The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 08, 1995

Filed:

Nov. 18, 1993
Applicant:
Inventor:

Leslie R Summerfield, Bristol, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D / ; B64D / ;
U.S. Cl.
CPC ...
36443102 ; 36443101 ; 36443104 ; 60 39281 ; 60 3901 ; 60 3959 ; 60243 ;
Abstract

In the event of incipient engine speed or loss of normal engine control fuel flow rate in a jet engine is limited by a speed governor. A speed governor arrangement with optionally selectable emergency speed control is described. Maximum engine speed limits are stored in ROM and compared with sensed values. When an overspeed threshold is reached an output is produced to reduce fuel flow rate. If normal engine control is lost an alternative governor mode can be selected in which a second fuel flow rate is read from ROM as determined by the pilot's speed lever setting. A lowest wins circuit selects the lower of this emergency control or the governor limit signal to drive the fuel metering unit.


Find Patent Forward Citations

Summerfield, Leslie. (1995). Aircraft engine emergency control system (U.S. Patent No. 5440490). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/5440490

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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