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U.S. Patent Specifications

U.S. Patent Specifications The combination with a turbosupercharger 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. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology , Volume 18 (3): 2 – Mar 1, 1946
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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031354
Publisher site
See Article on Publisher Site

Abstract

The combination with a turbosupercharger 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.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Mar 1, 1946

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