Supports – Aircraft engine support – Three or more circumferentially spaced supports
Patent
1981-02-05
1986-11-25
Schultz, William H.
Supports
Aircraft engine support
Three or more circumferentially spaced supports
F16M 1300
Patent
active
046244360
ABSTRACT:
An aircraft engine mount is disclosed which has removable struts attached between the front upper and lower portions of the engine and the airframe during servicing, and a front lower mount having a spherical bearing which permits the engine to pivot about a generally vertical axis at the front of the engine. A rear mounting ring attached to the engine is detachable from the airframe during servicing, accomplished by rotating the aft portion of the engine outward through an access door about an axis at the front of the engine. An angled load bearing pin attached to the rear portion of the engine supplements the rear mounting ring so as to transmit to the airframe the forward loads of the engine experienced during a crash.
REFERENCES:
patent: 694648 (1902-03-01), Jordan et al.
patent: 1852927 (1932-04-01), Hall
patent: 2343426 (1944-03-01), Tyler
patent: 2637516 (1953-05-01), Kessler
patent: 2969715 (1961-01-01), Mosby
patent: 3031929 (1962-05-01), Prutzman
patent: 3222017 (1965-12-01), Bobo
Learfan Propulsion System, Published by Society of Automotive Engineers Inc., 1980.
Cooney Daniel E.
Miller Russell D.
Lear Fan Corp. (U.S.)
Schultz William H.
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