Aeronautics and astronautics – Aircraft power plants – Mounting
Patent
1975-11-12
1977-07-26
Blix, Trygve M.
Aeronautics and astronautics
Aircraft power plants
Mounting
60226R, 181 33HD, 248 5, B64D 2716, B64D 2908
Patent
active
040378098
ABSTRACT:
A device for mounting in a nacelle on an airframe a turbojet engine contad by a casing, the device being of the type comprising a mast member integral with the airframe, a nacelle coaxial to the turbojet engine, quick release locking members connecting the compressor casing to the rear nacelle section, and elements for releasably connecting the rear nacelle section to the mast member wherein the device further comprises sliding guides permitting the nacelle to be displaced parallel to the longitudinal axis of the engine, along the mast member between an active and advanced position in which the rear nacelle section is supported against the casing of the compressor, and an inactive or remote position, in which the rear nacelle section is separate from the casing, and links directly connecting the casing of the engine to the mast with a view to ensuring support of the turbojet engine when the rear nacelle section is in the inactive or remote position.
REFERENCES:
patent: 2783003 (1957-02-01), Ralston et al.
patent: 2958480 (1960-11-01), Saulnier
patent: 2982497 (1961-05-01), Worley
patent: 3084507 (1963-04-01), Kleinhans et al.
patent: 3194515 (1965-07-01), Cohan
patent: 3637042 (1972-01-01), Raynes
Barefoot Galen L.
Blix Trygve M.
Societe Nationale d'Etude et de Construction de Moteurs d'Aviati
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