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公开(公告)号：US20160238456A1
公开(公告)日：2016-08-18
申请号：US14621027
申请日：2015-02-12
Applicant: Rosemount Aerospace Inc.
Inventor： Scott Wigen
CPC classification number: G01K1/08 , G01K1/14 , G01K13/02 , G01K13/028 , H05K5/0213
Abstract: A method is disclosed for making an air temperature sensor comprises first generating a digital model of an air temperature sensor housing. The digital model is inputted into an additive manufacturing apparatus comprising an energy source. The additive manufacturing apparatus applies energy from the energy source to successively applied incremental quantities of a fusible material. The energy source fuses the successively applied incremental quantities of the fusible material to form incremental portions of the air temperature sensor housing that accrete together to form the air temperature sensor housing
Abstract translation: 公开了一种用于制造空气温度传感器的方法，该方法首先产生一个空气温度传感器壳体的数字模型。 数字模型被输入到包括能量源的添加剂制造装置中。 添加剂制造装置从能量源施加能量以连续施加增量的可熔材料。 能量源熔化连续施加的可熔材料的增量，以形成空气温度传感器壳体的增加部分，该空气温度传感器壳体累积在一起形成空气温度传感器壳体
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22.发明授权公开(公告)号：US12180852B2
公开(公告)日：2024-12-31
申请号：US18400123
申请日：2023-12-29
Applicant: Rosemount Aerospace Inc.
Inventor： Andrew Holl , Scott Wigen , Robert Edward Sable , Scott D. Isebrand , Brian Boyd
Abstract: A sensor includes a mount arranged along a sensor axis, an airfoil body fixed to the mount and having a first face and second face extending along the sensor axis, a heater element, and a temperature probe. The heater element and the temperature probe are positioned within the airfoil body and extend axially along the airfoil body. The airfoil body defines within its interior a pressure channel having an inlet segment extending between the heater element and the first face of the airfoil body to prevent ice formation and/or melt ice entrained within air traversing the pressure channel. Gas turbine engines, methods of removing ice or preventing ice formation, and methods of making sensors are also described.
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公开(公告)号：US11655726B2
公开(公告)日：2023-05-23
申请号：US16805486
申请日：2020-02-28
Applicant: Rosemount Aerospace Inc.
Inventor： Andrew Holl , Scott Wigen , Robert Edward Sable , Scott D. Isebrand , Brian Boyd
CPC classification number: F01D17/085 , F01D25/02 , G01K1/14 , G01K1/20 , G01K13/028 , F05D2270/303 , F05D2270/80 , G01L19/0092 , G01L19/0654 , G01L19/14
Abstract: A sensor includes an airfoil body, a heater element, and a temperature probe. The airfoil body defines a sensor axis, an insulating cavity, and extends between a leading edge and a trailing edge of the airfoil body. The heater element extends axially within the airfoil body and is positioned between the leading edge and the trailing edge of the airfoil body. The temperature probe extends axially within the airfoil body, is positioned between the heater element and the trailing edge of the airfoil body, and is separated from the heater element by the insulating cavity to limit thermal communication between the temperature probe and the heater element. Gas turbine engines, methods of making sensors, and methods of thermally separating temperature probes and heater elements in sensors are also described.
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公开(公告)号：US20220184895A1
公开(公告)日：2022-06-16
申请号：US17123766
申请日：2020-12-16
Applicant: Rosemount Aerospace Inc.
Inventor： Rudy Pitera , Scott Wigen , Alexander Bosworth
IPC: B29C64/393 , B29C64/153 , B29C64/232 , B29C64/268 , B33Y10/00 , B33Y30/00 , B33Y50/02
Abstract: A method and an electrical circuit for measuring the traverse speed of an additive manufacturing system energy source includes installing the electrical circuit within a region of the additive manufacturing system and translating the energy source along a first segment of a path within the region that intersects the electrical circuit. While the energy source traverses the path, the energy source modifies the electrical circuit causing a change in an electrical signal of the circuit sensed by a monitoring circuit. The traverse speed of the energy source is determined based on the change in the electrical signal and a geometry of the electrical circuit along the first segment.
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公开(公告)号：US20210270146A1
公开(公告)日：2021-09-02
申请号：US16805468
申请日：2020-02-28
Applicant: Rosemount Aerospace Inc.
