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1. 发明授权

US09772345B2 Corrision-resistant heated air data probe 有权
公开(公告)号：US09772345B2
公开(公告)日：2017-09-26
申请号：US15045907
申请日：2016-02-17
申请人： ROSEMOUNT AEROSPACE, INC.
发明人： Timothy Thomas Golly , Matthew P. Anderson , Paul Robert Johnson , Greg Seidel
IPC分类号： G01F1/46 , G01P5/165 , G01P1/02 , G01P13/02
CPC分类号： G01P5/165 , G01F1/46 , G01P1/026 , G01P13/025
摘要： An air data probe is disclosed. The air data probe may include a probe body having an interior cavity and coated by a protective shell. A sensing port may be disposed in the air data probe and may extend through the probe body. The sensing port may also be lined by the protective shell. The protective shell may be made of an austenitic nickel-chromium alloy, or stainless steel, or any relatively corrosion resistant material. The probe body may be made of nickel, or a nickel alloy, or any relatively thermally conductive material. The protective shell may be joined to the probe body by additive manufacturing, such as laser cladding. In this manner, an air data probe capable withstanding high temperatures without corrosion and yet also being relatively thermally conductive is disclosed.

2. 发明授权

US10227139B2 Heated air data probes 有权
公开(公告)号：US10227139B2
公开(公告)日：2019-03-12
申请号：US15067650
申请日：2016-03-11
申请人： Rosemount Aerospace Inc.
发明人： Timothy T. Golly , Paul R. Johnson , Greg Seidel
IPC分类号： G01L19/00 , G01L19/04 , G01P5/165 , B64D43/02 , G01P13/02 , B65H54/10
摘要： An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. The probe includes a thermocouple having a sense end in the forward tip to measure the temperature in the forward tip. The probe includes a port opening defined in a side of the probe head and opening at an angle with respect to the longitudinal axis. The probe includes a bulkhead within the probe head. The bulkhead has a chamber in fluid communication with the port opening. The chamber includes a single chamber inlet having an elongated cross-sectional shape. The single elongated chamber inlet is in fluid communication with two downstream pressure conduits to provide redundancy in case one of the two pressure conduits is blocked.

3. 发明申请

US20180238723A1 METHOD OF FORMING AN ICE RESISTANT PITOT TUBE 审中-公开
公开(公告)号：US20180238723A1
公开(公告)日：2018-08-23
申请号：US15957234
申请日：2018-04-19
申请人： Rosemount Aerospace Inc.
发明人： Greg Seidel , Timothy Thomas Golly , Paul Robert Johnson
IPC分类号： G01F1/46 , G01P5/165
CPC分类号： G01F1/46 , G01P5/165
摘要： A method of forming a pitot tube includes forming a substantially cylindrical body portion including an outer surface, a tip portion having an inlet opening and an interior defining a flow passage, radially tapering the outer surface from the body portion toward the inlet opening, and disposing at least one electrical coil including one or more coil wraps along the flow passage of the pitot tube.

4. 发明授权

US10024877B2 Corrosion-resistant heated air data probe methods 有权
公开(公告)号：US10024877B2
公开(公告)日：2018-07-17
申请号：US15681651
申请日：2017-08-21
申请人： Rosemount Aerospace, Inc.
发明人： Timothy Thomas Golly , Matthew P. Anderson , Paul Robert Johnson , Greg Seidel
IPC分类号： B23P17/04 , G01P5/165 , G01F1/46 , G01P1/02 , G01P13/02
摘要： A method of making an air data probe may comprise forming a probe body, forming an interior cavity into the probe body, applying a protective shell to the probe body by an additive manufacturing technique, inserting a heating element into the interior cavity, machining a final profile of the air data probe, and forming a sensing port comprising a port passage defined through the probe body and lined by a portion of the protective shell.

5. 发明申请

US20160291051A1 CORRISION-RESISTANT HEATED AIR DATA PROBE 有权
标题翻译：耐腐蚀加热空气数据探头
公开(公告)号：US20160291051A1
公开(公告)日：2016-10-06
申请号：US15045907
申请日：2016-02-17
申请人： ROSEMOUNT AEROSPACE, INC.
发明人： Timothy Thomas Golly , Matthew P. Anderson , Paul Robert Johnson , Greg Seidel
IPC分类号： G01P5/165
CPC分类号： G01P5/165 , G01F1/46 , G01P1/026 , G01P13/025
摘要： An air data probe is disclosed. The air data probe may include a probe body having an interior cavity and coated by a protective shell. A sensing port may be disposed in the air data probe and may extend through the probe body. The sensing port may also be lined by the protective shell. The protective shell may be made of an austenitic nickel-chromium alloy, or stainless steel, or any relatively corrosion resistant material. The probe body may be made of nickel, or a nickel alloy, or any relatively thermally conductive material. The protective shell may be joined to the probe body by additive manufacturing, such as laser cladding. In this manner, an air data probe capable withstanding high temperatures without corrosion and yet also being relatively thermally conductive is disclosed.
摘要翻译：公开了一种空气数据探测器。空气数据探测器可以包括具有内部空腔并由保护壳涂覆的探针主体。感测端口可以设置在空气数据探头中并且可以延伸穿过探针主体。感测端口也可以由保护外壳衬里。保护壳可以由奥氏体镍铬合金或不锈钢或任何相对耐腐蚀的材料制成。探针体可以由镍或镍合金或任何相对导热的材料制成。保护壳可以通过添加剂制造（例如激光熔覆）与探针体接合。以这种方式，公开了能够耐受高温而没有腐蚀并且还具有相对导热性的空气数据探测器。

