Aircraft autothrottle system
First Claim
1. In a throttle control system for an aircraft having a throttle control lever and automatic control means for automatically controlling the positioning of said lever wherein the improvement comprises means for alternatively connecting said lever to said automatic control means for control of the throttle thereby or disconnecting said lever from said automatic control means to enably manual control of said lever comprising:
- a first plate member connected to said control lever,a second plate member connected to said automatic control means,a clutch mechanism for alternatively either connecting said first and second plate members together or disconnecting said plate members from each other, said clutch mechanism including wedge member means having a surface which abuts against one of said plate members, roller member means which abuts against the other of said plate members, said wedge member means having a wedge shaped surface positioned directly opposite said roller member means, andmeans responsive to manual actuation for alternatively engaging or disengaging said clutch mechanism by driving said wedge member means, said roller member means and said first and second plate members into locking engagement with each other to interconnect the control lever and the automatic control means or releasing the driving of said plate members and said wedge and roller member means from locking engagement thereby disconnecting the control lever from said automatic control means to permit manual control thereof.
1 Assignment
0 Petitions
Accused Products
Abstract
The throttle of an aircraft can be alternatively controlled either by a flight control computer or by the manual control of the pilot. A clutch is installed between the throttle control lever and a control input to the flight control computer which in the autothrottle mode of operation is engaged to enable control of the throttle by the flight control computer with the control lever being positioned in accordance with such control. When manual takeover of the throttle control is desired, a switch is actuated by the pilot which operates to disengage the clutch and thereby disconnects the control output of the computer from the lever so that only manual control is provided. A unique clutch mechanism is employed which utilizes a pair of locking wedges which operate in conjunction with a pair of rollers. The wedges and rollers are driven into engagement with each other by a solenoid, the opposing plates of the clutch being held in locking engagement through the intermediary provided by the wedges and rollers. Emergency "bump" disconnection of the clutch is effected by a pair of microswitches against which a cantilevered spring portion of the control lever abuts when the lever is "bumped", such switches operating to de-energize the solenoid and disengage the clutch.
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Citations
4 Claims
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1. In a throttle control system for an aircraft having a throttle control lever and automatic control means for automatically controlling the positioning of said lever wherein the improvement comprises means for alternatively connecting said lever to said automatic control means for control of the throttle thereby or disconnecting said lever from said automatic control means to enably manual control of said lever comprising:
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a first plate member connected to said control lever, a second plate member connected to said automatic control means, a clutch mechanism for alternatively either connecting said first and second plate members together or disconnecting said plate members from each other, said clutch mechanism including wedge member means having a surface which abuts against one of said plate members, roller member means which abuts against the other of said plate members, said wedge member means having a wedge shaped surface positioned directly opposite said roller member means, and means responsive to manual actuation for alternatively engaging or disengaging said clutch mechanism by driving said wedge member means, said roller member means and said first and second plate members into locking engagement with each other to interconnect the control lever and the automatic control means or releasing the driving of said plate members and said wedge and roller member means from locking engagement thereby disconnecting the control lever from said automatic control means to permit manual control thereof. - View Dependent Claims (2, 3, 4)
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Specification