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.

Patent No.:

US 9989015 B1

PDF
Full Text
Expired
Date of Patent:
Jun. 05, 2018

Filed:

Apr. 12, 2013
Applicant:

Snecma, Paris, FR;

Inventors:

Olivier Condaminet, Gasny, FR;

Guy Lecompte, Bonniers sur Seine, FR;

Philippe Matura, Saint Vincent des Bois, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/96 (2006.01); F02K 9/97 (2006.01); F01D 25/28 (2006.01); B64G 1/40 (2006.01); B64G 1/00 (2006.01);
U.S. Cl.
CPC ...
F02K 9/976 (2013.01); B64G 1/401 (2013.01); F01D 25/285 (2013.01); B64G 1/002 (2013.01); F05D 2230/68 (2013.01); F05D 2260/96 (2013.01); Y10T 29/49229 (2015.01);
Abstract

A stage of a space launcher including an engine core, a tank secured above the engine core, and a nozzle including a first deployable nozzle section secured below the engine core, the nozzle further including a second and a third section configured to be situated extending from each other when the nozzle is in a deployed propulsion configuration. The stage further includes a structure for temporarily supporting nozzle sections mounted on the tank, configured to change the nozzle to a configuration for accessing the engine core wherein the nozzle sections are inserted into each other, with the third section bearing against a lower support of the temporary structure.


Find Patent Forward Citations

Condaminet, Olivier. (2018). Launcher stage comprising a temporary support structure for temporarily supporting nozzle sections allowing access to the core of the engine (U.S. Patent No. 9989015). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9989015

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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