Apparatus and method for the diassembly of an ultra high bypass

Details Apparatus and method for the diassembly of an ultra high bypass Apparatus and method for the diassembly of an ultra high bypass

1993-09-29

1994-05-03

Bertisch, Richard A.

Power plants

Reaction motor

Interrelated reaction motors

60 3931, 416245R, F02K 302

Patent

active

053076230

ABSTRACT:
An apparatus and method for the disassembly of an ultra high bypass turbine engine having an outer engine portion and an inner engine portion. A plurality of fan blades and acoustic panels are removed from the inner portion of the engine. The outer portion of the engine which includes a plurality of fan outlet guide vanes and fan casing are disconnected from the engine and axially removed. Certain outer portions of the engine including a hinged thrust reverser and hinged fan cowling may be coupled to an aircraft pylon and used interchangeably with replacement engines.

REFERENCES:
patent: 3750983 (1973-08-01), Morris
patent: 4022018 (1977-05-01), Tuten et al.
patent: 4044973 (1977-08-01), Moorehead
patent: 4147029 (1979-04-01), Sargisson
patent: 4384453 (1983-05-01), Tudor et al.
patent: 4405285 (1983-09-01), Surdi
patent: 4940196 (1990-07-01), Lardellier
Brochure on the "CFM 56, fan and booster assembly" by CfM International Nov. 1979.
Brochure on the "PW2040", FAA Certification 1987, by United Technologies.

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