Invention Grant
- Patent Title: Auxiliary power unit inlet
- Patent Title (中): 辅助动力单元入口
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Application No.: US13860775Application Date: 2013-04-11
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Publication No.: US08740135B2Publication Date: 2014-06-03
- Inventor: Stacey H. Light , Jack V. Vitale
- Applicant: United Technologies Corporation
- Applicant Address: US CT Windsor Locks
- Assignee: Hamilton Sundstrand Corporation
- Current Assignee: Hamilton Sundstrand Corporation
- Current Assignee Address: US CT Windsor Locks
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: B64D33/02
- IPC: B64D33/02 ; B64D29/08 ; B64D41/00
Abstract:
An aircraft auxiliary power unit assembly includes an aircraft skin that provides a cavity. It is secured to a structure in an assembled condition and it provides an opening. An auxiliary power unit is arranged within the cavity and is secured to the structure. The aircraft skin substantially covers the auxiliary power unit in the assembled condition. An inlet duct that is removable is secured within the opening and is selectively connected to the auxiliary power unit between the installed and service positions. The installed and service positions are with the aircraft skin in the assembled condition.
Public/Granted literature
- US20130228648A1 AUXILIARY POWER UNIT INLET Public/Granted day:2013-09-05
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