Invention Grant
- Patent Title: Aerodynamic intercompressor bleed ports
- Patent Title (中): 气动压缩机排气口
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Application No.: US13644597Application Date: 2012-10-04
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Publication No.: US09322337B2Publication Date: 2016-04-26
- Inventor: Jonathan D. Little , Kevin J. Cummings , Paul S. Schweiger , Daniel J. Monahan
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Kinney & Lange, P.A.
- Main IPC: F02C9/18
- IPC: F02C9/18 ; F04D29/52 ; F04D27/02

Abstract:
An air bleed system for a gas turbine engine includes an annular bleed case with a manifold therein. The annular bleed case has a forward section and an aft section and ligaments connecting the two sections. The forward section, the aft section and the ligaments define bleed ports. The manifold is disposed radially outward of the ligaments and communicates with the series of bleed ports.
Public/Granted literature
- US20130340441A1 AERODYNAMIC INTERCOMPRESSOR BLEED PORTS Public/Granted day:2013-12-26
Information query
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