-
公开(公告)号:US20190086084A1
公开(公告)日:2019-03-21
申请号:US15709333
申请日:2017-09-19
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Carey Clum , Shayan Ahmadian , Christopher W. Robak
CPC classification number: F23R3/04 , F23M20/00 , F23R3/002 , F23R2900/03041 , F23R2900/03044
Abstract: A combustor may include a combustor shell, a particle collection panel, and a combustor panel. The combustor shell may define a plurality of first impingement holes, the particle collection panel may include a plurality of particle collection chambers and may define a plurality of second impingement holes, and the combustor panel may define a plurality of effusion holes. The particle collection panel may be disposed inward of the combustor shell and the combustor panel may be disposed inward of the particle collection panel. Each particle collection chamber may have a closed inward end and an opening defined in an outward end. The particle collection chambers may be configured to entrap particulates.
-
公开(公告)号:US10975713B2
公开(公告)日:2021-04-13
申请号:US16239616
申请日:2019-01-04
Applicant: United Technologies Corporation
Inventor: Eric A. Grover , Brian F. Hilbert , Nathan L. Messersmith , Christopher W. Robak
Abstract: A hydrostatic seal configured to be disposed between relatively rotatable components. The seal includes a base. The seal also includes a seal housing. The seal further includes a shoe operatively coupled to the base and extending axially from a forward end to an aft end. The seal yet further includes a plurality of teeth extending radially from a sealing surface of the shoe, one of the teeth being a longest tooth that extends furthest radially from the sealing surface, the axial distance from the forward end of the shoe to the longest tooth being greater than a radial distance from a radial tooth tip to the sealing surface.
-
公开(公告)号:US20200217216A1
公开(公告)日:2020-07-09
申请号:US16239616
申请日:2019-01-04
Applicant: United Technologies Corporation
Inventor: Eric A. Grover , Brian F. Hilbert , Nathan L. Messersmith , Christopher W. Robak
Abstract: A hydrostatic seal configured to be disposed between relatively rotatable components. The seal includes a base. The seal also includes a seal housing. The seal further includes a shoe operatively coupled to the base and extending axially from a forward end to an aft end. The seal yet further includes a plurality of teeth extending radially from a sealing surface of the shoe, one of the teeth being a longest tooth that extends furthest radially from the sealing surface, the axial distance from the forward end of the shoe to the longest tooth being greater than a radial distance from a radial tooth tip to the sealing surface.
-
公开(公告)号:US10329941B2
公开(公告)日:2019-06-25
申请号:US15148336
申请日:2016-05-06
Applicant: United Technologies Corporation
Inventor: Michael D. Werkheiser , Christopher W. Robak , Thomas J. Martin , Matthew E. Lynch
Abstract: An impingement manifold includes a fluid inlet passage and a pressurized chamber. The pressurized chamber includes at least one lobe. The at least one lobe includes a flow improving feature configured to minimize vorticity of a flow field within the pressurized chamber, and at least one flow outlet.
-
5.
公开(公告)号:US20190048796A1
公开(公告)日:2019-02-14
申请号:US16048738
申请日:2018-07-30
Applicant: United Technologies Corporation
Inventor: Walter A. Ledwith, Jr. , Scott A. Carr , Christopher J. Hanlon , Peter A. White , Theodore W. Hall , John R. Farris , Andrew S. Miller , Christopher W. Robak , David C. Pimenta , David Richard Griffin
Abstract: A method of assembling a gas turbine engine includes setting a build clearance at assembly in response to a running tip clearance defined with a cooled cooling air. A method of operating a gas turbine engine includes supplying a cooled cooling air to a high pressure turbine in response to an engine rotor speed.
-
6.
公开(公告)号:US20170328231A1
公开(公告)日:2017-11-16
申请号:US14640060
申请日:2015-03-06
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Walter A. Ledwith, JR. , Scott A. Carr , Christopher J. Hanlon , Peter A. White , Theodore W. Hall , John R. Farris , Andrew S. Miller , Christopher W. Robak , David C. Pimenta , David Richard Griffin
CPC classification number: F02C3/055 , F01D11/24 , F02C7/185 , F05D2260/213 , F05D2270/20 , F05D2270/44 , Y02T50/676
Abstract: A method of assembling a gas turbine engine includes setting a build clearance at assembly in response to a running tip clearance defined with a cooled cooling air. A method of operating a gas turbine engine includes supplying a cooled cooling air to a high pressure turbine in response to an engine rotor speed.
-
公开(公告)号:US20170321568A1
公开(公告)日:2017-11-09
申请号:US15148336
申请日:2016-05-06
Applicant: United Technologies Corporation
Inventor: Michael D. Werkheiser , Christopher W. Robak , Thomas J. Martin , Matthew E. Lynch
CPC classification number: F01D11/24 , F01D11/20 , F01D25/12 , F02C3/04 , F02C6/08 , F02C7/18 , F05D2220/32 , F05D2240/12 , F05D2240/30 , F05D2260/201 , F05D2300/5021 , Y02T50/676
Abstract: An impingement manifold includes a fluid inlet passage and a pressurized chamber. The pressurized chamber includes at least one lobe. The at least one lobe includes a flow improving feature configured to minimize vorticity of a flow field within the pressurized chamber, and at least one flow outlet.
-
公开(公告)号:US20170080371A1
公开(公告)日:2017-03-23
申请号:US14860604
申请日:2015-09-21
Applicant: United Technologies Corporation
Inventor: Carey Clum , Christopher W. Robak
CPC classification number: B01D45/08 , B01D45/04 , F02C3/04 , F02C7/00 , F05D2220/32 , F05D2260/607 , Y02T50/675
Abstract: A particle collection device for an engine is provided. The particle collection device having: an inlet for directing air towards a first member having a first orifice located therein; and a second member having a second orifice located therein, the second orifice being aligned with the first orifice and wherein the second member and the second orifice are spaced from the first member and the first orifice by a first distance, and wherein the particle collection device is located in the engine.
-
公开(公告)号:US11255267B2
公开(公告)日:2022-02-22
申请号:US16386527
申请日:2019-04-17
Applicant: United Technologies Corporation
Inventor: Christopher W. Robak
IPC: F02C7/18
Abstract: A method of designing a gas turbine engine includes locating purge openings in fluid communication with a first stage cavity. At least one of a cover plate or a rotor disk is positioned adjacent the first stage cavity and radially inward from the purge openings. A portion of a rotor blade is positioned radially outward from the purge openings. A mass flow rate of cooling air through the purge openings is selected based on a radial location of the purge openings to create an air barrier between a radially inner side of the purge openings and a radially outer side of the purge openings.
-
公开(公告)号:US10961858B2
公开(公告)日:2021-03-30
申请号:US16239611
申请日:2019-01-04
Applicant: United Technologies Corporation
Inventor: Eric A. Grover , Brian F. Hilbert , Daniel L. Gysling , Christopher W. Robak
Abstract: A hydrostatic seal configured to be disposed between relatively rotatable components includes a base. The seal also includes a seal housing. The seal further includes a shoe operatively coupled to the base and extending axially from a forward end to an aft end. The seal yet further includes a plurality of teeth extending radially from a sealing surface of the shoe, one of the teeth being a longest tooth that extends furthest radially from the sealing surface, the axial distance from the forward end of the shoe to the longest tooth being greater than a radial distance from a radial tooth tip to the sealing surface.
-
-
-
-
-
-
-
-
-