|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/039.5; 060/687; 060/772|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 10 인용 특허 : 32|
Thermally compliant auxiliary power unit (APU) ducts arrangements, and associated systems and methods are disclosed. A system in accordance with one embodiment includes an auxiliary power unit exhaust, that in turn includes an exhaust flow conduit, a housing disposed outwardly from the conduit, a support providing a load path between the conduit and the housing, and a baffle positioned along the flow conduit. At least one of the support and the baffle can have a resilient, radially compressible portion between the flow conduit and the housing.
We claim: 1. An aircraft system, comprising; an auxiliary power unit exhaust that includes: an exhaust flow conduit; a housing disposed outwardly from the flow conduit; a support providing a loadpath between the flow conduit and the housing; and a baffle positioned along the flow conduit; wherein at least one of the support and the baffle has a resilient, radially compressible portion between the flow conduit and the housing, the compressible portion having cross-sectional profile shape that varies in a non-monotonic manner. 2. The system of claim 1...