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:
Feb. 25, 2025

Filed:

Apr. 20, 2022
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventor:

Gilles Debril, Hamburg, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 37/30 (2006.01); B64D 37/04 (2006.01); F17C 1/12 (2006.01);
U.S. Cl.
CPC ...
B64D 37/30 (2013.01); B64D 37/04 (2013.01); F17C 1/12 (2013.01); F17C 2201/0104 (2013.01); F17C 2201/0128 (2013.01); F17C 2203/0329 (2013.01); F17C 2203/0391 (2013.01); F17C 2203/0629 (2013.01); F17C 2203/0673 (2013.01); F17C 2221/012 (2013.01); F17C 2223/0161 (2013.01); F17C 2223/036 (2013.01); F17C 2227/0341 (2013.01); F17C 2270/0189 (2013.01);
Abstract

A cryogenic fluid pressure vessel for an aircraft, having: a first wall layer, which contains carbon fiber-reinforced plastic, having an inner contact surface for the contact with a pressurized cryogenic fluid to be accommodated inside the cryogenic fluid pressure vessel; a second wall layer, which is arranged on an outer surface of the first wall layer and has a thermal barrier; a closable inlet/outlet opening for cryogenic fluid, which extends through the first and the second wall layer; and a structural insert integrated in the first and the second wall layer, which has a fastening connecting piece located on the outside of the cryogenic fluid pressure vessel for mechanically coupling the cryogenic fluid pressure vessel with external structures; wherein the cryogenic fluid pressure vessel forms an essentially cylindrical main body. Furthermore, the present invention provides an aircraft having such a cryogenic fluid pressure vessel.


Find Patent Forward Citations

Loading…