Invention Grant
- Patent Title: Tip turbine engine composite tailcone
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Application No.: US15784629Application Date: 2017-10-16
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Publication No.: US10760483B2Publication Date: 2020-09-01
- Inventor: Brian Merry , Gabriel L. Suciu , James W. Norris
- 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: F02C1/00
- IPC: F02C1/00 ; F02C3/073 ; F02K1/04 ; F02K3/068

Abstract:
A non-metallic tailcone in a tip turbine engine includes a tapered wall structure disposed about a central axis. The non-metallic tailcone is fastened to a structural frame in the aft portion of the tip turbine engine. The tip turbine engine produces a first temperature gas stream from a first output source and a second temperature gas stream from a second output source. The second temperature gas stream is a lower temperature than the first temperature gas stream. The second temperature gas stream is discharged at an inner diameter of the tip turbine engine over an outer surface of the tailcone. Discharging the cooler second temperature gas stream at the inner diameter allows a non-metallic to be used to form the tailcone.
Public/Granted literature
- US20180106194A1 TIP TURBINE ENGINE COMPOSITE TAILCONE Public/Granted day:2018-04-19
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