Fuel supply system for hydrogen aircraft, and tank internal pressure adjustment method
US-2024263745-A1 · Aug 8, 2024 · US
Fuel tank installation
US8960237B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8960237-B2 |
| Application number | US-201213654800-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 18, 2012 |
| Priority date | Oct 18, 2011 |
| Publication date | Feb 24, 2015 |
| Grant date | Feb 24, 2015 |
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- Title
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Abstract
Official abstract text for this publication.
A fuel tank installation comprising: a fuel tank for holding fuel, the fuel tank comprising a fuel tank wall formed with a hole; a fuel pump assembly fitted into the hole in the fuel tank wall with an inner part of the fuel pump assembly protruding from an inner side of the hole and an outer part of the fuel pump assembly protruding from an outer side of the hole; a cage surrounding the outer part of the fuel pump assembly; and a mounting piece which attaches both the cage and the fuel pump assembly to the fuel tank wall.
First claim
Opening claim text (preview).
The invention claimed is: 1. A fuel tank installation comprising: a) a fuel tank wall formed with a hole; b) a fuel pump assembly fitted into the hole in the fuel tank wall with an inner part of the fuel pump assembly protruding from an inner side of the hole and an outer part of the fuel pump assembly protruding from an outer side of the hole; c) a cage surrounding the outer part of the fuel pump assembly; and d) a mounting piece which attaches both the cage and the fuel pu…
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Inventors
Classifications
Operations & Transport · mapped topic
Cross-Sectional Technologies · mapped topic
- B64D37/10Primary
Operations & Transport · mapped topic
Cross-Sectional Technologies · mapped topic
Cross-Sectional Technologies · mapped topic
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Frequently asked questions
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- What does patent US8960237B2 cover?
- A fuel tank installation comprising: a fuel tank for holding fuel, the fuel tank comprising a fuel tank wall formed with a hole; a fuel pump assembly fitted into the hole in the fuel tank wall with an inner part of the fuel pump assembly protruding from an inner side of the hole and an outer part of the fuel pump assembly protruding from an outer side of the hole; a cage surrounding the outer p…
- Who is the assignee on this patent?
- Airbus Operations Ltd, Airbus Operations Limted
- What technology area does this patent fall under?
- Primary CPC classification B64D37/10. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Tue Feb 24 2015 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
- What related patents are in patentsdb?
- We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).