020
Status
Under Development
Primary user
Indian Air Force

Indian Navy

Friday, 17 January 2014

STIRLING ENGINE


A Stirling engine is a heat engine operating by cyclic compression and expansion of air or other gas, the working fluid, at different temperature levels such that there is a net conversion of heat energy to mechanical work.Or more specifically, a closed-cycle regenerative heat engine with a permanently gaseous working fluid, where closed-cycle is defined as a thermodynamic system in which the working fluid is permanently contained within the system, and regenerative describes the use of a specific type of internal heat exchanger and thermal store, known as the regenerator. It is the inclusion of a regenerator that differentiates the Stirling engine from other closed cycle hot air engines. Originally conceived in 1816 as an industrial prime mover to rival the steam engine, its practical use was largely confined to low-power domestic applications for over a century. The Stirling engine is noted for its high efficiency compared to steam engines,quiet operation, and the ease with which it can use almost any heat source. This compatibility with alternative and renewable energy sources has become increasingly significant as the price of conventional fuels rises, and also in light of concerns such as peak oil and climate change. This engine is currently exciting interest as the core component of micro combined heat and power (CHP) units, in which it is more efficient and safer than a comparable steam engine.

Tuesday, 14 January 2014

Monday, 9 December 2013

TEJAS PRODUCTION BY HAL

Hindustan Aeronautics Ltd aims to deliver 16 Tejas a year from its new production line>>

If the indigenous Tejas Light Combat Aircraft (LCA) has taken decades for completion, it is now in a record-breaking sprint to the finish line. The Tejas has flown an unprecedented 450 test flights this year towards a splashy ceremony in Bangalore scheduled for December 20, where Defence Minister A K Antony will preside over its induction into the Indian Air Force (IAF).
That landmark event will be the award of the Tejas’ Initial Operational Certificate (IOC), which will allow the country’s first indigenous modern fighter to be flown by regular pilots of the Indian Air Force (IAF). The first Tejas squadron (18-20 fighters) will be based at Sulur, near Coimbatore.
So far, only highly qualified test pilots of the National Flight Testing Centre (NFTC) in Bangalore have flown the Tejas. In the 2,400 test flights since it took to the air in 2001, the NFTC has incrementally flown the Tejas higher, faster and carried out increasingly difficult manoeuvres and weapon firings to test it meets the IAF’s requirements.
On Saturday, Group Captain Suneet Verma, a veteran NFTC test pilot, fired an air-to-air missile from the Tejas at an airborne target off the Goa coast, striking the target and taking the Tejas a step closer towards IOC.
While awarding the IOC, Antony will ceremonially hand over to the IAF boss, Air Chief Marshal N A K Browne, the fighter’s “Release to Service Document (RSD)”, which specifies the capabilities the Tejas has already demonstrated during flight testing.
This includes aerodynamic capabilities like speed, acceleration, climb rate and angle of attack; and also the basic weapons operations already tested on the Tejas, and the fighter’s proven radar and sensor capabilities. The Tejas flight-testing programme has been a prolonged and painstaking exercise, since this is India’s first modern fighter. The Aeronautical Development Agency (ADA) – a special purpose vehicle of the Defence R&D Organisation (DRDO), set up to manage the Tejas programme – worried that a crash during flight-testing might be a fatal blow to the project itself, and so has handled flight testing cautiously, taking twice the time that experienced countries do.
Once the IOC is awarded, Hindustan Aeronautics Ltd (HAL) will build the IAF’s first 20 Tejas fighters on a brand new production line in Bangalore. HAL has told Business Standard that it aims to roll out the first two fighters by March 2014, deliver eight fighters by end-2014, and then enhance the production line’s capability to 16 fighters a year.
So far, the IAF has committed to just 40 Tejas fighters. Of these, 20 will be built to IOC standards, and the next 20 ordered when Final Operation Clearance (FOC) is obtained. The defence minister has ordered the DRDO to ensure the FOC is not delayed beyond end-2014.
Avinash Chander, the DRDO chief, tells Business Standard the FOC will involve firing a range of different weapons, including missiles and bombs, and testing the fighter for mid-air refuelling.
“With the IAF now enthused about the Tejas, and participating actively in the project, we will surely obtain FOC next year. We could not have completed over 450 test flights this year without close cooperation between the IAF, ADA and HAL,” says Chander.
After obtaining FOC for the Tejas, ADA will start work on the Tejas Mark II. The key change is replacing the General Electric F-404 engine that powers the Mark I with the larger, more powerful GE F-414 engine. This will involve re-engineering the Mark I to fit in the bulkier F-414, a technological challenge for ADA.
ADA has also briefed Business Standard that the Tejas Mark II would have more fuel capacity for added range; a retractable mid-air refuelling system; a DRDO-built Airborne Electronically Scanned Array radar; world beating air-to-air missiles; an on-board oxygen-generating system, and a state-of-the-art Electronic Warfare suite to confuse enemy radars and sensors. “Eventually, the IAF is very likely to have at least 200 Tejas fighters in its fleet,” says Chander.

