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公开(公告)号：US20240270374A1
公开(公告)日：2024-08-15
申请号：US18432687
申请日：2024-02-05
申请人： Goodrich Corporation
发明人： Kamil Mateusz Babicki , Marcin Szymon Sokolowski , BARTLOMIEJ Kamil Zuk , Karol Stras , Andrzej Pawel Chwalek , Piotr Kielczykowski , Nicholas Edward Scaggs , Scottie G. Whittle
IPC分类号： B64C25/36 , B64C25/42 , F16D65/78 , F16D65/847
CPC分类号： B64C25/36 , B64C25/42 , F16D65/847 , F16D2065/785
摘要： A heat shield assembly comprising a sheet of flexible heat shield material and one or more hook and loop fasteners comprising a first part attached to the sheet of flexible heat shield material and a second part configured to be attached to a structure to which, in use, the sheet of flexible heat shield material is to be attached, one of the first and second parts having a plurality of hooks and the other of the first and second part having a plurality of loops such that when the sheet of flexible heat shield material is brought into engagement with the structure, the hooks and loops mesh to secure the sheet of heat shield material to the structure.
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公开(公告)号：US12017487B2
公开(公告)日：2024-06-25
申请号：US17116908
申请日：2020-12-09
申请人： GOODRICH CORPORATION
CPC分类号： B60C23/18 , B64C25/36 , B64C25/42 , F16D65/78 , B60B2900/513
摘要： A retainer assembly may comprise: a retainer main body having a first mounting flange, a second mounting flange, a body portion, a first rib and a second rib, the body portion extending from the first mounting flange to the second mounting flange, the first rib extending from the second mounting flange towards the first mounting flange, the second rib extending from the second mounting flange towards the first mounting flange, the first rib and the second rib extending orthogonal to the body portion; and a retainer sleeve having a first slot extending from the first axial end towards the second axial end and a second slot extending from the first axial end towards the second axial end, a portion of the first rib disposed in the first slot, and a portion of the second rib disposed in the second slot.
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公开(公告)号：US11897603B1
公开(公告)日：2024-02-13
申请号：US18196288
申请日：2023-05-11
IPC分类号： B64C25/66 , B64C37/00 , B60F5/02 , B64C11/00 , B64C25/32 , F04D29/52 , F01D15/00 , F04D29/32 , B64C25/36
CPC分类号： B64C25/66 , B60F5/02 , B64C11/001 , B64C25/36 , B64C25/405 , B64C37/00 , F04D29/526 , B60F2301/04 , F01D15/00 , F04D29/326
摘要： A convertible ducted fan engine and mounting system. The convertible ducted fan engine has a shroud encircling a mechanical fan. The convertible ducted fan engine includes a fluid-propulsion configuration in which the mechanical fan rotates freely with respect to the shroud to produce thrust through fluid flow, and a drive-wheel configuration in which the shroud rotates about the rotational axis.
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公开(公告)号：US11845540B2
公开(公告)日：2023-12-19
申请号：US17505731
申请日：2021-10-20
发明人： Michael Robertson
CPC分类号： B64C25/36 , B60C23/00318 , B60C23/0474 , B60C23/20 , G01K13/00 , G01L17/00 , B60C2200/02
摘要： An apparatus for determining tire pressure of an aircraft tire. The apparatus includes a processing system configured to: obtain a first set and a second set of tire measurement data for an aircraft, wherein the first set is from a start of a flight cycle and the second set is from a time before the first set; and determine a steady state tire pressure based on the first and second sets of measurement data.
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公开(公告)号：US20230348056A1
公开(公告)日：2023-11-02
申请号：US17732938
申请日：2022-04-29
申请人： Sandor Mark Langer
发明人： Sandor Mark Langer
IPC分类号： B64C9/02 , B64C1/14 , B60L50/60 , B64C39/02 , B64D27/26 , B64C25/36 , B64D27/24 , B64D9/00 , B64C37/02
CPC分类号： B64C39/024 , B60L50/66 , B64C1/1415 , B64C9/02 , B64C25/36 , B64C37/02 , B64D9/003 , B64D27/24 , B64D27/26 , B64C29/0008 , B64C2201/042 , B64C2201/108 , B64C2201/128
摘要： An unmanned aerial vehicle (UAV) has a wing assembly that is coupled to a cargo carrying pod. The pod has a pallet storage volume and an aerodynamic outer surface. The wing assembly has wings that are coupled to rotor booms that include motors and rotors. A tail assembly is coupled to tail booms that extend back from the wings. Rudders are coupled to the rear portions of the tail booms and an elevator is coupled to top portions of the rudders. The elevator is at least 84 inches high and the rudders are at least 48 apart so that a forklift can drive under the elevator and between the rudders to a rear door of the pod to place cargo on a pallet into the storage area of the pod.
