Method of combining ducted fan gas turbine engine modules and ai

Details Method of combining ducted fan gas turbine engine modules and ai Method of combining ducted fan gas turbine engine modules and ai

1997-01-07

1999-01-19

Freay, Charles G.

Power plants

Reaction motor

Interrelated reaction motors

60 3931, 244 54, F02K 302

Patent

active

058602755

ABSTRACT:
In a ducted fan gas turbine engine the fan module is connected rigidly to aircraft structure and flexibly to the core gas generator via flanged annular diaphragms (62,66) thus obviating the exertion of bending loads on the core gas generator casing when the fan intake experiences asymmetric aerodynamic loads.

REFERENCES:
patent: 2680346 (1954-06-01), Michael
patent: 4361296 (1982-11-01), Hall et al.
patent: 4603821 (1986-08-01), White
patent: 5452575 (1995-09-01), Freid
patent: 5524847 (1996-06-01), Brodell et al.

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