Sunday, 8 December 2013

America's Next Bomber



America’s next bomber could cost $810 million apiece>>

The U.S. Air Force’s new long-range bomber may cost as much as $81 billion for the 100 planes planned, 47 percent more than the $55 billion sticker price the service has listed.
The Air Force based its estimate of $550 million per plane on the value of the dollar in 2010, and it represents only the production costs for an aircraft that won’t be deployed for at least 10 years. Including research and development, the bomber would cost as much as $810 million apiece in this year’s dollars, according to calculations by three defense analysts.
The cost of the new bomber will draw close scrutiny in an era of declining defense budgets, as the Pentagon faces $500 billion in reductions over nine years under the budget process called sequestration. The Air Force’s track record also is being questioned after soaring costs for the aging B-2 stealth bomber the new plane would replace and the F-35 fighter jet, the most expensive U.S. weapons system, that’s now being built.
“The Air Force has zero credibility on start-of-program cost estimates unless and until it ponies up real details about the bomber and its acquisition plan,” Winslow Wheeler, a former Government Accountability Office defense analyst now with the Project on Government Oversight in Washington, said in an e-mail. “It is a fool’s errand, or worse, to pretend the cost stated now is anything but a bait-and-switch buy-in gambit.”
B-2, F-35
The B-2 was planned as 132 planes for about $571 million each in 1991 dollars before the first Bush administration cut the fleet to 20 planes in the early 1990s. That resulted in a price of about $2.2 billion per bomber, a fourfold increase, in a program that remained highly classified during its development.
The F-35 program has a current price tag of $391.2 billion for 2,443 aircraft, a 68 percent increase from the projection in 2001, as measured in current dollars, for 409 fewer planes than originally planned.
Whatever its ultimate cost, the new bomber would mean billions for the defense contractor chosen to build it. Lockheed Martin Corp. (LMT:US) of Bethesda, Maryland, and Chicago-based Boeing Co. (BA:US), the No. 1 and No. 2 U.S. defense contractors, said in October that they’ll bid for the project as a team. They may end up competing against Northrop Grumman Corp. (NOC:US) of Falls Church, Virginia, the prime contractor for the B-2, which hasn’t yet announced an intention to bid.
The Air Force has requested $379 million in funding for development this year, increasing to more than $1 billion in fiscal 2015 and $2.8 billion in fiscal 2018, according to data released by the service.
Through 2023
The Air Force hasn’t provided its rationale for the increased spending. The Congressional Budget Office said the Air Force plans to request $32.1 billion through 2023.
The $550 million per plane projection for the new bomber is “the only cost estimate approved for public release at this time,” Air Force spokesman Ed Gulick said in a statement.
Gulick said the estimate is a “target that helps balance capabilities and cost” and is being used in “rigidly containing the design” of the bomber.
The more complete “program acquisition unit cost” will be derived later by adding research and development, as well as estimating “inflation up to the year you purchase aircraft,” Gulick said.
The Air Force’s cost estimate “seems rather ambitious,” said Todd Harrison, a defense budget analyst with the Center for Strategic and Budgetary Assessments, a Washington-based policy group. He calculated a price of $810 million a plane in fiscal 2014 dollars, or $81 billion for 100, based on $20 billion in projected research and development costs.
Historical Increases
“Aircraft programs, and stealth aircraft in particular, have gone far over their initial cost estimates,” Harrison said. “If you factor in historical cost growth, the total program cost could easily top $100 billion.”
Russell Rumbaugh, a defense analyst with the Stimson Center, also a policy group in Washington, said his comparable estimate is $682 million per plane. Kevin Brancato, a defense analyst with Bloomberg Government, projected $784 million per plane in this year’s dollars.
“The incentives in the budget system almost force the services to low-ball their cost estimates,” said Gordon Adams, a professor at American University in Washington who oversaw the national security budget for the White House under President Bill Clinton. “Otherwise they do not get the program in the budget. It grows later.”
The Air Force now operates a fleet of 159 long-range bombers, including 63 swing-wing B-1Bs developed in the 1980s by Rockwell International, which is now part of Boeing, and the 20 B-2s from the 1990s.
Aging B-2s
The new bomber is needed because the “B-2 is an older airplane that’s getting expensive” to maintain and “it’s not as stealthy as we’re now capable of making aircraft,” Deputy Defense Secretary Ashton Carter said in an interview before he left office Dec. 4.
As the Air Force anticipates its needs 10 or 20 years from now, “expecting those aircraft to perform reliably at such advanced ages may prove to be overly optimistic,” said Mark Gunzinger, an airpower analyst with the Center for Strategic and Budgetary Assessments.
The Air Force is still flying 76 B-52 bombers from the H series that entered service in May 1961. They remain capable of launching conventional and nuclear bombs and cruise missiles.
Top Projects
The Air Force has identified the new long-range bomber as one of its top three weapons projects, along with the F-35 from Lockheed and the KC-46 aerial refueling tanker made by Boeing.
Defense Secretary Chuck Hagel has said the bomber will support the U.S. strategy of rebalancing toward Asia. Pentagon officials have said they’ll do as much as they can to shelter such priority weapons systems from the automatic budget cuts.
An Air Force summary of the bomber describes a stealth aircraft able to deliver both nuclear and conventional weapons. While the “baseline aircraft” would be piloted, the bomber would be designed to “enable future unmanned capability,” according to the service.
Beyond that, the Air Force, which has said the bomber would incorporate “proven technologies,” has said little about its classified plans for the new plane.
“It would be a mistake to view this aircraft as simply another bomber,” said Retired Lieutenant General David Deptula, the Air Force’s former chief of intelligence, surveillance and reconnaissance.
‘Cloaked in Secrecy’
It may take off on a bombing run, using intelligence and surveillance sensors provided from other platforms and on-board jammers to degrade ground radar, he said in an e-mail. The bomber crew also could use its radar and sensors to direct land-and sea-based strikes, as well as collect intelligence on the return flight, according to Deptula, who helped plan the air campaign in the 1991 Gulf War.
“The operational characteristics are going to be cloaked in secrecy for a while, and I think that makes perfect sense,” Air Force Chief of Staff General Mark Welsh told reporters in November.
Welsh said capabilities would be carefully weighed against the $550 million-a-plane target.
“What we don’t want to do is try to reach into some level of technology that’s impractical.” That’s when “prices start to get out of control and your requirements start to drift,” Welsh said. “We are not going to go there.”
Adams cited the B-2’s cost escalation, as well as plans for a medium-range bomber that Defense Secretary Robert Gates canceled as too costly in 2009. Gates supports the new bomber.
“How many times are we going to go down this overpriced bomber road?” said Adams said. “It’s like Lucy with the football. We never get to kick an affordable aircraft through the goalpost.”

