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公开(公告)号:US20240280049A1
公开(公告)日:2024-08-22
申请号:US18650586
申请日:2024-04-30
Applicant: General Electric Company , GE Avio S.r.l.
Inventor: Daniel Alan Niergarth , Jorge de Luis , Douglas Downey Turner , Michael Macrorie , Keith W. Wilkinson , Arthur William Sibbach , Vincenzo Martina
CPC classification number: F02C6/06 , F02C7/185 , F05D2260/213
Abstract: A gas turbine engine is provided having a turbomachine comprising a compressor section, a combustion section, and a turbine section arranged in serial flow order, the compressor section having a high pressure compressor defining a high pressure compressor exit area (AHPCExit) in square inches and the turbine section having a drive turbine defining a drive turbine exit area (ADTExit) in square inches, the turbomachine further comprising a drive turbine shaft coupled to the drive turbine; wherein the gas turbine engine defines a maximum exhaust gas temperature (EGT) in degrees Celsius, a maximum drive turbine shaft torque (TOUT) in Newton meters, and a corrected specific power (CSP) in Newtons squared times degrees Celsius over meters squared, wherein the corrected specific power is determined as follows:
(
T
O
U
T
A
D
T
E
x
i
t
)
2
*
E
G
T
A
H
P
C
E
x
i
t
*
1
0
-
1
1
;
wherein CSP is greater than 0.0001194×EGT2−0.103×EGT+22.14 and less than 0.0003294×EGT2−0.306×EGT+77.91; and wherein EGT is greater than 525 degrees Celsius and less than 1250 degrees Celsius.-
公开(公告)号:US12006860B2
公开(公告)日:2024-06-11
申请号:US18133665
申请日:2023-04-12
Applicant: Polaris Industries Inc.
Inventor: James H. Buchwitz , Lucas R. Salfer , Derek Zimney , Tim Keller , Karsten Scholle , Marcel Semrau , Clifton J. Seusy
IPC: F02B37/18 , F02B37/02 , F02B37/16 , F02B37/22 , F02B75/02 , F02C5/00 , F02C6/06 , F02C6/12 , F02C9/18 , F02D9/08 , F02D23/00 , F02D41/00 , F02M35/10
CPC classification number: F02B37/186 , F02B37/025 , F02B37/16 , F02B37/162 , F02B37/164 , F02B37/22 , F02B37/225 , F02B75/02 , F02C5/00 , F02C6/06 , F02C6/12 , F02C9/18 , F02D9/08 , F02D23/00 , F02D41/0007 , F02M35/10026 , F02M35/10091 , F02M35/10157 , F02B2075/025 , F05D2220/40
Abstract: A turbocharger and method of controlling the same includes a turbine housing comprising an inlet and an outlet, turbine wheel coupled to a shaft. The turbine housing comprising a first scroll and a second scroll for fluidically coupling the inlet and the turbine wheel. The first scroll has a first end adjacent the inlet and a second end adjacent the turbine wheel. The second scroll has a third end adjacent the inlet and a fourth end adjacent the turbine wheel. An exhaust gas diverter valve is coupled to the turbine housing restricting flow into the first scroll or the second scroll.
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公开(公告)号:US11859543B2
公开(公告)日:2024-01-02
申请号:US17967501
申请日:2022-10-17
Applicant: Pratt & Whitney Canada Corp.
Inventor: Jason Nichols , Ryan Perera
CPC classification number: F02C6/06 , F02C7/32 , F02K3/00 , F04D29/284 , F04D29/288 , F04D29/44 , F04D29/441 , F05D2220/32 , F05D2250/52 , F05D2250/71
Abstract: A diffuser pipe has a tubular body defining a pipe center axis extending therethrough. The tubular body includes a first portion extending in a generally radial direction from an inlet of the tubular body, a second portion extending in a generally axial direction and terminating at a pipe outlet, and a bend portion fluidly linking the first portion and the second portion. The tubular body has a length defined between the inlet and the pipe outlet. The tubular body has cross-sectional profiles defined in a plane normal to the pipe center axis. An area of the cross-sectional profile at the pipe outlet is at least 20% greater than an area of the cross-sectional profile at a point upstream from the pipe outlet a distance corresponding to 10% of the length of the tubular body.
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公开(公告)号:US11846196B2
公开(公告)日:2023-12-19
申请号:US16797194
申请日:2020-02-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Dmitriy B. Sidelkovskiy , Pitchaiah Vijay Chakka , Michael Winter , Daniel Bernard Kupratis , Nathan L. Messersmith
IPC: F01D15/10 , B64D27/10 , B64D27/24 , B64D41/00 , F01D15/12 , F02C6/06 , F02K3/065 , H02K7/116 , H02K7/18 , H02K7/20 , H02K11/00 , B64D27/02
CPC classification number: F01D15/10 , B64D27/10 , B64D27/24 , B64D41/00 , F01D15/12 , F02C6/06 , F02K3/065 , H02K7/116 , H02K7/1823 , H02K7/20 , H02K11/0094 , B64D2027/026 , F05D2220/50 , F05D2220/76
Abstract: An after-fan system for an engine may comprise an after-fan turbine an electrical generator operationally coupled to the after-fan turbine, and an electric motor electrically coupled to the electrical generator. The electrical generator may be configured to generate an electrical current in response to rotation of the after-fan turbine. The electric motor may be configured to generate torque.
