Invention Grant
- Patent Title: Boundary layer excitation aft fan gas turbine engine
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Application No.: US15371589Application Date: 2016-12-07
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Publication No.: US10823056B2Publication Date: 2020-11-03
- Inventor: Gabriel L. Suciu , Jesse M. Chandler
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C6/08
- IPC: F02C6/08 ; F02K3/06 ; F02C7/36 ; F02C3/20 ; B64D33/02 ; F02C3/10 ; B64D27/20 ; F02K3/062 ; B64C1/16 ; B64C21/00

Abstract:
A boundary layer ingestion engine includes a gas generator and a turbine fluidly connected to the gas generator. A fan is mechanically linked to the turbine via a shaft such that rotation of the turbine is translated to the fan. A boundary layer ingestion inlet is aligned with an expected boundary layer, such that the boundary layer ingestion inlet is configured to ingest fluid from a boundary layer during operation of the boundary layer ingestion engine.
Public/Granted literature
- US10781749B2 Boundary layer excitation aft fan gas turbine engine Public/Granted day:2020-09-22
Information query
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