B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 33/08 (2006.01) F02C 1/10 (2006.01) F02C 7/12 (2006.01) F28D 21/00 (2006.01)
Patent
CA 2048807
13DV-10540 ABSTRACT OF THE DISCLOSURE A heat exchange system for a supersonic flight vehicle. A first conduit connects the gas (e.g., helium) exit of a compressor of a gas-driven turbocompressor to the gas inlet of a turbine of the turbocompressor, and a second conduit connects the gas outlet of the turbine to the gas entrance of the compressor. The first conduit has a portion positioned near a hotter temperature region (e.g., the combustor wall) and the second conduit has a portion positioned near a colder temperature region (e.g., the fuel region) of the flight vehicle. The temperature difference self powers the turbocompressor which can transfer large amounts of heat and which is hermetically-sealed in a housing against gas leaks.
Coffinberry George A.
Company General Electric
Craig Wilson And Company
LandOfFree
Self-powered heat exchange system does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Self-powered heat exchange system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Self-powered heat exchange system will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1779914