Saturday, 7 December 2013

Arduino 4d9a3348ad10c407354911e17196ac65c564a40

Arduino Uno - R3.jpg


Arduino is a single-board microcontroller to make using electronics in multidisciplinary projects more accessible. The hardware consists of an open-source hardware board designed around an 8-bit Atmel AVR microcontroller, or a 32-bit Atmel ARM. The software consists of a standard programming language compiler and a boot loader that executes on the microcontroller.
Arduino boards can be purchased pre-assembled or as do-it-yourself kits. Hardware design information is available for those who would like to assemble an Arduino by hand. It was estimated in mid-2011 that over 300,000 official Arduinos had been commercially produced.

An arduino board consists of an Atmel 8-bit AVR microcontroller with complementary components to facilitate programming and incorporation into other circuits. An important aspect of the Arduino is the standard way that connectors are exposed, allowing the CPU board to be connected to a variety of interchangeable add-on modules known as shields. Some shields communicate with the Arduino board directly over various pins, but many shields are individually addressable via an I²C serial bus, allowing many shields to be stacked and used in parallel. Official Arduinos have used the megaAVR series of chips, specifically the ATmega8, ATmega168, ATmega328, ATmega1280, and ATmega2560. A handful of other processors have been used by Arduino compatibles. Most boards include a 5 voltlinear regulator and a 16 MHz crystal oscillator (or ceramic resonator in some variants), although some designs such as the LilyPad run at 8 MHz and dispense with the onboard voltage regulator due to specific form-factor restrictions. An Arduino's microcontroller is also pre-programmed with a boot loader that simplifies uploading of programs to the on-chip flash memory, compared with other devices that typically need an external programmer.
At a conceptual level, when using the Arduino software stack, all boards are programmed over an RS-232 serial connection, but the way this is implemented varies by hardware version. Serial Arduino boards contain a level shifter circuit to convert between RS-232-level andTTL-level signals. Current Arduino boards are programmed via USB, implemented using USB-to-serial adapter chips such as the FTDIFT232. Some variants, such as the Arduino Mini and the unofficial Boarduino, use a detachable USB-to-serial adapter board or cable,Bluetooth or other methods. (When used with traditional microcontroller tools instead of the Arduino IDE, standard AVR ISPprogramming is used.)
The Arduino board exposes most of the microcontroller's I/O pins for use by other circuits. The Diecimila, Duemilanove, and current Uno provide 14 digital I/O pins, six of which can produce pulse-width modulated signals, and six analog inputs. These pins are on the top of the board, via female 0.10-inch (2.5 mm) headers. Several plug-in application shields are also commercially available.
The Arduino Nano, and Arduino-compatible Bare Bones Board and Boarduino boards may provide male header pins on the underside of the board to be plugged into solderless breadboards.
There are many Arduino-compatible and Arduino-derived boards. Some are functionally equivalent to an Arduino and may be used interchangeably. Many are the basic Arduino with the addition of commonplace output drivers, often for use in school-level education to simplify the construction of buggies and small robots. Others are electrically equivalent but change the form factor, sometimes permitting the continued use of Shields, sometimes not. Some variants use completely different processors, with varying levels of compatibility.
Official boards
Further information: List of Arduino boards and compatible systems
The original Arduino hardware is manufactured by the Italian company Smart Projects.Some Arduino-branded boards have been designed by the American company SparkFun Electronics.Sixteen versions of the Arduino hardware have been commercially produced to date.

