or
Bookmark and Share
Operational circuitry for gas turbine engine control
   
Document Number
US Patent 3987394
Issued Date
October 19, 1976
Link
Inventors
Map
Abstract
A mathematical expression is converted and approximations applied to remove complex processes, simplifying the circuitry of system which controls compressor speed in dependence on ambient temperature.
Drawing
Operational circuitry for gas turbine engine control - US Patent 3987394 Drawing
Drawing from US Patent 3987394
Tags:
Description:
Amusing 0%
Clever 0%
Complex 0%
Efficient 0%
Historic 0%
Important 0%
Innovative 0%
Interesting 0%
Practical 0%
Simple 0%
Number of Claims:
1
Comments:
no comments yet
Owner
Published
October 19, 1976
Application Number
05/526,425
Filed
November 22, 1974
US Classification
324/160   324/163 73/497
Int'l Classification
F02C   9/00   (20060101)   F02C   9/32   (20060101)  
Examiner
Assistant Examiner
Priority Data
Nov 28, 1973 [JA] 48-132561
USPTO Field of Search
324/160   324/163   73/497  
Related Patents
4194129 - Armature slip analysis of induction motors with temperature and voltage correction - Owned by Rexnord Inc. (Milwaukee, WI)

Loading of induction motors is monitored and displayed by meters or alarms by analyzing slip of the armature derived from pulse signals indicating motor shaft speed. A special sensor sensing the motor shaft rotation also provides motor operating temperature signals accompanying shaft rotation speed signals. Corresponding circuitry compensates the load display over motor temperature variations. Also, the motor operating voltage is detected and voltage variations are processed to modify the load display for improved accuracy in the presence of voltage variations and by linearization of the slip characteristic.

Claims
Description
About| FAQs| Terms & Disclaimer| Link to Us| Contact Us