6. 发明申请

US20160282158A1 Air Data Probe With Improved Performance at Angle of Attack Operation 审中-公开
标题翻译：空中数据探测器具有改进的攻击角度的性能
公开(公告)号：US20160282158A1
公开(公告)日：2016-09-29
申请号：US14665007
申请日：2015-03-23
申请人： Rosemount Aerospace, Inc.
发明人： Paul Robert Johnson , Aaron A. Cusher , Timothy Thomas Golly , Brian Daniel Matheis , Greg Seidel
IPC分类号： G01F1/46 , B64D45/00
CPC分类号： G01F1/46 , B64D45/00 , G01P5/165
摘要： An air data probe has a pitot tube with a tap at a forward end that defines an inner flow path. The inner flow path decreases in the cross-sectional area until reaching a throat. The inner flow path has cross-sections that are generally cylindrical and also has sections of removed material. Other embodiment have unique shapes.
摘要翻译：空气数据探头具有皮托管，其在前端具有限定内部流动路径的水龙头。内部流路在横截面积减小直到达到喉部。内部流动路径具有大致圆柱形的横截面并且还具有被去除的材料的部分。其他实施例具有独特的形状。

7. 发明申请

US20140116154A1 ICE RESISTANT PITOT TUBE 有权
标题翻译：耐寒铅管
公开(公告)号：US20140116154A1
公开(公告)日：2014-05-01
申请号：US14065878
申请日：2013-10-29
申请人： Rosemount Aerospace Inc.
发明人： Greg Seidel , Timothy Thomas Golly , Paul Robert Johnson
IPC分类号： G01P5/165
CPC分类号： G01F1/46 , G01P5/165
摘要： A pitot tube includes a substantially cylindrical body portion and a tip portion extending along a pitot tube axis from the body portion. The tip portion includes an inlet opening and a radially tapering outer surface extending from the body portion toward the inlet opening. Another pitot tube includes a substantially cylindrical body portion and a tip portion extending along a pitot tube axis from the body portion. The tip portion includes an inlet opening. One or more electrical coils including one or more coil wraps are located at an interior of the pitot tube. One or more bulkeads are located between a forwardmost coil wrap and a drainage feature to limit travel of particles ingested into the interior.
摘要翻译：皮托管包括基本上圆柱形的主体部分和沿皮托管轴线从主体部分延伸的尖端部分。尖端部分包括从主体部分朝向入口开口延伸的入口和径向渐缩的外表面。另一皮托管包括基本上圆柱形的本体部分和从皮托管轴线从主体部分延伸的尖端部分。尖端部分包括入口开口。包括一个或多个线圈圈的一个或多个电线圈位于皮托管的内部。一个或多个保险杠位于最前面的线圈包裹物和排水特征之间，以限制摄入到内部的颗粒的行进。

8. 发明申请

US20210172973A1 HYBRID MATERIAL AIRCRAFT SENSORS AND METHOD OF MANUFACTURING 有权
公开(公告)号：US20210172973A1
公开(公告)日：2021-06-10
申请号：US17178331
申请日：2021-02-18
申请人： Rosemount Aerospace Inc.
发明人： Robin Jacob , Guru Prasad Mahapatra , Paul Robert Johnson , Greg Seidel
IPC分类号： G01P5/165 , G01F1/46 , G01K13/02 , G01P1/02 , G01P13/02 , B22F10/20
摘要： An air data probe includes a probe body including a probe wall. The probe body is formed from a first material by direct energy metal deposition. An insert is positioned in the probe wall. The insert is formed from a second material different from the first material. The insert is encapsulated in the probe wall via the direct energy metal deposition. A method of forming an air data probe includes forming one or more thermally conductive inserts, and encapsulating the one or more inserts into a wall of an air data probe via direct energy metal deposition. The air data probe is formed from a first material and the one or more inserts are formed from a second material different from the first material.

9. 发明申请

US20200333206A1 CORROSION RESISTANT SLEEVE FOR AN AIR DATA PROBE 审中-公开
公开(公告)号：US20200333206A1
公开(公告)日：2020-10-22
申请号：US16918224
申请日：2020-07-01
申请人： Rosemount Aerospace Inc.
发明人： Timothy Thomas Golly , Paul Robert Johnson , Greg Seidel
IPC分类号： G01L19/06 , G01L13/00 , B64D47/00
摘要： A corrosion resistant apparatus for an air data probe with a sleeve being cylindrical in shape with a first end and a second end, at least one circumferentially extending groove on an outside of the sleeve configured to accommodate coils of a heater, and a bore at a center of the sleeve and extending between the first end and the second end configured to provide a pneumatic pathway that allows atmospheric conditions to reach measurement equipment of the air data probe.

10. 发明申请

US20200216191A1 AIR DATA PROBES 审中-公开
公开(公告)号：US20200216191A1
公开(公告)日：2020-07-09
申请号：US16818998
申请日：2020-03-13
申请人： Rosemount Aerospace Inc.
发明人： Timothy T. Golly , Paul R. Johnson , Greg Seidel
IPC分类号： B64D43/02 , G01L19/04 , G01L19/00 , B65H54/10 , G01P13/02 , G01P5/165
摘要： An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. A port opening is defined in a side of the probe head and opening at an angle with respect to the longitudinal axis. A bulkhead within the probe head has a chamber in fluid communication with the port opening. The chamber includes a single chamber inlet having an elongated cross-sectional shape. The single elongated chamber inlet is in fluid communication with two downstream pressure conduits to provide redundancy in case one of the two pressure conduits is blocked.

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