Shields

Arduino and Arduino-compatible boards make use of shields—printed circuit expansion boards that plug into the normally supplied Arduino pin-headers. Shields can provide motor controls, GPS, ethernet, LCD display, or breadboarding (prototyping). A number of shields can also be made.
Example Arduino shields

Software

Arduino Software IDE
Arduino 1.0 IDE, Ubuntu 11.10.png
A screenshot of the Arduino IDE showing the "Blink" program, a simple beginner program
Developer(s)Arduino Software
Stable release1.0.5 / May 15, 2013[9]
Preview release1.5.4 Beta / September 10, 2013
Written inJavaC and C++
Operating systemCross-platform
TypeIntegrated development environment
LicenseLGPL or GPL license
Websitearduino.cc
The Arduino integrated development environment (IDE) is a cross-platform application written in Java, and is derived from the IDE for theProcessing programming language and the Wiring projects. It is designed to introduce programming to artists and other newcomers unfamiliar with software development. It includes a code editor with features such as syntax highlightingbrace matching, and automatic indentation, and is also capable of compiling and uploading programs to the board with a single click. A program or code written for Arduino is called a "sketch".[10]
Arduino programs are written in C or C++. The Arduino IDE comes with a software library called "Wiring" from the original Wiring project, which makes many common input/output operations much easier. Users only need define two functions to make a runnablecyclic executive program:
  • setup(): a function run once at the start of a program that can initialize settings
  • loop(): a function called repeatedly until the board powers off
A typical first program for a microcontroller simply blinks an LED on and off. In the Arduino environment, the user might write a program like this:[11]

The integrated pin 13 LED
#define LED_PIN 13
 
void setup () {
  pinMode (LED_PIN, OUTPUT); // Enable pin 13 for digital output
}
 
void loop () {
  digitalWrite (LED_PIN, HIGH); // Turn on the LED
  delay (1000); // Wait one second (1000 milliseconds)
  digitalWrite (LED_PIN, LOW); // Turn off the LED
  delay (1000); // Wait one second
}
It is a feature of most Arduino boards that they have an LED and load resistor connected between pin 13 and ground; a convenient feature for many simple tests. The previous code would not be seen by a standard C++ compiler as a valid program, so when the user clicks the "Upload to I/O board" button in the IDE, a copy of the code is written to a temporary file with an extra include header at the top and a very simple main() function at the bottom, to make it a valid C++ program.
The Arduino IDE uses the GNU toolchain and AVR Libc to compile programs, and uses avrdude to upload programs to the board.
As the Arduino platform uses Atmel microcontrollers, Atmel's development environment, AVR Studio or the newer Atmel Studio, may also be used to develop software for the Arduino.

Development

The core Arduino developer team is composed of Massimo Banzi, David Cuartielles, Tom Igoe, Gianluca Martino, David Mellis and Nicholas Zambetti. Massimo Banzi was interviewed on the March 21st, 2009 episode (Episode 61) of FLOSS Weekly on the TWiT.tvnetwork, in which he discussed the history and goals of the Arduino project. He also gave a talk at TEDGlobal 2012 Conference, where he outlined various uses of Arduino boards around the world.Arduino is open source hardware: the Arduino hardware reference designs are distributed under a Creative Commons Attribution Share-Alike 2.5 license and are available on the Arduino Web site. Layout and production files for some versions of the Arduino hardware are also available. The source code for the IDE is available and released under the GNU General Public License, version 2.Although the hardware and software designs are freely available under copyleft licenses, the developers have requested that the name "Arduino" be exclusive to the official productand not be used for derivative works without permission. The official policy document on the use of the Arduino name emphasizes that the project is open to incorporating work by others into the official product.[Several Arduino-compatible products commercially released have avoided the "Arduino" name by using "-duino" name variants

Applications

Xoscillo: open-source oscilloscope
Scientific equipment
Arduinome: a MIDI controller device that mimics the Monome
OBDuino: a trip computer that uses the on-board diagnostics interface found in most modern cars
The Humane Reader and Humane PC from Humane Informatics: low-cost electronic devices with TV-out that can hold a five thousand book library (e.g. offline Wikipedia compilations) on a microSD card
Ardupilot: drone software / hardware
ArduinoPhone

