|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||62/402 ; ; 62/88|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 18 인용 특허 : 14|
Improved cooling of electronic heat loads aboard aircraft is achieved in a system including a sealable aircraft cabin (10), first and second electronic heat loads (38), (40) and a means (42) for maintaining a desired pressure within the cabin (10). A rotatable turbine wheel (16) is associated with an overboard dump port (32) such that air being dumped overboard from the cabin is expanded to rotate the turbine wheel (16). A mechanical load (20) is connected to the turbine wheel (16) for harnessing the rotation thereof and means (24), (60) are employed for...
An aircraft electronics cooling system comprising: a sealable aircraft cabin; first and second electronic heat loads, said first load requiring a relatively high temperature coolant and said second load requiring a relatively low temperature coolant; means for maintaining a desired pressure within said cabin, including means for providing fresh air to said cabin and means for dumping exhaust air from said cabin overboard; a rotatable turbine wheel associated with said dumping means such that air being dumped overboard is expanded to rotate said turbine w...