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公开(公告)号：US20230160640A1
公开(公告)日：2023-05-25
申请号：US17534028
申请日：2021-11-23
Applicant: Delavan Inc.
Inventor： Jason Ryon , Raffi O. Mangoyan , David Saltzman , Michael Doe
CPC classification number: F28D7/103 , F28F1/22 , F28F7/02 , F28F9/18 , F28F2275/04 , F28F2275/127
Abstract: A heat exchanger assembly includes a first member defining fluid passages therein for a first heat exchanger fluid. A second member defines fluid passages therein for a second heat exchanger fluid. The second member is engaged to the second member with an interference fit. A method of assembling a heat exchanger includes thermally resizing at least one of a first heat exchanger member and a second heat exchanger member and assembling the second heat exchanger member to the first heat exchanger member. The method includes thermally equalizing the first and second heat exchanger members to engage the second heat exchanger member to the first heat exchanger member with an interference fit.
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公开(公告)号：US20230099661A1
公开(公告)日：2023-03-30
申请号：US17484857
申请日：2021-09-24
Applicant: Delavan Inc.
Inventor： Jason Ryon , Jacob Greenfield , Adrian L. Stoicescu
IPC: F04D29/32
Abstract: A method of making an impeller includes building the impeller in a layer by layer process in a build direction along the rotational axis starting from a base of the hub. The plurality of blades includes a plurality of perforated blades that support the shroud during additively manufacturing the impeller. The method can include installing the impeller in a fuel pump, air compressor, or the like, without removing the perforated blades from the impeller.
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公开(公告)号：US11608783B2
公开(公告)日：2023-03-21
申请号：US17089254
申请日：2020-11-04
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev Alexander Prociw
IPC: F02C7/264
Abstract: An embodiment of a torch igniter for a combustor of a gas turbine engine includes a combustion chamber oriented about an axis, a cap defining an axially upstream end of the combustion chamber, a tip defining the axially downstream end of the combustion chamber, an igniter wall extending from the cap to the tip and defining a radial extent of the combustion chamber, a structural wall coaxial with and surrounding the igniter wall, an outlet passage defined by the igniter wall within the tip, a glow plug housing configured to receive a glow plug and allow an innermost end of the glow plug to extend into the combustion chamber, and a cooling system. The cooling system includes an air inlet formed within an exterior of the structural wall, a cooling channel forming a flow path through the structural wall at the glow plug housing, and an air passage.
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公开(公告)号：US20230061595A1
公开(公告)日：2023-03-02
申请号：US17460823
申请日：2021-08-30
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev A. Prociw
Abstract: A torch ignitor system includes a torch wall defining a combustion chamber therein with a flame outlet passing out of the torch wall downstream of the combustion chamber. A fuel nozzle is mounted to the torch wall to issue fuel into the combustion chamber. An ignitor is mounted to the torch wall, extending into the combustion chamber to ignite fuel issued from the fuel nozzle. A cooling passage is in thermal communication with the ignitor for cooling the ignitor with fluid passing through the cooling passage.
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公开(公告)号：US11566565B2
公开(公告)日：2023-01-31
申请号：US17133303
申请日：2020-12-23
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev A. Prociw , Brandon Phillip Williams
IPC: F02C7/264
Abstract: An embodiment of an ignition system for a gas turbine engine includes a high pressure engine case, a torch ignitor disposed at least partially within the high pressure engine case, the torch ignitor having a combustion chamber oriented about a torch axis, the combustion chamber having axially upstream and downstream ends defining a flow direction through the combustion chamber, along the axis. The ignition system also includes an access hatch configured to allow access through a high pressure engine case to the cap and to seal against the high pressure engine case when not accessing the cap. An embodiment of a method includes removing a hatch from a high pressure engine case to open a hatch opening, performing maintenance on a torch ignitor that is inside the high pressure engine case by accessing the torch ignitor through the hatch opening, replacing the hatch to close the hatch opening after completion of maintenance on the torch ignitor.
