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:
Jun. 09, 2015

Filed:

Feb. 11, 2014
Applicant:

Aircelle, Gonfreville l'Orcher, FR;

Inventors:

Helene Malot, Sainte Adresse, FR;

Philippe Bienvenu, Rogerville, FR;

Assignee:

AIRCELLE, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G10K 11/172 (2006.01); F02K 1/82 (2006.01); F02K 1/04 (2006.01); F02K 1/44 (2006.01); F02K 1/80 (2006.01);
U.S. Cl.
CPC ...
F02K 1/827 (2013.01); F02K 1/04 (2013.01); F02K 1/44 (2013.01); F02K 1/80 (2013.01); F05D 2260/30 (2013.01); F05D 2230/232 (2013.01); F05D 2250/283 (2013.01); Y02T 50/671 (2013.01);
Abstract

An exhaust cone for an aircraft turbojet engine includes a front part which has a front end and a rear end. The front end is equipped with a front connecting flange connecting to an outlet of a turbojet engine and the rear end is equipped with a rear connecting flange connecting to a rear part of the exhaust cone. In particular, the front part is further equipped with a sound attenuation structure including an outer skin, and the outer skin overlaps the front connecting flange and the rear connecting flange.


Find Patent Forward Citations

Malot, Helene. (2015). Exhaust cone for aircraft turbojet engine (U.S. Patent No. 9051899). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9051899

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

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