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公开(公告)号:US3829950A
公开(公告)日:1974-08-20
申请号:US34783273
申请日:1973-04-04
申请人: GOODRICH CO B F
发明人: KUTS M
CPC分类号: H05B3/16 , B64D15/12 , B64D15/14 , Y10T29/53174 , Y10T29/53261 , Y10T29/53348
摘要: An apparatus for the fabricating of deicers wherein a plurality of alternating slides are selectively moved by cams so that a wire extending longitudinally therethrough is wound back and forth in an alternating pattern as the slides move off the cams. Slip clutches are employed to move the respective slides in sequential order.
摘要翻译: 一种用于制造除冰器的装置,其中多个交替的滑块通过凸轮选择性地移动,使得当滑块从凸轮移动时,纵向延伸穿过的线以交替的方式前后旋转。 采用滑动离合器依次顺序移动各个滑块。
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公开(公告)号:US3453415A
公开(公告)日:1969-07-01
申请号:US3453415D
申请日:1967-04-27
申请人: LICENTIA GMBH
发明人: HERMES HEINZ , VOLKNER WOLFGANG
CPC分类号: B64D15/14
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公开(公告)号:US2686640A
公开(公告)日:1954-08-17
申请号:US22096051
申请日:1951-04-13
申请人: NEEL JR CARR B , BERGRUN NORMAN R
发明人: NEEL JR CARR B , BERGRUN NORMAN R
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公开(公告)号:US2638295A
公开(公告)日:1953-05-12
申请号:US74256247
申请日:1947-04-19
申请人: CURTISS WRIGHT CORP
发明人: SHEETS JACK H
IPC分类号: B64D15/14
CPC分类号: B64D15/14
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公开(公告)号:US2625661A
公开(公告)日:1953-01-13
申请号:US16364950
申请日:1950-05-23
申请人: PHILIPS LAB INC
发明人: HAYDON ARTHUR W
CPC分类号: B64D15/12 , B64D15/14 , Y10T307/484 , Y10T307/76
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76.
公开(公告)号:US12037122B2
公开(公告)日:2024-07-16
申请号:US17713912
申请日:2022-04-05
申请人: GOODRICH CORPORATION
发明人: Brandon Hein , Casey M. Slane , Galdemir C. Botura
摘要: An aircraft wing may comprise an airfoil having deicing zone, an anti-icing zone, and an ice runback control zone. An aircraft wing may comprise an electro-thermal ice protection system disposed in the aircraft wing. The electro-thermal ice protection system may be disposed along the deicing, anti-icing, and ice runback control zones of the airfoil to improve aerodynamic performance of the aircraft and reduce ice formation along the wings of the aircraft.
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公开(公告)号:US20240217664A1
公开(公告)日:2024-07-04
申请号:US18601353
申请日:2024-03-11
申请人: Goodrich Corporation
摘要: An electrothermal ice protection system (IPS) installed on an aircraft includes a sensor, a parting strip assembly, and a controller. The sensor monitors a direction of a local incident airflow that is imparted on the sensor. The parting strip assembly is coupled to the critical surface and includes a plurality of heating sections. The controller is in signal communication with the sensor and the parting strip assembly. The controller determines a direction of surface airflow incident on a critical surface of the aircraft based on the local incident airflow and selectively concentrates power to at least one targeted heating section among the plurality of heating sections with respect to non-targeted heating sections among the plurality of heating sections based on the direction of the surface airflow.
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78.
公开(公告)号:US20230312111A1
公开(公告)日:2023-10-05
申请号:US17713912
申请日:2022-04-05
申请人: GOODRICH CORPORATION
发明人: BRANDON HEIN , CASEY M. SLANE , GALDEMIR C. BOTURA
摘要: An aircraft wing may comprise an airfoil having deicing zone, an anti-icing zone, and an ice runback control zone. An aircraft wing may comprise an electro-thermal ice protection system disposed in the aircraft wing. The electro-thermal ice protection system may be disposed along the deicing, anti-icing, and ice runback control zones of the airfoil to improve aerodynamic performance of the aircraft and reduce ice formation along the wings of the aircraft.
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公开(公告)号:US11198513B1
公开(公告)日:2021-12-14
申请号:US16384284
申请日:2019-04-15
发明人: Michael Milardo , Igor Giterman
摘要: An anti-icing/de-icing system for an airfoil structure having multiple layers is provided and includes a thermal article, wherein the thermal article is embedded within the airfoil structure to be located between the multiple layers. The thermal article includes a first terminal end, a second terminal end and a thermal expanded mesh material which connects the first terminal end with the second terminal end, and wherein the thermal expanded mesh material is configured to have at least one predetermined resistance between the first terminal end and the second terminal end.
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公开(公告)号:US11181545B2
公开(公告)日:2021-11-23
申请号:US15824589
申请日:2017-11-28
发明人: Alexander N. Reid , Richard Alan Schwartz , William B. Krueger , Timothy DeAngelo , Kenneth Freeman
摘要: An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a heated chassis defining a pocket and a mounting plate positioned adjacent the heated chassis and having an opening. The vane assembly has a portion that is positioned in the pocket of the heated chassis and extends through the opening of the mounting plate.
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