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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: VALVE, STARTER CONTROL, AIRCRAFT ENGINE, FOR T56 ENGINE/C-2 AIRCRAFT
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Supplier: Accuris
Description: STARTER, AIRCRAFT ENGINE, HYDRAULIC, FOR T64 ENGINE
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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: 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: 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, for the purpose of starting aircraft jet engines.
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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: SAE International
Description: More-Electric Aircraft (MEA). As a result, a large number of new electrical loads have been introduced in order to power many primary functions including actuation, de-icing, cabin air-conditioning, and engine start. Therefore electric power generation systems have a key role in
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Supplier: Safran Electrical & Power
Description: the ongoing development of new machines. The starter generator operates as a motor to provide torque for engine starting and as a generator to provide 28V DC electrical power after engine starting. Labinal Power Systems also provides a range of DC generators without the start
- Volt-Ampere: 5,000 to 250,000 VA
- Features: Other
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Supplier: Safran Helicopter Engines
Description: Air Force) but also for the Australian and South African air forces. This APU provides the pneumatic power required for the air turbine starter developed by Microturbo for the main engine as well as 12 kVA of electrical power. It also provides output for cockpit air conditioning.
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Supplier: Electric Generators Direct
Description: 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 •19 hours without refueling (at 1/4 rated load) w/economy idle
- Voltage: 120 V
- Frequency: 60 Hz
- Phase: AC Single Phase Power
- Fuel Type: Gasoline
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Supplier: UL Standards & Engagement
Description: battery chargers; - battery chargers installed on land 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
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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)
Browse Linear Actuators Datasheets for Columbus McKinnon Corporation
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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.