Redundant aircraft cooling system for redundant aircraft...

B - Operations – Transporting – 64 – D

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

B64D 13/06 (2006.01) F25B 25/00 (2006.01) F25D 17/02 (2006.01)

Patent

CA 2670241

An aircraft cooling system (1) according to the invention comprises a first coolant stream (4a) which cools at least one first heat load (2a), and a second coolant stream (4b) which cools at least one second heat load (2b), wherein the aircraft cooling system (1) is formed such that the first heat load (2a) and the second heat load (2b) are thermally coupled together. The first heat load (2a) and the second heat load (2b) are formed by two mutually redundant- aircraft components. A third coolant stream (12) can thermally couple the first heat load (2a) and the second heat load (2b) together. The third coolant stream (12) can be cooled by a heat sink (16).

Système (1) de refroidissement d'avion qui comprend un premier écoulement (4a) de refroidissement qui refroidit au moins une première charge (2a) de chaleur et un deuxième écoulement (4b) de refroidissement qui refroidit au moins une deuxième charge (2b) de chaleur. Ledit système (1) de refroidissement d'avion est formé de telle sorte que la première charge (2a) de chaleur et la deuxième charge (2b) de chaleur sont thermiquement couplées ensemble. La première charge (2a) de chaleur et la deuxième charge (2b) de chaleur sont formées de deux pièces d'avion mutuellement redondantes. Un troisième écoulement (12) de refroidissement peut coupler thermiquement ensemble la première charge (2a) de chaleur et la deuxième charge (2b) de chaleur. Le troisième écoulement (12) de refroidissement peut être refroidi par un dissipateur (16) de chaleur.

LandOfFree

Say what you really think

Search LandOfFree.com for Canadian inventors and patents. Rate them and share your experience with other people.

Rating

Redundant aircraft cooling system for redundant aircraft... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Redundant aircraft cooling system for redundant aircraft..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Redundant aircraft cooling system for redundant aircraft... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-1557694

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.