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:
Jan. 21, 1992

Filed:

Feb. 07, 1990
Applicant:
Inventors:

Elizabeth Acton, Cambridge, GB;

Alexander M Cargill, Derby, GB;

Colin F Ross, Cambridge, GB;

Graham P Eatwell, Cambridge, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D / ;
U.S. Cl.
CPC ...
415118 ; 415114 ;
Abstract

A control system actively controls at least one troublesome mode of an unsteady motion phenomenon in turbomachinery in order to enable an increase in the operating range of the turbomachinery. For example, rotor blade flutter or rotating stall may be controlled in a turbocompressor. The control system has a control bandwidth which is at least partly coextensive with the bandwidth of the unsteady motion phenomenon and operates by passing sensor signals related to the unstady motion phenomenon from a sensor array in the turbomachine to a mode filter which produces a signal or signals which are related to the troublesome mode or modes. The selected mode signals are amplified and phase-shifted by time-variable amounts so as to produce control signals having controlled amplitude and phase relationship to the troublesome mode. Actuators in an actuaor array are continuously driven by the control signals and produce physical effects in the turbomachine which act counter to the troublesome mode without exciting others.


Find Patent Forward Citations

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Acton, Elizabeth. (1992). Active control of unsteady motion phenomena in turbomachinery (U.S. Patent No. 5082421). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/5082421

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

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