The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 22, 2015

Filed:

Mar. 14, 2012
Applicant:

Jim A. Clark, Jupiter, FL (US);

Inventor:

Jim A. Clark, Jupiter, FL (US);

Assignee:

AEROJET ROCKETOYNE OF DE, INC., Canoga Park, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 9/60 (2006.01); G01M 15/00 (2006.01); G01M 3/04 (2006.01); G01F 1/36 (2006.01); F02K 9/56 (2006.01); G01F 1/44 (2006.01);
U.S. Cl.
CPC ...
F02K 9/60 (2013.01); G01M 3/04 (2013.01); G01M 15/00 (2013.01); F02K 9/56 (2013.01); F05D 2260/80 (2013.01); F05D 2270/301 (2013.01); G01F 1/36 (2013.01); G01F 1/363 (2013.01); G01F 1/44 (2013.01);
Abstract

A rocket engine with a manifold is in communication with a combustion chamber. A sense line extends through the propellant manifold and into the combustion chamber. The sense line includes a venturi arranged downstream from the combustion chamber, and at least one aperture fluidly connecting the propellant manifold to a sense-line passageway downstream from the venturi. A method of sensing conditions in a combustion chamber includes exposing an end of a sense line to the combustion chamber, creating a low static pressure in the sense line at a location upstream from the end, introducing a fluid at the location to purge the sense line, and sensing the conditions downstream from the location.


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