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Supplier: Accuris
Description: STARTER, AIRCRAFT ENGINE, AIR TURBINE
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Supplier: SAE International
Description: The starters covered by this specification shall be designed to operate on compressed air from ground support equipment, engine interbleed or on board air supply.
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Supplier: Accuris
Description: STARTER: AIRCRAFT ENGINE, AIR TURBINE
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Supplier: Accuris
Description: Starter, Aircraft Engine, Air Turbine
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Supplier: Accuris
Description: STARTERS, AIRCRAFT ENGINE, HYDRAULIC, GENERAL SPECIFICATION FOR
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Supplier: Safran Helicopter Engines
Description: Originally created for the Dassault Aviation Rafale aircraft, the Air Turbine Starter ATS-305 is designed to start the SNECMA M88 engines, from the intake air flow supplied by the Auxiliary Power Unit of the aircraft (Microturbo APU Rubis 3). The ATS 305 starter
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Supplier: Safran Helicopter Engines
Description: Associated with the Saphir 10 APU, the ATS 323 air turbine starter, in a very short time, start the Turbomeca / Rolls-Royce Adour Mk871 jet engine installed on the BAE SYSTEMS Hawk advanced training aircraft. The result of Microturbo's know-how in starting systems, the ATS 323
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Supplier: Safran Helicopter Engines
Description: million starts. Light and compact, the ATS 346 air turbine starter accepts high air inlet temperatures. Associated with the Opale 3 APU, it provides the aircraft with complete self-sustained starting. It contributes to safety in operation by providing additional starting capacity in
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Supplier: Safran Helicopter Engines
Description: The ATS M air turbine starters are designed to start the two EJ200 jet engines (cooperation between MTU, Rolls-Royce, Avio and ITP) that power the Typhoon Eurofighter. The Typhoon Eurofighter program consists of over 600 aircraft for the Air Forces of the four founding nations
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Supplier: SAE International
Description: This specification covers the general requirements for pneumatic control valves for use with the starters on aircraft gas turbine engines. This specification shall be used in conjunction with AS943, ARP949, and AIR1639.
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Supplier: Safran Electrical & Power
Description: electrical power after engine starting. Labinal Power Systems also provides a range of DC generators without the start function. The starter generators / generators are air cooled and Labinal Power Systems can provide a number of air inlet and outlet duct options to match with the
- Applications: Other
- Volt-Ampere: 5000 to 250000 VA
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Supplier: Electric Generators Direct
Description: •Effortless starting and easy operation 12 Volt DC Output (Battery Charging Cables Included) •Recharge 12 volt batteries for RV, auto, marine, aircraft, etc •12vdc output is 12amps Oil Watch Warning System •Automatically shuts off before oil level is low to protect engine Long Run Time
- Frequency: 60 Hz
- Fuel Type: Gasoline
- Phase: AC Single Phase Power
- Voltage: 120 V
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Supplier: UL Standards & Engagement
Description: vehicles, including caravans; - battery chargers installed on marine craft; - automotive battery chargers intended to charge lead-acid engine-starter and other starting, lighting, and ignition (SLI) type batteries; - battery chargers for e-mobility devices and e-bikes, provided
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control across a variety of applications: Aircraft Component Manufacturing: Precise positioning for fuselage assembly, wing installations, and landing gear production. Aerospace Maintenance & Repair: Controlled lifting and positioning of engines, landing gear, and interior (read more)
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Indicates content that may require registration and/or purchase.
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Two-channel switched reluctance starter/generator results
Abstract— Measured data and simulation results for a two- channel experimental switched-reluctance-motor (SRM)-based aircraft engine starter /generator system are presented.
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A very high speed switched-reluctance starter-generator for aircraft engine applications
MacMinn S.R. and Sember J.W., "Control of a Switched-Reluctance Aircraft Engine Starter - Generator over a Very Wide Speed Range," To be presented at the 24th Intersociety Energy Conversion Engineering Conference (IECEC), August 6-11 1989, Washington, D.C.
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Power Electronics Building Blocks (PEBB) in Aerospace Power Electronic Systems
MacMinn S.R. , Sember J.W. , “Control of a switched-Reluctance Aircraft Engine Starter -Generator Over a Very Wide Speed Range” , IEEE IECEC record , 1989 , pp. 631 -638 .
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The Quest for Oil-Free Gas Turbine Engines
[20] Radun, A. , and Richter, E. , “Detailed Power Inverter Design for a 250 kW Switched Reluctance Aircraft Engine Starter Generator,” SAE Paper 931388 , April 1993 .
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Detailed power converter design for a 30kW s starter/generator used in aircraft
[7] Arthur Radun and Eike Richter, “A Detailed Power Inverter Design for a 250kW Switched Reluctance Aircraft Engine Starter /Generator,” in Proc. SAE Aerospace Atlantic Conference & Exposition, April, 1993.
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Analysis of the four-phase switched reluctance motor drive under the lacking one phase fault condition
S. R. MacMinn, et al., “Control of a switched reluctance aircraft engine starter -generator over a very wide speed range”, in Proceedings of the IEEE 24th Intersociety .
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High power density switched reluctance motor drive for aerospace applications
[5] S.R. MacMinn, J.W. Sember, “Control of a Switched- Reluctance Aircraft Engine Starter -Generator Over a Wide Speed Range,” Proceedings of IECEC-89 Washington, D.C., .
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Effects of Electrochemical Potential on the Slow Strain Rate Fracture of 4340 Steel in a Combustion Product Residue
ABSTRACT: Steel breech chambers in cartridge-ignition aircraft engine starters have failed in service by fracture of the chamber dome during firing.