Microelectromechanical systems

Microelectromechanical systems (MEMS) (also written as micro-electro-mechanical, MicroElectroMechanical or microelectronic and microelectromechanical systems) is the technology of very small devices; it merges at the nano-scale into nanoelectromechanical systems (NEMS) and nanotechnology. MEMS are also referred to as micromachines (in Japan), or micro systems technology – MST (in Europe).
MEMS are separate and distinct from the hypothetical vision of molecular nanotechnology or molecular electronics. MEMS are made up of components between 1 to 100 micrometres in size (i.e. 0.001 to 0.1 mm), and MEMS devices generally range in size from 20 micrometres (20 millionths of a metre) to a millimetre (i.e. 0.02 to 1.0 mm). They usually consist of a central unit that processes data (the microprocessor) and several components that interact with the surroundings such as microsensors.At these size scales, the standard constructs of classical physics are not always useful. Because of the large surface area to volume ratio of MEMS, surface effects such as electrostatics and wetting dominate over volume effects such as inertia or thermal mass.
The potential of very small machines was appreciated before the technology existed that could make them—see, for example, Richard Feynman's famous 1959 lecture There's Plenty of Room at the Bottom. MEMS became practical once they could be fabricated using modified semiconductor device fabrication technologies, normally used to make electronics. These include molding and plating, wet etching (KOH, TMAH) and dry etching (RIE and DRIE), electro discharge machining (EDM), and other technologies capable of manufacturing small devices. An early example of a MEMS device is the resonistor – an electromechanical monolithic resonator.

