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RELIABILITY OF TEMPERATURE CONTROLS
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English
Abstract
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Citation
DESI, G. and WOOD, C., "RELIABILITY OF TEMPERATURE CONTROLS," SAE Technical Paper 540164, 1954, https://doi.org/10.4271/540164.Also In
References
- “A PILOT'S VIEWPOINT OF TURBOJET CONTROL REQUIREMENTS” presented by LaCroix R. E. SAE annual meeting in Detroit January 1954
- Trade Name by Manning, Maxwell and Moore Incorporated, Stratford, Conn
- All temperatures are as indicated by the standard turbine outlet thermocouples supplied on the engine. These thermocouples have a time constant of 0.8 seconds under sea level static conditions when the engine is operating at either military or afterburning thrust
- Motor rotation is said to be in the “closing” direction when its effect is to decrease exhaust nozzle area. The rotation is said to be in the “opening” direction when its effect is to increase exhaust nozzle area. It should be noted that turbine outlet temperature increases with the decrease in exhaust nozzle area