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Patent Agency Ranking
公开(公告)号：US11549441B1
公开(公告)日：2023-01-10
申请号：US17499484
申请日：2021-10-12
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev A. Prociw , Brandon Phillip Williams
Abstract: A fuel injector includes a fuel nozzle configured to issue a spray of fuel from a fuel outlet in a downstream direction along an injection axis. The fuel nozzle defines a main flow passage therethrough. An injection fuel line is in fluid communication with the fuel nozzle to supply fuel to the fuel nozzle. A torch ignitor has a flame outlet opening into the main flow passage of the fuel nozzle for issuing flame into the main flow passage.
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97.发明授权公开(公告)号：US11486309B2
公开(公告)日：2022-11-01
申请号：US17125083
申请日：2020-12-17
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev Alexander Prociw , Brandon P. Williams
Abstract: An embodiment of a combustor for a gas turbine engine includes a combustor case, a combustor liner disposed within the combustor case, a fuel nozzle at an upstream end of the combustor liner, a torch igniter at least partially within the combustor case, and a removable surface igniter. The torch igniter includes a combustion chamber, a cap configured to receive a fuel injector, a tip, an annular igniter wall extending from the cap to the tip and defining a radial extent of the combustion chamber, an aperture, a structural wall coaxial with and surrounding the igniter wall, and an outlet passage within the tip which fluidly connects the combustion chamber to the combustor. The torch igniter is configured to receive the removable surface igniter through the aperture. An internal end of the removable surface igniter extends through the aperture into the combustion chamber of the torch igniter.
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公开(公告)号：US11415059B2
公开(公告)日：2022-08-16
申请号：US17133216
申请日：2020-12-23
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev A. Prociw , Brandon Phillip Williams
Abstract: A torch ignitor system for a combustor of a gas turbine engine includes a torch ignitor, the torch ignitor including a combustion chamber oriented about a torch axis, the combustion chamber having axially upstream and downstream ends defining a flow direction through the combustion chamber, along the axis. The torch ignitor includes a cap defining the axially upstream end of the combustion chamber and oriented about the axis, wherein the cap is configured to receive a fuel injector and at least one glow plug. The torch ignitor includes an elbow connected to the downstream end of the combustion chamber for diverting combustion products along an ignition jet flame axis that is off of the torch axis for injection of combustion products into a gas turbine engine combustor. The torch ignitor further includes a tip at a downstream end of the elbow for issuing the injection of combustion products.
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公开(公告)号：US20220243916A1
公开(公告)日：2022-08-04
申请号：US17533682
申请日：2021-11-23
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev Alexander Prociw
Abstract: A fuel injector system for a torch igniter includes an injector body centered on an axis, a receiving aperture formed in a cap of the torch igniter, an injector aperture, an air channel, a fuel channel, and a purge passage formed in a housing of the torch igniter and fluidly connected to a cooling air source. The injector body includes an axial wall at a first axial end of the injector body, an outer wall connected to the axial wall and extending along the axis transverse to the first wall, and an inner portion connected to the axial wall and extending along the axis transverse to the axial wall. An outer surface of the inner portion is spaced a distance from an inner surface of the outer wall, forming an insulating space between the outer wall and the inner portion.
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公开(公告)号：US20220195939A1
公开(公告)日：2022-06-23
申请号：US17133216
申请日：2020-12-23
Applicant: Delavan Inc.
Inventor： Jason Ryon , Lev A. Prociw , Brandon Phillip Williams
Abstract: A torch ignitor system for a combustor of a gas turbine engine includes a torch ignitor, the torch ignitor including a combustion chamber oriented about a torch axis, the combustion chamber having axially upstream and downstream ends defining a flow direction through the combustion chamber, along the axis. The torch ignitor includes a cap defining the axially upstream end of the combustion chamber and oriented about the axis, wherein the cap is configured to receive a fuel injector and at least one glow plug. The torch ignitor includes an elbow connected to the downstream end of the combustion chamber for diverting combustion products along an ignition jet flame axis that is off of the torch axis for injection of combustion products into a gas turbine engine combustor. The torch ignitor further includes a tip at a downstream end of the elbow for issuing the injection of combustion products.
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