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公开(公告)号：US20230312087A1
公开(公告)日：2023-10-05
申请号：US18128808
申请日：2023-03-30
发明人： Fraser WILSON
CPC分类号： B64C25/36 , B64C25/50 , B64C25/405 , B60T8/1703 , B60L7/10 , B60T2270/60 , B60T2260/02
摘要： An aircraft nose landing gear assembly is disclosed including two wheels, motors, brakes, and a controller. The wheels are separated by a steering axis and independently rotatable about a rotation axis in a rotation direction. The motors and brakes are each arranged to selectively engage a respective wheel. The motors and brakes supplement and resist rotation of the respective wheel in the rotation direction, respectively. On the basis of an indication to the controller of rotation of the two wheels in the rotation direction, the controller is arranged to: cause one motor to engage its respective wheel and supplement rotation, and cause the brake associated with the other wheel to engage the other wheel and resist rotation. Engagement of the motor and brake causes the wheels to pivot about the steering axis during a turning event.
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公开(公告)号：US11585387B2
公开(公告)日：2023-02-21
申请号：US16799392
申请日：2020-02-24
发明人： Bradley E. Fish
摘要： In some examples, an assembly includes a rotor drive key configured to be positioned over a wheel boss defined by a wheel. A drive key body defines a trough configured to receive the wheel boss. An inner surface of the drive key body is configured to establish a conforming contact with an outer profile of the wheel boss and oppose relative motion of the rotor drive key in a radial direction of the wheel. The rotor drive key includes a tab having a tab aperture configured to receive a fastener extending in an axial direction of the wheel and engaging the wheel boss.
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公开(公告)号：US20230047751A1
公开(公告)日：2023-02-16
申请号：US16996253
申请日：2020-08-18
申请人： David Hoady Spencer
发明人： David Hoady Spencer
IPC分类号： B64C25/36 , F16D65/847 , B60B27/00 , B64C25/42
摘要： A detachable airplane wheel prerotation/landing brake cooling device is disclosed that comprises: an outer circular cage rim, an inner circular cage rim confronting and spaced apart from the outer circular cage rim, and a plurality of spaced apart arcuate blades spanning across and connecting the outer circular cage rim to the inner circular cage rim at a slant. Each arcuate blade includes a first section connected to the outer circular cage rim and a second section connected to inner circular cage rim. The plurality of slanted arcuate blades are, when the detachable airplane wheel prerotation/landing brake cooling device is being impinged by an airstream during the landing of the airplane, configured to (i) rotate the wheel about the axle in a forward direction, and (ii) funnel air into the plurality of annular spaces adjacent to the plurality of heat shields to thereby remove heat away from the disc brake assembly.
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公开(公告)号：US11472498B2
公开(公告)日：2022-10-18
申请号：US16689864
申请日：2019-11-20
发明人： Fadl Abdellatif , Jeff S. Shamma
IPC分类号： B64C39/02 , B62D57/024 , B60K1/02 , B62D21/09 , B60G3/01 , B60G11/00 , B62D61/12 , B60R11/00 , G01N29/265 , G01N29/04 , B62D9/00 , B64C25/24 , B64C25/36 , B64C25/40 , B64D1/02 , G01B17/02 , G05D1/00 , G05D1/10 , B64C25/32 , G06T7/50 , G01S17/86 , G01S17/89 , H04N5/222 , G06V20/10
摘要： An unmanned aerial vehicle (UAV) includes a body constructed to enable the UAV to fly and three or more legs connected to the body and configured to land and perch the UAV on a curved ferromagnetic surface. Each leg includes a first portion connected to the body, a second portion including a magnet and configured to magnetically attach and maintain the magnetic attachment of the leg to the ferromagnetic surface during the landing and perching, and a passive articulation joint connecting the first and second portions and configured to passively articulate the second portion with respect to the first portion in response to the second portion approaching the ferromagnetic surface. The UAV further includes a releasable crawler including magnetic wheels which detach the crawler from the body during the perching and maneuver the crawler on the ferromagnetic surface while magnetically attaching the crawler to the ferromagnetic surface after detachment.
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公开(公告)号：US11440646B2
公开(公告)日：2022-09-13
申请号：US16772484
申请日：2018-11-06
发明人： Hayato Toda , Seigo Hata
摘要： A remaining tire tread depth management system includes a remaining tire tread depth measurement device configured to measure a remaining tread depth of at least one of aircraft tires mounted on an aircraft, a tire wear amount estimation device configured to estimate a wear amount of all of the aircraft tires mounted on the aircraft including the aircraft tires, and a tire management server configured to estimate a remaining tread depth and a number of available flight times of all of the aircraft tires in accordance with measurement data output from the remaining tire tread depth measurement device and estimation data output from the tire wear amount estimation device.
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