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:
Mar. 03, 2020

Filed:

Oct. 02, 2015
Applicant:

Airbus Safran Launchers Sas, Paris, FR;

Inventors:

Robert Gazave, Panilleuse, FR;

Frédérick Millon, Saint Marcel, FR;

Jacques Lelong, Puiseux En Bray, FR;

Assignee:

ARIANEGROUP SAS, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 9/97 (2006.01); F02K 9/76 (2006.01); B64G 1/40 (2006.01); F15B 1/02 (2006.01); F15B 11/20 (2006.01); F15B 15/20 (2006.01);
U.S. Cl.
CPC ...
F02K 9/976 (2013.01); B64G 1/40 (2013.01); F02K 9/76 (2013.01); F02K 9/978 (2013.01); F15B 1/02 (2013.01); F15B 11/20 (2013.01); F15B 15/20 (2013.01); F05D 2220/80 (2013.01);
Abstract

A nozzle () for a space vehicle engine (M), the nozzle comprising a stationary portion () and a movable portion (), the nozzle () including a pneumatic deployment system () comprising: a deployment actuator () for deploying the movable portion () of the nozzle (); a high unlocking actuator (); a low unlocking actuator (); and an ejector (); the deployment system () including a feed system () configured so as to, sequentially: move the deployment actuator () from its support position towards its deployment position; move the high and low unlocking actuators () into their high and low unlocking positions; and actuate the ejector so as to eject the deployment system () from the nozzle ().


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