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U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 March 1946

Abstract

The combination with a turbo‐supercharger comprising a turbine adapted to be supplied with operating gases from an internal combustion engine, a compressor adapted to supply air to such an engine, and control valve means for the turbine, of control mechanism for said valve means comprising a movable abutment, means connecting the movable abutment to said valve means to effect regulating movements thereof, means subjecting said movable abutment to the pressure on the discharge side of said compressor, and means for accelerating the effective action of said pressure on said movable abutment responsive to rate of change of said pressure.

Citation

(1946), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 18 No. 3, pp. 107-108. https://doi.org/10.1108/eb031354

Publisher

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MCB UP Ltd

Copyright © 1946, MCB UP Limited