Inventor： Andrew Holl , Scott Wigen , Scott D. Isebrand , Robert Edward Sable , Brian Boyd
Abstract: A sensor includes an airfoil body, a heater element, and a temperature probe. The airfoil body defines a sensor axis and having a leading edge, a trailing edge, and an ice accretion feature. The heater element extends axially through the airfoil body between the leading edge and the trailing edge of the airfoil body. The temperature probe extends axially through the airfoil body between the heater element and the trailing edge of the airfoil body. The heater element is axially overlapped by the ice accretion feature to accrete ice chordwise forward of a tip surface aperture. Gas turbine engines, methods of making sensors, and methods of accreting ice on sensors are also described.
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Patent Agency Ranking
公开(公告)号：US20210055143A1
公开(公告)日：2021-02-25
申请号：US16545591
申请日：2019-08-20
Applicant: Rosemount Aerospace Inc.
Inventor： Scott Wigen , Greg Allen Seidel , Ram Ranjan , Timothy Thomas Golly
Abstract: An air data probe includes an air data probe body and an additively manufactured heater on the air data probe body, the heater including a first heater layer and a first dielectric layer on the first heater layer. The first dielectric layer makes up an exterior surface of the heater.
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公开(公告)号：US20210053118A1
公开(公告)日：2021-02-25
申请号：US16545649
申请日：2019-08-20
Applicant: Rosemount Aerospace Inc.
Inventor： Scott Wigen , Rudy Pitera , Ryan P. Chou , Greg A. Seidel , Kent A. Ramthun
Abstract: An additive manufacturing apparatus including an energy source configured for transmitting a laser, a build plate configured to have a powder configured to be heated by the laser for additive manufacturing, at least one mirror positioned between the energy source and the build plate, the at least one mirror configured to direct the laser from the energy source to the build plate, and an optical isolator configured to reduce energy bounce back into the energy source.
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公开(公告)号：US20170241842A1
公开(公告)日：2017-08-24
申请号：US15588890
申请日：2017-05-08
Applicant: Rosemount Aerospace Inc.
Inventor： Matthew J. T. Gmach , Robert E. Sable , John T. Otto , Scott Wigen
CPC classification number: G01K1/22 , G01K13/00 , G01K13/028
Abstract: A temperature sensor includes a sensor body and a wedge extension. The sensor body extends from a sensor base to an opposed sensor tip along a longitudinal axis. The sensor body has a leading edge and opposed trailing edge. The sensor body also has an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage. The wedge extension is on the sensor body between the sensor tip and the sensor base on the leading edge of the sensor body.
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公开(公告)号：US11773745B2
公开(公告)日：2023-10-03
申请号：US16805468
申请日：2020-02-28
Applicant: Rosemount Aerospace Inc.
Inventor： Andrew Holl , Scott Wigen , Scott D. Isebrand , Robert Edward Sable , Brian Boyd
CPC classification number: F01D21/003 , F01D25/02 , G01K1/08 , G01K1/20 , G01K13/02 , B33Y80/00 , F05D2220/323 , F05D2220/3217
Abstract: A sensor includes an airfoil body, a heater element, and a temperature probe. The airfoil body defines a sensor axis and having a leading edge, a trailing edge, and an ice accretion feature. The heater element extends axially through the airfoil body between the leading edge and the trailing edge of the airfoil body. The temperature probe extends axially through the airfoil body between the heater element and the trailing edge of the airfoil body. The heater element is axially overlapped by the ice accretion feature to accrete ice chordwise forward of a tip surface aperture. Gas turbine engines, methods of making sensors, and methods of accreting ice on sensors are also described.
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公开(公告)号：US11662235B2
公开(公告)日：2023-05-30
申请号：US17492325
申请日：2021-10-01
Applicant: Rosemount Aerospace Inc.
Inventor： Scott D. Isebrand , Greg Allen Seidel , Scott Wigen
Abstract: A probe head of an air data probe includes a body extending from a first end to a second end of the probe head and a rod heater. The body includes an inlet adjacent the first end of the probe head, an air passageway extending through the body from the inlet to a second end of the probe head, a water dam extending radially through the body such that the air passageway is redirected around the water dam, a heater bore extending within the body, and an enhanced conduction area between heater bore and an exterior surface of the probe head. The inlet, the air passageway, the water dam, and the heater bore are all unitary to the body. The rod heater is positioned within the heater bore.
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