Materials for MEMS manufacturing

The fabrication of MEMS evolved from the process technology in semiconductor device fabrication, i.e. the basic techniques are deposition of material layers, patterning by photolithography and etching to produce the required shapes.
Silicon
Silicon is the material used to create most integrated circuits used in consumer electronics in the modern industry. The economies of scale, ready availability of cheap high-quality materials and ability to incorporate electronic functionality make silicon attractive for a wide variety of MEMS applications. Silicon also has significant advantages engendered through its material properties. In single crystal form, silicon is an almost perfect Hookean material, meaning that when it is flexed there is virtually no hysteresis and hence almost no energy dissipation. As well as making for highly repeatable motion, this also makes silicon very reliable as it suffers very little fatigue and can have service lifetimes in the range of billions to trillions of cycles without breaking.
Polymers
Even though the electronics industry provides an economy of scale for the silicon industry, crystalline silicon is still a complex and relatively expensive material to be produced. Polymers on the other hand can be produced in huge volumes, with a great variety of material characteristics. MEMS devices can be made from polymers by processes such as injection molding, embossing or stereolithography and are especially well suited to microfluidic applications such as disposable blood testing cartridges.
Metals
Metals can also be used to create MEMS elements. While metals do not have some of the advantages displayed by silicon in terms of mechanical properties, when used within their limitations, metals can exhibit very high degrees of reliability. Metals can be deposited by electroplating, evaporation, and sputtering processes. Commonly used metals include gold, nickel, aluminium, copper, chromium, titanium, tungsten, platinum, and silver.
Ceramics
The nitrides of silicon, aluminium and titanium as well as silicon carbide and other ceramics are increasingly applied in MEMS fabrication due to advantageous combinations of material properties. AlN crystallizes in the wurtzite structure and thus shows pyroelectric and piezoelectric properties enabling sensors, for instance, with sensitivity to normal and shear forces. TiN, on the other hand, exhibits a high electrical conductivity and large elastic modulus allowing to realize electrostatic MEMS actuation schemes with ultrathin membranes.Moreover, the high resistance of TiN against biocorrosion qualifies the material for applications in biogenic environments and in biosensors.
MEMS basic processes
Deposition processes
One of the basic building blocks in MEMS processing is the ability to deposit thin films of material with a thickness anywhere between a few nanometres to about 100 micrometres. There are two types of deposition processes, as follows.
Physical deposition
Physical vapor deposition ("PVD") consists of a process in which a material is removed from a target, and deposited on a surface. Techniques to do this include the process of sputtering, in which an ion beam liberates atoms from a target, allowing them to move through the intervening space and deposit on the desired substrate, and Evaporation (deposition), in which a material is evaporated from a target using either heat (thermal evaporation) or an electron beam (e-beam evaporation) in a vacuum system.
Chemical deposition
Chemical deposition techniques include chemical vapor deposition ("CVD"), in which a stream of source gas reacts on the substrate to grow the material desired. This can be further divided into categories depending on the details of the technique, for example, LPCVD (Low Pressure chemical vapor deposition) and PECVD (Plasma Enhanced chemical vapor deposition).
Oxide films can also be grown by the technique of thermal oxidation, in which the (typically silicon) wafer is exposed to oxygen and/or steam, to grow a thin surface layer of silicon dioxide.
Patterning
Patterning in MEMS is the transfer of a pattern into a material.
Lithography
Lithography in MEMS context is typically the transfer of a pattern into a photosensitive material by selective exposure to a radiation source such as light. A photosensitive material is a material that experiences a change in its physical properties when exposed to a radiation source. If a photosensitive material is selectively exposed to radiation (e.g. by masking some of the radiation) the pattern of the radiation on the material is transferred to the material exposed, as the properties of the exposed and unexposed regions differs.
This exposed region can then be removed or treated providing a mask for the underlying substrate. Photolithography is typically used with metal or other thin film deposition, wet and dry etching.
Photolithography
Photolithography is the process of transferring geometric shapes on a mask to the surface of a silicon wafer. The steps involved in the photolithographic process are wafer cleaning; barrier layer formation; photoresist application; soft baking; mask alignment; exposure and development; and hard-baking.
Wafer Cleaning, Barrier Formation and Photoresist Application
In the first step, the wafers are chemically cleaned to remove particulate matter on the surface as well as any traces of organic, ionic, and metallic impurities. After cleaning, silicon dioxide, which serves as a barrier layer, is deposited on the surface of the wafer. After the formation of the SiO2 layer, photoresist is applied to the surface of the wafer. High-speed centrifugal whirling of silicon wafers is the standard method for applying photoresist coatings in IC manufacturing. This technique, known as "Spin Coating," produces a thin uniform layer of photoresist on the wafer surface.
Positive and Negative Photoresist:-
There are two types of photoresist: positive and negative. For positive resists, the resist is exposed with UV light wherever the underlying material is to be removed. In these resists, exposure to the UV light changes the chemical structure of the resist so that it becomes more soluble in the developer. The exposed resist is then washed away by the developer solution, leaving windows of the bare underlying material. In other words, "whatever shows, goes." The mask, therefore, contains an exact copy of the pattern which is to remain on the wafer.
Negative resists behave in just the opposite manner. Exposure to the UV light causes the negative resist to become polymerized, and more difficult to dissolve. Therefore, the negative resist remains on the surface wherever it is exposed, and the developer solution removes only the unexposed portions. Masks used for negative photoresists, therefore, contain the inverse (or photographic "negative") of the pattern to be transferred. The figure below shows the pattern differences generated from the use of positive and negative resist.
Electron beam lithography
Electron beam lithography (often abbreviated as e-beam lithography) is the practice of scanning a beam of electrons in a patterned fashion across a surface covered with a film (called the resist),[7] ("exposing" the resist) and of selectively removing either exposed or non-exposed regions of the resist ("developing"). The purpose, as with photolithography, is to create very small structures in the resist that can subsequently be transferred to the substrate material, often by etching. It was developed for manufacturing integrated circuits, and is also used for creating nanotechnology architectures.
The primary advantage of electron beam lithography is that it is one of the ways to beat the diffraction limit of light and make features in the nanometer regime. This form of maskless lithography has found wide usage in photomask-making used in photolithography, low-volume production of semiconductor components, and research & development.
The key limitation of electron beam lithography is throughput, i.e., the very long time it takes to expose an entire silicon wafer or glass substrate. A long exposure time leaves the user vulnerable to beam drift or instability which may occur during the exposure. Also, the turn-around time for reworking or re-design is lengthened unnecessarily if the pattern is not being changed the second time.
Ion beam lithography
It is known that focused-ion-beam lithography has the capability of writing extremely fine lines (less than 50 nm line and space has been achieved) without proximity effect. However, because the writing field in ion-beam lithography is quite small, large area patterns must be created by stitching together the small fields.
Ion track technology
Ion track technology is a deep cutting tool with a resolution limit around 8 nm applicable to radiation resistant minerals, glasses and polymers. It is capable to generate holes in thin films without any development process. Structural depth can be defined either by ion range or by material thickness. Aspect ratios up to several 104 can be reached. The technique can shape and texture materials at a defined inclination angle. Random pattern, single-ion track structures and aimed pattern consisting of individual single tracks can be generated.
X-ray lithography
X-ray lithography, is a process used in electronic industry to selectively remove parts of a thin film. It uses X-rays to transfer a geometric pattern from a mask to a light-sensitive chemical photoresist, or simply "resist," on the substrate. A series of chemical treatments then engraves the produced pattern into the material underneath the photoresist.
Diamond patterning
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Etching processes
There are two basic categories of etching processes: wet etching and dry etching. In the former, the material is dissolved when immersed in a chemical solution. In the latter, the material is sputtered or dissolved using reactive ions or a vapor phase etchant for a somewhat dated overview of MEMS etching technologies.
 Etching (microfabrication)
Wet chemical etching consists in selective removal of material by dipping a substrate into a solution that dissolves it. The chemical nature of this etching process provides a good selectivity, which means the etching rate of the target material is considerably higher than the mask material if selected carefully.
Isotropic etching
Etching progresses at the same speed in all directions. Long and narrow holes in a mask will produce v-shaped grooves in the silicon. The surface of these grooves can be atomically smooth if the etch is carried out correctly, with dimensions and angles being extremely accurate.
Anisotropic etching
Some single crystal materials, such as silicon, will have different etching rates depending on the crystallographic orientation of the substrate. This is known as anisotropic etching and one of the most common examples is the etching of silicon in KOH (potassium hydroxide), where Si <111> planes etch approximately 100 times slower than other planes (crystallographic orientations). Therefore, etching a rectangular hole in a (100)-Si wafer results in a pyramid shaped etch pit with 54.7° walls, instead of a hole with curved sidewalls as with isotropic etching.
HF etching
Hydrofluoric acid is commonly used as an aqueous etchant for silicon dioxide (SiO
2, also known as BOX for SOI), usually in 49% concentrated form, 5:1, 10:1 or 20:1 BOE (buffered oxide etchant) or BHF (Buffered HF). They were first used in medieval times for glass etching. It was used in IC fabrication for patterning the gate oxide until the process step was replaced by RIE.
Hydrofluoric acid is considered one of the more dangerous acids in the cleanroom. It penetrates the skin upon contact and it diffuses straight to the bone. Therefore the damage is not felt until it is too late.
Electrochemical etching
Electrochemical etching (ECE) for dopant-selective removal of silicon is a common method to automate and to selectively control etching. An active p-n diode junction is required, and either type of dopant can be the etch-resistant ("etch-stop") material. Boron is the most common etch-stop dopant. In combination with wet anisotropic etching as described above, ECE has been used successfully for controlling silicon diaphragm thickness in commercial piezoresistive silicon pressure sensors. Selectively doped regions can be created either by implantation, diffusion, or epitaxial deposition of silicon.