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公开(公告)号:US11788465B2
公开(公告)日:2023-10-17
申请号:US17578612
申请日:2022-01-19
Applicant: General Electric Company
Inventor: Brandon Wayne Miller , Patrick Michael Marrinan , Arthur William Sibbach , Scott Alan Schimmels , Scott David Hunter
CPC classification number: F02C6/06 , F02C6/08 , F02C7/32 , F02C9/00 , F02K3/04 , F05D2220/32 , F05D2220/76
Abstract: A gas turbine engine comprises a turbomachine defining a core flow therethrough during operation. A flow tap is provided in fluid communication with the turbomachine, wherein the flow tap is configured to receive a portion of the core flow therethrough as a bleed flow. A bleed assembly includes a machine load, a bleed flow machine, and a bleed regulator. The bleed flow machine is disposed in fluid communication with the turbomachine through the flow tap, and is configured to drive the machine load. The bleed regulator is configured to regulate a bleed output provided to the bleed flow machine by controlling a capture rate of the bleed flow by the bleed flow machine.
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公开(公告)号:US11761349B2
公开(公告)日:2023-09-19
申请号:US17218564
申请日:2021-03-31
Applicant: Hamilton Sundstrand Corporation
Inventor: Darryl A. Colson , Eric Chrabascz
CPC classification number: F01D25/162 , F01D25/24 , F02C6/06 , F04D29/424 , F16C17/024 , F16C35/02 , F16C37/00 , F05D2220/50 , F05D2240/52 , F05D2240/54
Abstract: A bearing housing for a two-wheel air cycle machine includes a first housing portion, a second housing portion, a third housing portion, and a journal bearing bore. The first housing portion is centered around an axis and has a first side and a second side. The second side is positioned axially away from the first side. The second housing portion is centered around the axis and has a first side and a second side. The second side is positioned axially away from the first side. The first side of the second housing portion connects to the second side of the first housing portion. The third housing portion is centered around the axis and has a first side and a second side. The second side is positioned axially away from the first side. The first side of the third housing portion connects to the second side of the second housing portion. The journal bearing bore is centered axially with in the bearing housing and has a diameter of D1.
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公开(公告)号:US20220128005A1
公开(公告)日:2022-04-28
申请号:US17274262
申请日:2020-04-02
Applicant: Mike Richard John Smith
Inventor: Mike Richard John Smith
Abstract: The engine is adapted to generate thrust or designed to generate torque includes a combustor, the combustor generates an exhaust gas flow to push the rotor blades of a rotor in a rotor housing, the exhaust gas flow rotates the rotor, shaft, and fan which produces a rotating force and produces an air flow. The rotor housing having a first wall, a second wall, and a third wall which guides the exhaust gas flow until the exhaust gas flow reaches a housing gap at the second wall and the exhaust gas flow moves out from the rotor housing, while the first wall having another housing gap for the air flow to go through to cool the rotor and the cooling process adds torque to the engine. The engine includes an optional wind turbine assembly. An air compressor is either driven by an electric motor or driven by other means.
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公开(公告)号:US20220003154A1
公开(公告)日:2022-01-06
申请号:US17476761
申请日:2021-09-16
Applicant: Polaris Industries Inc.
Inventor: Sean Trihey , Darren HEDLUND , Reed HANSON , Lucas SALFER , James BUCHWITZ , Derek ZIMNEY
IPC: F02B37/18 , F02B75/02 , F02D9/08 , F02B37/16 , F02M35/10 , F02C5/00 , F02C6/06 , F02C9/18 , F02B37/02
Abstract: A turbocharger and method of controlling the same includes a turbine housing comprising an inlet and an outlet, turbine wheel coupled to a shaft. The turbine housing comprising a first scroll and a second scroll for fluidically coupling the inlet and the turbine wheel. The first scroll has a first end adjacent the inlet and a second end adjacent the turbine wheel. The second scroll has a third end adjacent the inlet and a fourth end adjacent the turbine wheel. An exhaust gas diverter valve is coupled to the turbine housing restricting flow into the first scroll or the second scroll.
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公开(公告)号:US20210131348A1
公开(公告)日:2021-05-06
申请号:US16472431
申请日:2018-01-29
Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.
Inventor: Hideyuki UECHI , Norihisa MATAKE , Kouji HORIZOE , Shigenori SUEMORI , Yasutaka AOKI , Yuya KONNO
IPC: F02C6/06 , F02C7/224 , F02C3/22 , F01K23/02 , F01K27/02 , H01M8/0612 , H01M8/04701 , H01M8/04791 , H01M8/04082
Abstract: A plant includes a fuel supply line for supplying high-pressure fuel gas; and at least one expander disposed in the fuel supply line and configured to extract power from the high-pressure fuel gas by expanding the high-pressure fuel gas.
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公开(公告)号:US20200378303A1
公开(公告)日:2020-12-03
申请号:US16429606
申请日:2019-06-03
Applicant: PRATT & WHITNEY CANADA CORP.
Inventor: Jason NICHOLS , Ryan John PERERA
Abstract: A diffuser pipe has a tubular body defining a pipe center axis extending therethrough. The tubular body includes a first portion extending in a generally radial direction from an inlet of the tubular body, a second portion extending in a generally axial direction and terminating at a pipe outlet, and a bend portion fluidly linking the first portion and the second portion. The tubular body has a length defined between the inlet and the pipe outlet. The tubular body has cross-sectional profiles defined in a plane normal to the pipe center axis. An area of the cross-sectional profile at the pipe outlet is at least 20% greater than an area of the cross-sectional profile at a point upstream from the pipe outlet a distance corresponding to 10% of the length of the tubular body.
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