Multi-path secondary power system for an aircraft

Details Multi-path secondary power system for an aircraft Multi-path secondary power system for an aircraft

1998-05-12

2000-11-07

Swiatek, Robert P.

Aeronautics and astronautics

Aircraft power plants

Auxiliary

244 1719, B64D 3500

Patent

active

061424188

ABSTRACT:
An improved single engine military aircraft is provided through the use of an improved secondary power system which incorporates an additional accessory drive, and utilizes improved multi-path system architecture together with optimal distribution of accessories to thereby enhance partial operational flexibility of the secondary power system in both normal and partial failure modes of operation. The additional accessory drive also provides an aircraft in which the engine can be removed with minimal disruption of the EMAD or AMAD and accessories mounted thereon to thereby enhance both initial manufacturability and repairability of the aircraft and secondary power system.

REFERENCES:
patent: 4514976 (1985-05-01), Christoff
patent: 4546865 (1985-10-01), Hodgman et al.
patent: 4747269 (1988-05-01), David
patent: 4900231 (1990-02-01), Kennedy
patent: 4912921 (1990-04-01), Rice et al.
patent: 4915200 (1990-04-01), Jacques et al.
patent: 4979362 (1990-12-01), Versure, Jr.
patent: 4993533 (1991-02-01), Brown
patent: 5040654 (1991-08-01), Trommer
patent: 5265825 (1993-11-01), Ebert et al.

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