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公开(公告)号：US20190106203A1
公开(公告)日：2019-04-11
申请号：US15728989
申请日：2017-10-10
摘要： One example of a mount for a rotorcraft comprises a structural support member, a bracket, and an elastomer. The bracket is configured to attach to a component of the rotorcraft. The component of the rotorcraft produces vibrations at a first frequency. The structural support member configured to transfer a weight of the component of a rotorcraft to an airframe of the rotorcraft. A rotor system of the aircraft vibrates the airframe of the rotorcraft at a second frequency. The elastomer is located between a structural support member and a bracket. The elastomer is configured to attenuate noise caused by the vibrations at the first frequency by isolating the vibrations at the first frequency from reaching the airframe of the rotorcraft while the airframe vibrates at the second frequency.
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公开(公告)号：US11167842B2
公开(公告)日：2021-11-09
申请号：US15728989
申请日：2017-10-10
摘要： One example of a mount for a rotorcraft comprises a structural support member, a bracket, and an elastomer. The bracket is configured to attach to a component of the rotorcraft. The component of the rotorcraft produces vibrations at a first frequency. The structural support member configured to transfer a weight of the component of a rotorcraft to an airframe of the rotorcraft. A rotor system of the aircraft vibrates the airframe of the rotorcraft at a second frequency. The elastomer is located between a structural support member and a bracket. The elastomer is configured to attenuate noise caused by the vibrations at the first frequency by isolating the vibrations at the first frequency from reaching the airframe of the rotorcraft while the airframe vibrates at the second frequency.
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公开(公告)号：US20180087561A1
公开(公告)日：2018-03-29
申请号：US15702958
申请日：2017-09-13
CPC分类号： F16C3/16 , B64C27/12 , B64C27/14 , B64C27/82 , B64D35/00 , B64D45/00 , B64D2045/009 , F16C3/02 , F16C3/026 , F16C2326/06 , F16C2326/43 , F16H57/0416
摘要： The present invention includes a thermal management system and method including: a drive shaft; one or more fans or impellers in fluid communication with at least a portion of the drive shaft; and one or more air management baffles configured to direct air flow between the impeller and the portion of the drive shaft. In one embodiment, the system and method further includes insulation positioned about the at least a portion of the drive shaft.
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公开(公告)号：US11255373B2
公开(公告)日：2022-02-22
申请号：US15702958
申请日：2017-09-13
摘要： A thermal management system and method includes: a drive shaft; one or more fans or impellers in fluid communication with at least a portion of the drive shaft; and one or more air management baffles configured to direct air flow between the impeller and the portion of the drive shaft. In one embodiment, the system and method further includes insulation positioned about the at least a portion of the drive shaft.
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公开(公告)号：US11028944B2
公开(公告)日：2021-06-08
申请号：US15994518
申请日：2018-05-31
发明人： Brent Scannell , Thomas Mast , Jon Damon Bennett , Joshua Allan Edler , Jean Pierre Paradis , Keith C. Pedersen
摘要： One example of a duct support for a rotorcraft includes a stabilizing mechanism configured to transfer a weight of a duct to an airframe of the rotorcraft, where the duct undergoes thermal expansion. The stabilizing mechanism includes a first stabilizing member attached to the duct, a second stabilizing member attached to the rotorcraft, and a coupling mechanism where the coupling mechanism is configured to couple the first stabilizing member to the second stabilizing member and accommodate thermal expansion of the duct by allowing for movement of the first stabilizing member relative to the second stabilizing member. In an example, the duct is an exhaust duct of an engine of the rotorcraft and heat from the engine cause the exhaust duct to undergo the thermal expansion.
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公开(公告)号：US10752332B2
公开(公告)日：2020-08-25
申请号：US15665627
申请日：2017-08-01
IPC分类号： B64D29/00 , B64D29/02 , B64D29/04 , B64D29/08 , B64C7/00 , B64C7/02 , B64C1/38 , B64C1/14 , B64D29/06 , B64C27/04 , B64C1/06
摘要： One example of a fairing for a rotorcraft includes an outer mold line portion (OML portion) and a bearing portion extending from the OML portion. The OML portion provides at least a portion of an outer mold line of the rotorcraft. Both the OML portion and the bearing portion shield a portion of a structural member. The bearing portion can protect the portion of the structural member from damage resulting from foot traffic associated with accessing an area nearby the structural member.
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公开(公告)号：US20190039713A1
公开(公告)日：2019-02-07
申请号：US15665627
申请日：2017-08-01
摘要： One example of a fairing for a rotorcraft includes an outer mold line portion (OML portion) and a bearing portion extending from the OML portion. The OML portion provides at least a portion of an outer mold line of the rotorcraft. Both the OML portion and the bearing portion shield a portion of a structural member. The bearing portion can protect the portion of the structural member from damage resulting from foot traffic associated with accessing an area nearby the structural member.
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