NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Real time pressure signal system for a rotary engineA real-time IMEP signal which is a composite of those produced in any one chamber of a three-lobed rotary engine is developed by processing the signals of four transducers positioned in a Wankel engine housing such that the rotor overlaps two of the transducers for a brief period during each cycle. During the overlap period of any two transducers, their output is compared and sampled for 10 microseconds per 0.18 degree of rotation by a sampling switch and capacitive circuit. When the switch is closed, the instantaneous difference between the value of the transducer signals is provided while with the switch open the average difference is produced. This combined signal, along with the original signal of the second transducer, is fed through a multiplexer to a pressure output terminal. Timing circuits, controlled by a crank angle encoder on the engine, determine which compared transducer signals are applied to the output terminal and when, as well as the open and closed periods of the switches.
Document ID
19840014491
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Rice, W. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 31, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: NASA-CASE-LEW-13622-1
Patent Application Number: US-PATENT-APPL-SN-350473
Patent Number: US-PATENT-4,428,226
Accession Number
84N22559
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-13622-1|US-PATENT-4,428,226
Patent Application
US-PATENT-APPL-SN-350473
No Preview Available