HIGH TEMPERATURE DISK CONDITIONING SYSTEM
摘要:
A gas-circulation system for conditioning a disk of an aircraft may comprise a first takeoff port configured to extract a combusted gas and a second takeoff port configured to extract an uncombusted gas. A first valve may comprise an inlet in fluid communication with the first and second takeoff ports and an outlet of the first valve in fluid communication with the disk.
公开/授权文献
信息查询
0/0