Xenon difluoride etching
Xenon difluoride is a dry vapor phase isotropic etch for silicon originally applied for MEMS in 1995 at University of California, Los Angeles.Primarily used for releasing metal and dielectric structures by undercutting silicon, XeF
2 has the advantage of a stiction-free release unlike wet etchants. Its etch selectivity to silicon is very high, allowing it to work with photoresist, SiO
2, silicon nitride, and various metals for masking. Its reaction to silicon is "plasmaless", is purely chemical and spontaneous and is often operated in pulsed mode. Models of the etching action are available, and university laboratories and various commercial tools offer solutions using this approach.

Reactive ion etching
In reactive ion etching (RIE), the substrate is placed inside a reactor, and several gases are introduced. A plasma is struck in the gas mixture using an RF power source, which breaks the gas molecules into ions. The ions accelerate towards, and react with, the surface of the material being etched, forming another gaseous material. This is known as the chemical part of reactive ion etching. There is also a physical part, which is similar to the sputtering deposition process. If the ions have high enough energy, they can knock atoms out of the material to be etched without a chemical reaction. It is a very complex task to develop dry etch processes that balance chemical and physical etching, since there are many parameters to adjust. By changing the balance it is possible to influence the anisotropy of the etching, since the chemical part is isotropic and the physical part highly anisotropic the combination can form sidewalls that have shapes from rounded to vertical. RIE can be deep (Deep RIE or deep reactive ion etching (DRIE)).
Deep reactive ion etching
Deep RIE (DRIE) is a special subclass of RIE that is growing in popularity. In this process, etch depths of hundreds of micrometres are achieved with almost vertical sidewalls. The primary technology is based on the so-called "Bosch process",[13] named after the German company Robert Bosch, which filed the original patent, where two different gas compositions alternate in the reactor. Currently there are two variations of the DRIE. The first variation consists of three distinct steps (the Bosch Process as used in the Plasma-Therm tool) while the second variation only consists of two steps (ASE used in the STS tool).
In the 1st Variation, the etch cycle is as follows:
(i) SF
6 isotropic etch;
(ii) C
4F
8 passivation;
(iii) SF
6 anisoptropic etch for floor cleaning.
In the 2nd variation, steps (i) and (iii) are combined.
Both variations operate similarly. The C
4F
8 creates a polymer on the surface of the substrate, and the second gas composition (SF
6 and O
2) etches the substrate. The polymer is immediately sputtered away by the physical part of the etching, but only on the horizontal surfaces and not the sidewalls. Since the polymer only dissolves very slowly in the chemical part of the etching, it builds up on the sidewalls and protects them from etching. As a result, etching aspect ratios of 50 to 1 can be achieved. The process can easily be used to etch completely through a silicon substrate, and etch rates are 3–6 times higher than wet etching.
Die preparation
After preparing a large number of MEMS devices on a silicon wafer, individual dies have to be separated, which is called die preparation in semiconductor technology. For some applications, the separation is preceded by wafer backgrinding in order to reduce the wafer thickness. Wafer dicing may then be performed either by sawing using a cooling liquid or a dry laser process called stealth dicing.
MEMS manufacturing technologies
Bulk micromachining
Bulk micromachining is the oldest paradigm of silicon based MEMS. The whole thickness of a silicon wafer is used for building the micro-mechanical structures.[9] Silicon is machined using various etching processes. Anodic bonding of glass plates or additional silicon wafers is used for adding features in the third dimension and for hermetic encapsulation. Bulk micromachining has been essential in enabling high performance pressure sensors and accelerometers that changed the sensor industry in the 1980's and 90's.

