Invention Grant
- Patent Title: Flutter inhibiting intake for gas turbine propulsion system
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Application No.: US15452627Application Date: 2017-03-07
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Publication No.: US10428685B2Publication Date: 2019-10-01
- Inventor: Bruce L. Morin , Daniel L. Gysling , Mani Sadeghi
- 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
- Main IPC: F01D25/06
- IPC: F01D25/06 ; B64D33/02 ; F02C7/045 ; F02K1/82 ; F02K3/06 ; G10K11/172

Abstract:
Disclosed is flutter damper including a first cavity having a radially inner side in fluid communication with a flow path, and a second cavity having a radially inner side in fluid communication with a radially outer side of the first cavity, and the flutter damper having an impedance characteristic at one or more target frequencies defined as ftarget=fS,ND+Ω·ND wherein fS,ND is a resonance frequency corresponding to a structural mode of a rotating component, ND is a nodal diameter count of the structural mode, and Ω is a rotational speed of the rotating component, and wherein the flutter damper has the following impedance characteristic at the one or more targeted frequencies R≥2ρc −3ρc≤X≤−0.6ρc wherein R is the real part of the impedance characteristic, X is the imaginary part of the impedance characteristic, ρ is air density, and c is speed of sound.
Public/Granted literature
- US20180258788A1 FLUTTER INHIBITING INTAKE FOR GAS TURBINE PROPULSION SYSTEM Public/Granted day:2018-09-13
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