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公开(公告)号：US11898496B1
公开(公告)日：2024-02-13
申请号：US17870078
申请日：2022-07-21
Applicant: Hamilton Sundstrand Corporation
Inventor： Ryan Prescott Susca , Morgan O'Rorke , Adrian L. Stoicescu
CPC classification number: F02C7/236 , F02C7/232 , F05D2220/323 , F05D2260/607 , F05D2260/84
Abstract: A fuel system of an aircraft engine, having: a boost pump having an input and an output; one or more selector valves; a first component pump having an input fluidly coupled to the output of the boost pump and an output of the first component pump is configured to direct fuel to a first component via the one or more selector valves; and a second component pump having an input that is selectively coupled to either the input or the output of the boost pump by the one or more selector valves, and an output of the second component pump is fluidly coupled to a second component and selectively coupled to the first component by the one or more selector valves.
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公开(公告)号：US20230130997A1
公开(公告)日：2023-04-27
申请号：US17508058
申请日：2021-10-22
Applicant: Hamilton Sundstrand Corporation
Inventor： Matej Rutar , Morgan O'Rorke , Ryan Shook , Ryan Susca
Abstract: In accordance with at least one aspect of this disclosure, a variable displacement pump system can include, a variable displacement pump disposed in a main line and configured to supply pressure to receive a low pressure fluid and to output a high pressure fluid. The main line can connect a hydraulic fluid source to a plurality of system actuators, where the variable displacement pump is disposed in the main line between the hydraulic fluid source and the plurality of system actuators to pressurize the hydraulic fluid.
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公开(公告)号：US20220372941A1
公开(公告)日：2022-11-24
申请号：US17324009
申请日：2021-05-18
Applicant: Hamilton Sundstrand Corporation
Inventor： Ryan Susca , Morgan O'Rorke , Matej Rutar , Todd Haugsjaahabink , Weishun William Ni , Benjamin T. Harder , Ryan Shook
Abstract: A fuel metering system includes a pump with an inlet and an outlet, a first flow path including a first valve fluidically connected to the outlet of the pump, and a second flow path including a second valve fluidically connected to the outlet of the pump, a third valve, and a fourth valve. An electrohydraulic servo valve in a first position hydraulically connects the inlet of the pump to the first, third, and fourth valves to close the first valve, open the third valve, open a first window of the fourth valve, and close a second window of the fourth valve. The electrohydraulic servo valve in a second position hydraulically connects the outlet of the pump to the first, third, and fourth valves to open the first valve, close the third valve, close the first window of the fourth valve, and open the second window of the fourth valve.
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公开(公告)号：US20190112987A1
公开(公告)日：2019-04-18
申请号：US15785717
申请日：2017-10-17
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Morgan O'Rorke , Erick Ramos , Adrian L. Stoicescu
Abstract: A fuel supply system for a gas turbine engine has a fuel tank, a main fuel pump for receiving fuel from the fuel tank, and an electric pump also for receiving fuel from the fuel tank. The main fuel pump and the electric pump both deliver fuel to a sharing valve. The sharing valve selectively delivers fuel downstream into a gas generator portion of the gas turbine engine and to an augmentor. A control is programmed to control the sharing valve, such that fuel flows from the main fuel pump to the augmentor, and to the gas generator at higher demand operation, and does not flow from the main fuel pump at lower demand operation. A gas turbine engine and a method are also disclosed.
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公开(公告)号：US20240026826A1
公开(公告)日：2024-01-25
申请号：US17870078
申请日：2022-07-21
Applicant: Hamilton Sundstrand Corporation
Inventor： Ryan Prescott Susca , Morgan O'Rorke , Adrian L. Stoicescu
CPC classification number: F02C7/236 , F02C7/232 , F05D2220/323 , F05D2260/607 , F05D2260/84
Abstract: A fuel system of an aircraft engine, having: a boost pump having an input and an output; one or more selector valves; a first component pump having an input fluidly coupled to the output of the boost pump and an output of the first component pump is configured to direct fuel to a first component via the one or more selector valves; and a second component pump having an input that is selectively coupled to either the input or the output of the boost pump by the one or more selector valves, and an output of the second component pump is fluidly coupled to a second component and selectively coupled to the first component by the one or more selector valves.