Surface micromachining
Surface micromachining uses layers deposited on the surface of a substrate as the structural materials, rather than using the substrate itself.Surface micromachining was created in the late 1980s to render micromachining of silicon more compatible with planar integrated circuit technology, with the goal of combining MEMS and integrated circuits on the same silicon wafer. The original surface micromachining concept was based on thin polycrystalline silicon layers patterned as movable mechanical structures and released by sacrificial etching of the underlying oxide layer. Interdigital comb electrodes were used to produce in-plane forces and to detect in-plane movement capacitively. This MEMS paradigm has enabled the manufacturing of low cost accelerometers for e.g. automotive air-bag systems and other applications where low performance and/or high g-ranges are sufficient. Analog Devices have pioneered the industrialization of surface micromachining and have realized the co-integration of MEMS and integrated circuits.
High aspect ratio (HAR) silicon micromachining
Both bulk and surface silicon micromachining are used in the industrial production of sensors, ink-jet nozzles, and other devices. But in many cases the distinction between these two has diminished. A new etching technology, deep reactive-ion etching, has made it possible to combine good performance typical of bulk micromachining with comb structures and in-plane operation typical of surface micromachining. While it is common in surface micromachining to have structural layer thickness in the range of 2 µm, in HAR silicon micromachining the thickness can be from 10 to 100 µm. The materials commonly used in HAR silicon micromachining are thick polycrystalline silicon, known as epi-poly, and bonded silicon-on-insulator (SOI) wafers although processes for bulk silicon wafer also have been created (SCREAM). Bonding a second wafer by glass frit bonding, anodic bonding or alloy bonding is used to protect the MEMS structures. Integrated circuits are typically not combined with HAR silicon micromachining.
Applications
microelectromechanical systems chip, sometimes called "lab on a chip"
MEMS compared to a 0.02 € coin
In one viewpoint MEMS application is categorized by type of use.
Sensor
Actuator
Structure
In another view point MEMS applications are categorized by the field of application (commercial applications include):
Inkjet printers, which use piezoelectrics or thermal bubble ejection to deposit ink on paper.
Accelerometers in modern cars for a large number of purposes including airbag deployment in collisions.
Accelerometers in consumer electronics devices such as game controllers (Nintendo Wii), personal media players / cell phones (Apple iPhone, various Nokia mobile phone models, various HTC PDA models)[15] and a number of Digital Cameras (various Canon Digital IXUS models). Also used in PCs to park the hard disk head when free-fall is detected, to prevent damage and data loss.
MEMS gyroscopes used in modern cars and other applications to detect yaw; e.g., to deploy a roll over bar or trigger dynamic stability control
MEMS microphones in portable devices, e.g., mobile phones, head sets and laptops.
Silicon pressure sensors e.g., car tire pressure sensors, and disposable blood pressure sensors
Displays e.g., the DMD chip in a projector based on DLP technology, which has a surface with several hundred thousand micromirrors or single micro-scanning-mirrors also called microscanners
Optical switching technology, which is used for switching technology and alignment for data communications
Bio-MEMS applications in medical and health related technologies from Lab-On-Chip to MicroTotalAnalysis (biosensor, chemosensor), or embedded in medical devices e.g. stents.
Interferometric modulator display (IMOD) applications in consumer electronics (primarily displays for mobile devices), used to create interferometric modulation − reflective display technology as found in mirasol displays
Fluid acceleration such as for micro-cooling
Micro-scale Energy harvesting including piezoelectric,electrostatic and electromagentic micro harvesters.
Micromachined Ultrasound Transducer including Piezoelectric Micromachined Ultrasonic Transducers and Capacitive Micromachined Ultrasonic Transducers.
Companies with strong MEMS programs come in many sizes. The larger firms specialize in manufacturing high volume inexpensive components or packaged solutions for end markets such as automobiles, biomedical, and electronics. The successful small firms provide value in innovative solutions and absorb the expense of custom fabrication with high sales margins. In addition, both large and small companies work in R&D to explore MEMS technology.
Industry structure

The global market for micro-electromechanical systems, which includes products such as automobile airbag systems, display systems and inkjet cartridges totaled $40 billion in 2006 according to Global MEMS/Microsystems Markets and Opportunities, a research report from SEMI and Yole Developpement and is forecasted to reach $72 billion by 2011.
MEMS devices are defined as die-level components of first-level packaging, and include pressure sensors, accelerometers, gyroscopes, microphones, digital mirror displays, microfluidic devices, etc. The materials and equipment used to manufacture MEMS devices topped $1 billion worldwide in 2006. Materials demand is driven by substrates, making up over 70 percent of the market, packaging coatings and increasing use of chemical mechanical planarization (CMP). While MEMS manufacturing continues to be dominated by used semiconductor equipment, there is a migration to 200 mm lines and select new tools, including etch and bonding for certain MEMS applications.