Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger
US10011362B2 · kind B2 · utility
4Cited by
13References
12Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | May 14, 2013 |
| Grant date | Jul 3, 2018 |
| Priority date | — |
| Expiry date | Jan 7, 2034 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/50
- WIPO fieldThermal processes and apparatus
- WIPO sectorMechanical engineering
Abstract
An aircraft outer skin heat exchanger includes a first cooling air inlet and a first cooling air duct section, in which a first heat carrier fluid duct section is arranged. A cooling air conveying device is configured to convey a cooling air stream in such a way through the first cooling air inlet and the first cooling air duct section that the cooling air stream is subdivided by a first heat carrier fluid duct section, arranged in the first cooling air duct section, into two partial air streams which flow through the first cooling air duct section substantially parallel to one another and in the same direction.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.