Nicolas Claude Parmentier,Pierre Froment,Jean-Francois Rideau,Bruno Thoraval
申请号：
GB20160013741
公开号：
GB2538018(A)
申请日:
2015.01.29
申请国别(地区):
英国
年份:
2016
代理人:
摘要：
The invention relates to an aircraft turboprop engine (110) comprising at least a low-pressure body (12) and a high-pressure body (14), the low-pressure body driving a propeller by means of a first gearbox (16), the turboprop engine also comprising means for supplying air to an air-conditioning circuit (36) of an aircraft cabin, characterised in that said supply means comprise at least one compressor (60) of which the rotor (61) is coupled to the low-pressure body, said compressor (60) comprising an air inlet (62) connected to means (66) for bleeding air from an air inlet duct (32) of the turboprop engine.
