Invention Grant
- Patent Title: Inlet manifold for multi-tube pulse detonation engine
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Application No.: US15109049Application Date: 2014-12-19
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Publication No.: US10393016B2Publication Date: 2019-08-27
- Inventor: James D. Hill , Michael J. Cuozzo
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- International Application: PCT/US2014/071576 WO 20141219
- International Announcement: WO2015/138033 WO 20150917
- Main IPC: F02C5/02
- IPC: F02C5/02 ; F02C5/10 ; F02C6/08 ; F23R7/00

Abstract:
An inlet manifold for a multi-tube pulse detonation engine includes a vaneless diffuser disposed in a first zone to collect an air discharged from a compressor; a vaned diffuser including a plurality of guide vanes disposed in a second zone to slow the air from the compressor; a plenum disposed in a third zone located next to second zone to provide the air from the compressor to chambers; and a splitter disposed in a fourth zone to split the air from the compressor into an airflow required by each pulse detonation tube for detonation.
Public/Granted literature
- US20160326956A1 INLET MANIFOLD FOR MULTI-TUBE PULSE DETONATION ENGINE Public/Granted day:2016-11-10
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