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公开(公告)号：US11512811B2
公开(公告)日：2022-11-29
申请号：US16316766
申请日：2017-07-11
Applicant: SIKORSKY AIRCRAFT CORPORATION
Inventor： Adam R. Glasser , Dwaine Wint , John J. Baldyga , Michael F. Mullen , David M. Lutian , Lindsey McKan
IPC: F16N29/02 , B64D45/00 , F16H57/04 , F16N29/04 , B64C27/14 , F16N29/00 , F16N7/00 , B64C27/16 , G01N33/28 , G01F23/22 , G01F23/24
Abstract: A gearbox includes a housing including a lubricant reservoir, at least one gear system arranged in the housing, at least one lubricant delivery passage operable to direct a flow of lubricant from a lubricant reservoir onto the at least one gear system, at least one lubricant return passage operable to guide the flow of lubricant to the lubricant reservoir, and a lubricant-out sensor fluidically connected to the at least one lubricant return passage. The lubricant-out sensor is operable to detect a non-pressure based parameter of the lubricant.
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公开(公告)号：US09624798B2
公开(公告)日：2017-04-18
申请号：US14100559
申请日：2013-12-09
Applicant: Sikorsky Aircraft Corporation
Inventor： Michael F. Mullen , Clark V. Cooper , Adam R. Glasser , Thomas L. Sbabo
CPC classification number: F01M9/02 , B64C27/14 , F16H57/0442 , F16H57/045 , F16H57/046 , F16N39/00
Abstract: A lubrication system includes an additive and a delivery system. During normal operational conditions, the lubricating oil circulating in the transmission system is collected and contained in a secondary oil reservoir to retain a quantity of the lubricating oil for use in an oil-out condition. When an oil-out condition is detected, the additive is injected and mixed with the collected lubricating oil in the secondary oil reservoir or dispersed directly into a power transmission gearbox housing to enhance the characteristics of the lubricating oil and increases the operational time period of the power transmission gearbox during an oil-out condition.
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公开(公告)号：US10421537B2
公开(公告)日：2019-09-24
申请号：US15203615
申请日：2016-07-06
Applicant: Sikorsky Aircraft Corporation
Inventor： William Wolcott , Michael F. Mullen
Abstract: A locking mechanism for a driveshaft disconnect coupling includes an input jaw member defining a rotation axis, an output jaw member connectable to the input jaw member for common rotation with the input jaw member, and a cartridge assembly. The cartridge assembly is fixed to the input jaw member, includes a pin, and defines a pin movement axis. The pin is movable along the pin axis between a radially inner position and a radially outer position, the pin being disengaged from the output jaw member in the radially inner position and the pin being engaged to the output jaw member in the radially outer position.
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Patent Agency Ranking
公开(公告)号：US20190154200A1
公开(公告)日：2019-05-23
申请号：US16316766
申请日：2017-07-11
Applicant: SIKORSKY AIRCRAFT CORPORATION
Inventor： Adam R. Glasser , Dwaine Wint , John J. Baldyga , Michael F. Mullen , David M. Lutian , Lindsey McKan
Abstract: A gearbox includes a housing including a lubricant reservoir, at least one gear system arranged in the housing, at least one lubricant delivery passage operable to direct a flow of lubricant from a lubricant reservoir onto the at least one gear system, at least one lubricant return passage operable to guide the flow of lubricant to the lubricant reservoir, and a lubricant-out sensor fluidically connected to the at least one lubricant return passage. The lubricant-out sensor is operable to detect a non-pressure based parameter of the lubricant.
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公开(公告)号：US10745122B2
公开(公告)日：2020-08-18
申请号：US15918816
申请日：2018-03-12
Applicant: Sikorsky Aircraft Corporation
Inventor： Michael F. Mullen , William Wolcott , Kyle Winters
Abstract: An aircraft tail rotor system includes a rotating pitch change shaft, a translating element, and a pitch change bearing assembly including a first bearing and a second bearing. The pitch change bearing assembly is operable to transmit movement of the translating element to the rotating pitch change shaft via the first bearing or the second bearing. A failure section is formed at an interface between the first bearing and the translating element. When the failure section decouples the first bearing from the translating element such that the first bearing does not transmit movement of the translating element to the rotating pitch change shaft, the second bearing transmits movement of the translating element to the rotating pitch change shaft.
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公开(公告)号：US20180009524A1
公开(公告)日：2018-01-11
申请号：US15203615
申请日：2016-07-06
Applicant: Sikorsky Aircraft Corporation
Inventor： William Wolcott , Michael F. Mullen
Abstract: A locking mechanism for a driveshaft disconnect coupling includes an input jaw member defining a rotation axis, an output jaw member connectable to the input jaw member for common rotation with the input jaw member, and a cartridge assembly. The cartridge assembly is fixed to the input jaw member, includes a pin, and defines a pin movement axis. The pin is movable along the pin axis between a radially inner position and a radially outer position, the pin being disengaged from the output jaw member in the radially inner position and the pin being engaged to the output jaw member in the radially outer position.
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公开(公告)号：US20170114439A1
公开(公告)日：2017-04-27
申请号：US15317804
申请日：2015-04-16
Applicant: Sikorsky Aircraft Corporation
Inventor： Ibibia Altraide , Tapas K. Mukherji , Michael F. Mullen
CPC classification number: C23C4/10 , B23P6/00 , C23C4/06 , C23C4/08 , C23C4/12 , C23C4/123 , C23C4/129
Abstract: A coating and surface repair method is provided. The method includes positioning a high velocity air fuel (HVAF) gun proximate to a damaged hardened steel surface and forming a ceramic metallic coating on the damaged hardened steel surface by executing an HVAF thermal spray process using the HVAF gun.
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公开(公告)号：US20140097044A1
公开(公告)日：2014-04-10
申请号：US14100559
申请日：2013-12-09
Applicant: Sikorsky Aircraft Corporation
Inventor： Michael F. Mullen , Clark V. Cooper , Adam R. Glasser , Thomas L. Sbabo
CPC classification number: F01M9/02 , B64C27/14 , F16H57/0442 , F16H57/045 , F16H57/046 , F16N39/00
Abstract: A lubrication system includes an additive and a delivery system. During normal operational conditions, the lubricating oil circulating in the transmission system is collected and contained in a secondary oil reservoir to retain a quantity of the lubricating oil for use in an oil-out condition. When an oil-out condition is detected, the additive is injected and mixed with the collected lubricating oil in the secondary oil reservoir or dispersed directly into a power transmission gearbox housing to enhance the characteristics of the lubricating oil and increases the operational time period of the power transmission gearbox during an oil-out condition.
Abstract translation: 润滑系统包括添加剂和递送系统。 在正常运行条件下，在传动系统中循环的润滑油被收集并包含在二次油存储器中，以保持一定数量的润滑油用于排油状态。 当检测到出油条件时，将添加剂注入并与收集的润滑油混合在二次油储存器中或直接分散到动力传动齿轮箱壳体中，以增强润滑油的特性并增加操作时间 输油条件下的变速箱。
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