Control apparatus

Aeronautics and astronautics – Aircraft control – Pilot operated

Patent

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Details

244 23D, 74471XY, B64C 1304

Patent

active

049019520

ABSTRACT:
Control apparatus for effecting control of thrust magnitude and thrust vector angle for aircraft of the short take-off and vertical landing type known by the acronym STOVL comprises a fixed housing (10), a manually movable stick member (7) supported with respect to the fixed housing (10) and arranged to provide a throttle input, the stick member (7) including a grip (8) to enable it to be gripped and moved manually relative to the fixed housing (10), and a rotatable collar (9) arranged to provide the thrust vector angle input. Preferably the grip includes an upright hand-datum flange (13) for positively laterally locating a controlling hand and the hand-datum flange (13) is located at one extremity of the grip (8) and the collar (9) is located at the other extremity of the grip (8).

REFERENCES:
patent: 2787746 (1957-04-01), Redmond
patent: 2923502 (1960-02-01), Rossire
patent: 3098628 (1963-07-01), Chaplin
patent: 3599510 (1971-08-01), Scott
patent: 3726497 (1973-04-01), Gannett et al.
patent: 4130259 (1978-12-01), Carlson et al.
patent: 4134560 (1979-11-01), Messerschmidt
patent: 4280371 (1981-07-01), Kobelt
patent: 4567786 (1986-02-01), Sakurai
patent: 4574651 (1986-03-01), Nordstrom
patent: 4667909 (1987-05-01), Curci

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