-
公开(公告)号：US11685506B2
公开(公告)日：2023-06-27
申请号：US15929764
申请日：2020-05-20
CPC分类号： B64C1/18 , B32B3/12 , B32B5/06 , B32B7/09 , B32B7/14 , B64C1/403 , B32B2307/10 , B32B2307/102 , B32B2471/02 , B32B2605/003 , B32B2605/18
摘要： A finished floor assembly covers a floor area of an aircraft and includes a subfloor, a padding assembly, and a finish flooring layer. Noise radiates from the subfloor due to vibrations transmitted by an aircraft structure. The padding assembly attenuates the noise and includes a first pad layer, a second pad layer, and a plurality of discontinuous couplings. The first pad layer abuts the subfloor. The second pad layer is adjacent to the first pad layer. The plurality of discontinuous couplings are laterally separated from each other along the floor area by void portions. The discontinuous couplings secure the first pad layer to the second pad layer and the first pad layer and the second pad layer are in contact at the void portions. The finish flooring layer disposed overtop the padding assembly.
-
公开(公告)号：US20200369362A1
公开(公告)日：2020-11-26
申请号：US15929764
申请日：2020-05-20
摘要： A finished floor assembly covers a floor area of an aircraft and includes a subfloor, a padding assembly, and a finish flooring layer. Noise radiates from the subfloor due to vibrations transmitted by an aircraft structure. The padding assembly attenuates the noise and includes a first pad layer, a second pad layer, and a plurality of discontinuous couplings. The first pad layer abuts the subfloor. The second pad layer is adjacent to the first pad layer. The plurality of discontinuous couplings are laterally separated from each other along the floor area by void portions. The discontinuous couplings secure the first pad layer to the second pad layer and the first pad layer and the second pad layer are in contact at the void portions. The finish flooring layer disposed overtop the padding assembly.
-
公开(公告)号：US20180105275A1
公开(公告)日：2018-04-19
申请号：US15292776
申请日：2016-10-13
发明人： Kristopher Lynch , Mike Lucas
IPC分类号： B64D13/06
CPC分类号： B64D13/06 , B64D2013/003 , B64D2013/0625
摘要： A ventilation system for ventilating a passenger compartment of an aircraft, an aircraft, and a method of operating the ventilation system are disclosed herein. The ventilation system includes, but is not limited to, a bezel, a fluid vent, an electronic sensor, and a valve. The bezel defines a bezel aperture and the fluid vent defines an axis that passes through the bezel aperture to direct a stream of air through the bezel into the passenger compartment. The electronic sensor is associated with the bezel and is configured to generate a bezel position signal. The valve is configured to vary a flow rate of the stream of air through the fluid vent based on the bezel position signal.
-
公开(公告)号：US09834320B2
公开(公告)日：2017-12-05
申请号：US14697895
申请日：2015-04-28
发明人： Michael Lucas , Michael Brinley , Kristopher Lynch
CPC分类号： B64D47/02 , B64D45/00 , B64D2045/0095 , G10K9/20 , G10K2210/1281 , H04R7/045
摘要： Aircraft, aircraft exterior speaker systems, and methods of projecting sound waves from an exterior of an aircraft are provided. An aircraft includes an outer skin membrane, a vibration actuator, and a controller. The outer skin membrane has an exterior surface that defines an exterior boundary of the aircraft. The vibration actuator is coupled for common vibration with the outer skin membrane. The controller is operatively coupled with the vibration actuator and is configured to generate a command for the vibration actuator based on audible content to be projected from the exterior surface. The controller is further configured to transmit the command to the vibration actuator. The vibration actuator is configured to vibrate in response to receiving the command.
-
公开(公告)号：US11059592B2
公开(公告)日：2021-07-13
申请号：US15292776
申请日：2016-10-13
发明人： Kristopher Lynch , Mike Lucas
摘要： A ventilation system for ventilating a passenger compartment of an aircraft, an aircraft, and a method of operating the ventilation system are disclosed herein. The ventilation system includes, but is not limited to, a bezel, a fluid vent, an electronic sensor, and a valve. The bezel defines a bezel aperture and the fluid vent defines an axis that passes through the bezel aperture to direct a stream of air through the bezel into the passenger compartment. The electronic sensor is associated with the bezel and is configured to generate a bezel position signal. The valve is configured to vary a flow rate of the stream of air through the fluid vent based on the bezel position signal.
