|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-013/00 B64D-013/08 B64D-013/02 B64D-013/06 B64D-037/32|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 3|
A replacement system, which includes a plurality of heat exchangers and a compressing device, is configured to prepare in parallel a medium bled from a low-pressure location of an engine and flowing through a plurality of heat exchangers into a chamber. The compressing device is in communication with the plurality of heat exchangers and regulates a pressure of the medium flowing through the plurality of heat exchangers. The replacement system employs a subsystem to treat the medium from the low-pressure location of the engine before it is received by the...
1. An aircraft comprising a bleed medium, an environmental control system, and an inerting system, wherein the environmental control system provides the bleed medium to the inerting system,wherein the replacement system provides a treated medium to the inerting system in lieu of the bleed medium flowing from the environmental control system to the inerting system,wherein the replacement system comprises: a shaft;a compressor configured to receive and compress a first portion of a chamber medium to produce a compressed medium;a turbine configured to recei...