Aircraft auto throttle system

• US 5,613,652 A
• Filed: 10/21/1994
• Issued: 03/25/1997
• Est. Priority Date: 10/21/1994
• Status: Expired due to Term

• Current Assignee: Safe Flight Instrument Corporation
• Original Assignee: Safe Flight Instrument Corporation
• Inventors: Greene, Leonard M.
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US08/327,040
• Time in Patent Office: 886 Days
• Field of Search: 60/39.281, 244/234, 244/236, 244/197, 244/220, 244/221, 244/75 R, 192/41 R, 192/44
• US Class Current: 244/76.00R
• CPC Class Codes: B64D 31/02 Initiating means

Abstract

An auto throttle system for FAYDEC equipped aircraft includes a remote friction element which is separated from a pilot'"'"'s console. The system also includes an auto throttle control and a manual throttle control which are mechanically coupled through the friction element. The friction element provides the "feel" of a cable operated throttle system and allows a pilot to manually override the auto throttle without a significant change in the torque required to advance or retard the throttle. The system also includes a servo motor, gear drive and shaft with the friction element disposed on the shaft. A mechanical coupling connects the shaft and the manual control so that any changes caused by the auto throttle cause a corresponding change in a pilot'"'"'s manual throttle control.

Claims

1. An auto throttle system for aircraft equipped with a full authority digital engine control comprising:

automatic means for controlling the power output of an engine;

manually operable means for controlling the power output of the engine;

a remote friction clutch which is separate from said manually operable means; and

mechanical means coupling said automatic means for controlling the power output of an engine and said manually operable means for controlling the power output of an engine through said friction clutch and for providing the feel of a cable based throttle system and allowing the automatic means for controlling the power output of the engine to be overridden by the manually operable means for controlling the power output of the engine without a significant increase in torque.

2. An auto throttle system according to claim 1 in which said manually operable means for controlling the power output of an engine includes a pilot'"'"'s control console and throttle control arm and in which said friction element is separated from said pilot'"'"'s control console.

3. An auto throttle system according to claim 2 in which said automatic means is coupled to said manual means by a servo driven shaft.

4. An auto throttle system according to claim 3 in which said shaft is mechanically coupled to said servo through a gear train.

5. An auto throttle system according to claim 2 which includes output means associated with said pilot'"'"'s console for transmitting a signal representing the position of said throttle control arm to the full authority digital engine control.

6. An auto throttle system for multi-engine aircraft equipped with full authority digital engine control comprising:

automatic means for controlling the power output of a plurality of engines;

manually operable means for controlling the power output of the engines, including a pilot'"'"'s console and a plurality of throttle control arms;

a plurality of remote friction clutches, one of said clutches for each of the engines which is separated from said pilot'"'"'s control console; and

mechanical means for coupling said automatic means for controlling the power output of the plurality of engines and said manually operable means for controlling the power output of the engines through said friction clutches and for providing the feel of a cable based throttle system and allowing the automatic means for controlling the power output of the plurality of engines to be overridden by the manually operable means for controlling the power output of the engines without a significant increase in torque.

7. An auto throttle system according to claim 6 which includes output means associated with said pilot'"'"'s console for transmitting a signal representing the position of each of said throttle control arms to the full authority digital engine control.

8. An auto throttle system according to claim 7 which includes a rotary component for sensing the position of each of said throttle arms.

9. An auto throttle system for an aircraft which is equipped with full authority digital engine control comprising:

a speed control computer for generating a signal in response to an input signal and changes in the flight characteristics of the aircraft;

a manual throttle control for controlling the power output of an engine by means of an electromagnetic coupling;

a rotatable shaft, a servo motor and gear train coupled to said shaft for rotating said shaft in response to a signal from said speed control;

a friction clutch engaging said rotatable shaft;

mechanical means coupling said rotatable shaft through said friction element to said manual throttle control so that said manual throttle control is advanced or retarded in response to a signal from said speed control; and

means acting through said friction clutch for providing the feel of a cable based throttle and for manually overriding any positioning of the manual throttle control by said shaft without any significant increase in the torque required to initially position the manual throttle control.

10. An auto throttle system according to claim 9 in which said friction clutch can be disengaged to thereby disengage the coupling between said rotatable shaft and said manual throttle control.