Geodesic engine mount structure

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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F02G 100

Patent

active

054289521

ABSTRACT:
The lack of torsional rigidity in the mounting of a turbine engine (10) to a transmission (12) in a power unit (14), (16) is avoided utilizing a mounting structure including a relatively small ring-like base (58), (60) connected to the transmission (12) and a relatively larger, ring-like base (66) connected to the engine shroud (32). A plurality of struts (68) extend between the bases (58), 60) and (66) and are configured to define a series of triangular and/or trapezoidal openings (76). The arrangement of the struts (68) and the openings (76) provides exceptional torsional rigidity.

REFERENCES:
patent: 2410450 (1946-11-01), Kroon
patent: 2718756 (1955-09-01), McDowall
patent: 2738647 (1956-03-01), Hill
patent: 2828607 (1958-04-01), Johnson
patent: 3020004 (1962-12-01), Blyth et al.
patent: 3352114 (1967-11-01), Wilde et al.
patent: 3675418 (1972-07-01), Lenkelt et al.
patent: 3750983 (1973-08-01), Morris
patent: 3902314 (1975-09-01), Straniti
patent: 4040249 (1977-08-01), Kahle et al.
patent: 4266741 (1981-05-01), Murphy
patent: 4326682 (1982-04-01), Nightingale
patent: 4603721 (1986-08-01), White
Flight, Mar. 13, 1947, pp. a, b, c, d.

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