Invention Application
- Patent Title: TANDEM AIR INLET APPARATUS AND METHOD FOR AN AIRBORNE MOBILE PLATFORM
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Application No.: PCT/US2007/081463Application Date: 2007-10-16
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Publication No.: WO2008115273A3Publication Date: 2008-09-25
- Inventor: ATKEY, Warren A. , PARIKH, Pradip G.
- Applicant: THE BOEING COMPANY , ATKEY, Warren A. , PARIKH, Pradip G.
- Applicant Address: 100 North Riverside Plaza Chicago, Illinois 60606-2016 US
- Assignee: THE BOEING COMPANY,ATKEY, Warren A.,PARIKH, Pradip G.
- Current Assignee: THE BOEING COMPANY,ATKEY, Warren A.,PARIKH, Pradip G.
- Current Assignee Address: 100 North Riverside Plaza Chicago, Illinois 60606-2016 US
- Agency: POOLE, James M.
- Priority: US11/553,181 20061026
- Main IPC: B64D13/02
- IPC: B64D13/02
Abstract:
A tandem inlet apparatus (10) for use with a high speed mobile platform, for example a commercial or military aircraft. The tandem inlet apparatus includes a Pitot inlet (102) for feeding air to a cabin air compressor (CAC) of an air conditioning pack carried on the mobile platform. A flush heat exchanger inlet (104) is disposed forwardly of the Pitot inlet and longitudinally aligned with the Pitot inlet, for supplying cooling air to a heat exchanger of the air conditioning pack. By locating the heat exchanger inlet forwardly and longitudinally in line with the Pitot inlet, the heat exchanger inlet is able to effectively swallow a large portion of the boundary layer (118), which results in a thinner boundary layer (122) at the inlet face of the Pitot inlet. This enables a smaller throat area Pitot inlet (113) to be used, as well as a shorter diverter height (108) to be employed with the Pitot inlet, while still realizing an improved recovery factor (RF) performance with the Pitot inlet. The reduced height Pitot inlet also enables drag to be reduced.
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