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Patent Agency Ranking
公开(公告)号：US11859551B2
公开(公告)日：2024-01-02
申请号：US17581506
申请日：2022-01-21
Applicant: Hamilton Sundstrand Corporation
Inventor： Morgan O'Rorke , Todd Haugsjaahabink , Matej Rutar , Ryan Susca
CPC classification number: F02C7/22 , F02C7/236 , F02C9/263 , F02C9/26 , F05D2220/323 , F05D2240/35
Abstract: A fuel system can include a selection and shutoff valve (SSOV) configured to allow a primary flow having a primary flow pressure to pass therethrough in a first state such that the primary flow can travel to an output line. The SSOV can also be configured to shut off the primary flow in a second state to prevent the primary flow from travelling to the output line. In the second state, the SSOV can be configured to allow a secondary flow from a secondary flow source to pass therethrough such that the secondary flow can travel to the output line.
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公开(公告)号：US11746710B2
公开(公告)日：2023-09-05
申请号：US17533668
申请日：2021-11-23
Applicant: Hamilton Sundstrand Corporation
Inventor： Morgan O'Rorke , Ryan Susca , Todd Haugsjaahabink
CPC classification number: F02C9/263 , F02C3/00 , F05D2220/32 , F05D2240/35
Abstract: A fluid flow system includes a main valve having a spool, a first chamber, and a second chamber. A pressure difference between the first chamber and the second chamber is configured to move the spool to control fluid flow. An electromechanical meter interface device (EMID) is in fluid communication with at least one of the first and second chambers of the main valve. The EMID is configured to meter fluid from a first source and a second source to the at least one of the first chamber and the second chamber. The first source has a different pressure from the second source. A fixed orifice is arranged between the main valve and the EMID. A fuel system for a gas turbine engine is also disclosed.
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公开(公告)号：US20230167773A1
公开(公告)日：2023-06-01
申请号：US17538965
申请日：2021-11-30
Applicant: Hamilton Sundstrand Corporation (HSC)
Inventor： Ryan Susca , Todd Haugsjaahabink , Morgan O'Rorke
CPC classification number: F02C7/236 , F02C7/232 , F02C9/26 , F01D21/003 , F02C9/18 , F05D2220/32
Abstract: In accordance with at least one aspect of this disclosure, a pump selector system can include a primary pump fluidly connected to provide a primary flow to a fluid destination, a secondary pump fluidly connected to provide a secondary flow to the fluid destination, and a selector valve disposed downstream of the primary pump and the secondary pump. The selector valve can be configured to toggle between a first position configured to allow flow from the primary pump to flow to the fluid destination and to block flow from the secondary pump to the fluid destination, and a second position configured to allow flow from the secondary pump to flow to the fluid destination and to block flow from the primary pump to the fluid destination.
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公开(公告)号：US20230167771A1
公开(公告)日：2023-06-01
申请号：US17537355
申请日：2021-11-29
Applicant: Hamilton Sundstrand Corporation (HSC)
Inventor： Morgan O'Rorke , Ryan Susca , Todd Haugsjaahabink
CPC classification number: F02C7/232 , F02C7/236 , F02C9/263 , F02C9/28 , F02C9/24 , F05D2220/32 , F05D2260/606
Abstract: A fluid delivery system can include a main pump disposed in a primary fluid line configured to receive a low pressure fluid on a low pressure side and output a high pressure fluid on a high pressure side to provide flow from the fluid source to a fluid destination via the primary fluid line. An interconnected valve system can be disposed in the primary fluid line configured to control flow through the primary fluid line.
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公开(公告)号：US11635097B1
公开(公告)日：2023-04-25
申请号：US17724682
申请日：2022-04-20
Applicant: Hamilton Sundstrand Corporation
Inventor： Morgan O'Rorke , Frank Perrelli
Abstract: Actuator systems and methods of operation are disclosed. The systems include a hydraulic actuator having a primary piston having a piston head arranged within a housing defining retract and extend chambers on opposite sides of the piston head. A control element is configured to control a supply of pressure to each of the retract and extend chambers. An actuator valve is coupled to the housing and includes a secondary piston that is biased into the retract chamber in an open flow state and when the primary piston is in a fully retracted state the piston head urges the secondary piston into a closed flow state. The actuator valve defines a flow chamber where, in an open flow state, fluid can be passed through the flow chamber and in a closed flow state the fluid is prevented from passing through the flow chamber.
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