Invention Grant
- Patent Title: Damped fluid transfer tube for a gas turbine engine
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Application No.: US15681551Application Date: 2017-08-21
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Publication No.: US10746283B2Publication Date: 2020-08-18
- Inventor: Christopher T. Anglin
- 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: Getz Balich LLC
- Main IPC: F16H57/04
- IPC: F16H57/04 ; F01D9/06 ; F16C3/02 ; F01D25/04 ; F01D25/16

Abstract:
An assembly is provided for a gas turbine engine. This assemble includes a stationary structure configured with a first side, a second side and a bore that extends through the stationary structure between the first side and the second side. The assembly also includes a fluid transfer tube extending within the bore and forming a plenum between a sidewall of the fluid transfer tube and the stationary structure. The fluid transfer tube is configured with a first end at the first side, a second end at the second side, a flowpath and an aperture. The flowpath is at least partially formed by the sidewall and extends through the fluid transfer tube between the first end and the second end. The aperture fluidly couples the flowpath with the plenum.
Public/Granted literature
- US20190056024A1 DAMPED FLUID TRANSFER TUBE FOR A GAS TURBINE ENGINE Public/Granted day:2019-02-21
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