|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||165/70 ; 165/41 ; 165/10414 ; 422/200|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 20 인용 특허 : 0|
A heat exchanger for use in high speed aircraft propulsion engines provides a plurality of heat pipes wherein the evaporator sections of the heat pipes are disposed in a hot fluid flow conduit and the condenser sections are disposed in a cold fluid flow conduit and the flow conduits are separated by a vented cavity and thin heat transfer fins are disposed around the condenser sections. Another embodiment provides a reactor using the heat exchanger and having a metalized, preferably with platinum, carbon fiber supported catalyst in the form of batting wov...
A reactor having a heat exchanger comprising: a cold fluid conduit, a hot fluid conduit spaced apart from said cold fluid conduit, a plurality of heat pipes having evaporator sections disposed in said hot fluid conduit and condenser sections disposed in said cold fluid conduit, heat transfer fins mounted on said condenser sections, a vented cavity between said hot fluid conduit and said cold fluid conduit, and a metalized carbon fiber supported catalyst disposed between said condenser sections.