Throttle lever for controlling the speed of at least one...

Aeronautics and astronautics – Aircraft control – Pilot operated

Reexamination Certificate

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Details

C074S491000

Reexamination Certificate

active

07143984

ABSTRACT:
A throttle lever that for being pivoted by a pilot of an aircraft may include a guidance device that is integral with the lever and capable of interacting with first and second guide tracks. The first guide track allows the lever to be moved to continuously control the reverse thrust speed. The second guide track has a plurality of detents for receiving the guidance device so that the lever may take different positions, each of which controls a particular forward engine speed. An auxiliary guide track allows the lever to be moved to continuously control the forward speed of the engine.

REFERENCES:
patent: 2417691 (1947-03-01), Kelley et al.
patent: 2789418 (1957-04-01), Machlanski
patent: 2865171 (1958-12-01), Gaubatz
patent: 2901919 (1959-09-01), Cravero
patent: 2945347 (1960-07-01), Colley
patent: 2967436 (1961-01-01), Steinlein
patent: 2999355 (1961-09-01), Fishpaw et al.
patent: 4567786 (1986-02-01), Sakurai
patent: 4651954 (1987-03-01), Miller
patent: 0431655 (1991-06-01), None

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