Invention Application
- Patent Title: DILUTION HOLES FOR GAS TURBINE ENGINES
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Application No.: US15654324Application Date: 2017-07-19
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Publication No.: US20190024894A1Publication Date: 2019-01-24
- Inventor: Dominic Mongillo , Christopher Whitfield , Tracy Propheter-Hinckley
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Main IPC: F23R3/04
- IPC: F23R3/04 ; F02C3/04 ; F02C7/18 ; F23R3/00

Abstract:
A grommet may define a dilution hole in a combustor panel. The grommet may comprise a set of upstream features such as, for example, a first inlet leading into a first plurality of passages with the first plurality of passages each having a first outlet directed towards an inner diameter of the grommet. A set of perimeter features may include a second inlet leading into a convective cooling passage having a plurality of internal cooling features. The convective cooling passage may further lead into a second plurality of passages each having a second outlet extending about the inner diameter of the grommet in a circumferential direction A set of downstream features may include a third inlet leading to a third plurality of passages each having a third outlet directed towards an outer diameter of the grommet.
Public/Granted literature
- US10408453B2 Dilution holes for gas turbine engines Public/Granted day:2019-09-10
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