Gas turbine engine module assembly

Details Gas turbine engine module assembly Gas turbine engine module assembly

1991-06-27

1993-06-22

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3933, 60 3975, 416198A, F02C 720, B63H 100

Patent

active

052207846

ABSTRACT:
A gas turbine engine compressor module subassembly construction and associated assembly method and tooling includes a threaded inner bore on the first stage compressor adapted to receive a tubular tool that slips axially between the compressor bores and the engine central shaft. Securement of the accessible tooling to the module's stationary structure permits assembly and handling of the module independently of the engine shaft.

REFERENCES:
patent: 3528241 (1970-09-01), Venable et al.

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