AIR PRESSURISATION SYSTEM
简介：There is provided an air pressurisation system for an aircraft, the air pressurisation system comprising: a transmission for driving a rotor of a blower compressor for the air pressurisation system, wherein the transmission comprises: a first input configured to receive drive from a spool of a gas turbine engine; a second input; and an output configured to drive to the rotor of the blower compressor, wherein a speed of the output is determined by a function of speeds of the first and second inputs; and a brake coupled to the second input, wherein the brake is operable to engage and brake the transmission at the second input, in order to fix a transmission ratio of the transmission between the first input and the output.展开
主分类号：B64D 13/ 02(用于与飞机配合或装到飞机上的设备；飞行衣；降落伞；动力装置或推进传动装置的配置或安装)
分类号：B64D 13/ 02;F01D 15/ 10;F01D 21/ 006;F02C 7/ 32;F05D2260/ 40311
发明/设计人：Christopher A. MURRAY