-
公开(公告)号：US20210078691A1
公开(公告)日：2021-03-18
申请号：US16570960
申请日：2019-09-13
发明人： Robert Telmos , Eric Cox , Harrison Grantham , Daniel Condroski , Mike Lucas , Kristopher Lynch
摘要： Exemplary embodiments of a decorative hard flooring system for an aircraft are disclosed herein. The hard flooring system includes a plurality of decorative hard floor assemblies at least some of which include a decorative hard flooring layer and a metallic substrate layer having at least one aperture formed therein to receive a warming element. The flooring system further includes, a power supply coupled to the warming element and a controller coupled to the power supply to control the power supplied to the warming element. An ambient temperature sensor coupled to the controller to provide an indication of ambient temperature so that the controller controls the power supply to power the warming elements to warm the decorative hard floor assemblies to be substantially at the ambient temperature.
-
公开(公告)号：US20160318627A1
公开(公告)日：2016-11-03
申请号：US14697895
申请日：2015-04-28
发明人： Michael Lucas , Michael Brinley , Kristopher Lynch
CPC分类号： B64D47/02 , B64D45/00 , B64D2045/0095 , G10K9/20 , G10K2210/1281 , H04R7/045
摘要： Aircraft, aircraft exterior speaker systems, and methods of projecting sound waves from an exterior of an aircraft are provided. An aircraft includes an outer skin membrane, a vibration actuator, and a controller. The outer skin membrane has an exterior surface that defines an exterior boundary of the aircraft. The vibration actuator is coupled for common vibration with the outer skin membrane. The controller is operatively coupled with the vibration actuator and is configured to generate a command for the vibration actuator based on audible content to be projected from the exterior surface. The controller is further configured to transmit the command to the vibration actuator. The vibration actuator is configured to vibrate in response to receiving the command.
摘要翻译： 提供飞机，飞机外部扬声器系统以及从飞机外部投射声波的方法。 飞机包括外皮膜，振动致动器和控制器。 外皮膜具有限定飞机外部边界的外表面。 振动致动器与外皮膜共同振动。 控制器可操作地与振动致动器耦合，并且被配置为基于从外表面突出的可听内容产生用于振动致动器的命令。 控制器还被配置为将该命令发送到振动致动器。 振动致动器被配置为响应于接收到该命令而振动。
-
公开(公告)号：US20230271692A1
公开(公告)日：2023-08-31
申请号：US18315253
申请日：2023-05-10
CPC分类号： B64C1/18 , B32B3/12 , B32B5/06 , B32B7/09 , B32B7/14 , B64C1/403 , B32B2307/10 , B32B2307/102 , B32B2471/02 , B32B2605/003 , B32B2605/18
摘要： A finished floor assembly covers a floor area of an aircraft and includes a subfloor, a padding assembly, and a finish flooring layer. Noise radiates from the subfloor due to vibrations transmitted by an aircraft structure. The padding assembly attenuates the noise and includes a first pad layer, a second pad layer, and a plurality of discontinuous couplings. The first pad layer abuts the subfloor. The second pad layer is adjacent to the first pad layer. The plurality of discontinuous couplings are laterally separated from each other along the floor area by void portions. The discontinuous couplings secure the first pad layer to the second pad layer and the first pad layer and the second pad layer are in contact at the void portions. The finish flooring layer disposed overtop the padding assembly.
-
公开(公告)号：US11293664B2
公开(公告)日：2022-04-05
申请号：US15913688
申请日：2018-03-06
发明人： Randy Hull , Andrew Gorton , Kristopher Lynch
摘要： Ventilation systems, aircraft, and silencers are disclosed herein. An aircraft includes a ventilation system. A ventilation system includes first and second air flow sources configured to generate first and second air flows, a silencer, a first conditioning vent, and a second conditioning vent. A divider spans an interior dimension of the housing to define a first cavity and a second cavity, where the divider restricts substantially all mass flow between the first cavity and the second cavity in the housing. First and second silencer tubes have porous portions disposed in the respective cavity and are operatively coupled with the respective air flow source to receive the respective air flow. First and second conditioning vents are operatively coupled with the respective silencer tubes to direct the respective air flows to a conditioned volume.
-
公开(公告)号：US20190277535A1
公开(公告)日：2019-09-12
申请号：US15913688
申请日：2018-03-06
发明人： Randy Hull , Andrew Gorton , Kristopher Lynch
摘要： Ventilation systems, aircraft, and silencers are disclosed herein. An aircraft includes a ventilation system. A ventilation system includes first and second air flow sources configured to generate first and second air flows, a silencer, a first conditioning vent, and a second conditioning vent. A divider spans an interior dimension of the housing to define a first cavity and a second cavity, where the divider restricts substantially all mass flow between the first cavity and the second cavity in the housing. First and second silencer tubes have porous portions disposed in the respective cavity and are operatively coupled with the respective air flow source to receive the respective air flow. First and second conditioning vents are operatively coupled with the respective silencer tubes to direct the respective air flows to a conditioned volume.
-
-
-
-
-
-
-
-
-
搜索结果
10 条记录 (耗时 0.014 秒)
