|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 13 인용 특허 : 5|
A power and cooling management system configured to flexibly couple various adaptive modules to an integrated power and cooling unit to suit any aircraft platform is provided. The integrated power and cooling unit has a compressor(s), power turbine(s), cooling turbine(s) and integral starter generator(s) mounted to the shaft of the power and cooling turbine. The integrated power and cooling unit may be pneumatically and/or pneumatically coupled to an adaptive module that comprises an additional compressor and an additional turbine or electrically coupled...
What is claimed is: 1. A power and cooling system, comprising: an integrated power and cooling unit, comprising: a first compressor connected to a discharged air inlet of an engine; a power turbine located at downstream of the compressor; a cooling turbine connected to the engine discharged air; and a first starter generator mounted to a common shaft of the power and cooling turbine; and an adaptive module pneumatically coupled to the integrated power and cooling unit, the adaptive module comprising: a second compressor pneumatically coupled to downstr...