Variable stiffness blanket with variable heating
    3.
    发明授权
    Variable stiffness blanket with variable heating 有权
    可变刚度毯可变加热

    公开(公告)号:US09585198B2

    公开(公告)日:2017-02-28

    申请号:US14283555

    申请日:2014-05-21

    Abstract: A heater system includes a bag forming a cavity, a fluid bladder carried within the cavity and forming a fluidly sealed chamber. The fluid bladder being configured to store electrorheological fluid within a fluidly sealed chamber. The heater system further including an electrical wire in fluid communication with the electrorheological fluid and a heater blanket carried within the cavity. The method includes altering the electrorheological fluid with a current and providing heat with a heater blanket.

    Abstract translation: 加热器系统包括形成空腔的袋,在腔内承载的流体气囊并形成流体密封的室。 流体囊被构造成将电流变流体存储在流体密封的腔室内。 加热器系统还包括与电流变流体流体连通的电线和在空腔内承载的加热器毯。 该方法包括用电流改变电流变流体并用加热器毯提供热量。

    ELECTRIC REACTION CONTROL SYSTEM
    4.
    发明申请

    公开(公告)号:US20200172237A1

    公开(公告)日:2020-06-04

    申请号:US16206088

    申请日:2018-11-30

    Abstract: An electric reaction control system that can selectively expel a “burst” or “puff” of air to alter the orientation of the aircraft during flight. An aircraft incorporating ducting, an air compressor, an electric motor, and a plurality of nozzles can facilitate in-flight trajectory modifications. When an air burst is needed to provide thrust for the purposes of reaction control, nozzles are selectively opened and closed to provide roll, pitch, and yaw of the aircraft. The ERCS can facilitate an electric aircraft that would be very agile and very light, utilizing electric power, as opposed to jet power.

    Electric distributed propulsion anti-torque redundant power and control system

    公开(公告)号:US10526085B2

    公开(公告)日:2020-01-07

    申请号:US15598842

    申请日:2017-05-18

    Inventor: Carlos Fenny

    Abstract: The present invention includes an electric distributed propulsion for anti-torque modules for a helicopter and methods of use comprising: two or more generators connected to a main gearbox transmission; at least a first and a second plurality of variable speed motors connected to one or more fixed pitch blades to provide anti-torque thrust connected to the two or more generators, and at least a first and a second yaw control computer independently connected to each of the at least first and second plurality of variable speed motors, wherein each of the first and second yaw control computer serves as a primary and a backup yaw control computer to provide redundant control to both the first and second plurality of variable speed motors.

    Automated diagnostic inspection of mechanical controls
    6.
    发明授权
    Automated diagnostic inspection of mechanical controls 有权
    机械控制自动诊断检查

    公开(公告)号:US09227738B2

    公开(公告)日:2016-01-05

    申请号:US13731974

    申请日:2012-12-31

    CPC classification number: B64F5/0045 B64F5/60 G05B23/0256

    Abstract: A system and method to diagnosis an actuator of a flight control system. The system and method includes interfacing a diagnostic computer to the flight control system, commanding movement of an actuator with the diagnostic computer via the flight control system, measuring performance of the actuator via the diagnostic computer, and comparing the measured performance of the actuator with allowable performance values.

    Abstract translation: 一种用于诊断飞行控制系统的执行器的系统和方法。 该系统和方法包括将诊断计算机连接到飞行控制系统,通过飞行控制系统命令致动器与诊断计算机的运动,通过诊断计算机测量致动器的性能,并将执行器的测量性能与允许的 性能价值。

    AUTOMATED DIAGNOSTIC INSPECTION OF MECHANICAL CONTROLS
    7.
    发明申请
    AUTOMATED DIAGNOSTIC INSPECTION OF MECHANICAL CONTROLS 有权
    机械控制自动诊断检测

    公开(公告)号:US20140188332A1

    公开(公告)日:2014-07-03

    申请号:US13731974

    申请日:2012-12-31

    CPC classification number: B64F5/0045 B64F5/60 G05B23/0256

    Abstract: A system and method to diagnosis an actuator of a flight control system. The system and method includes interfacing a diagnostic computer to the flight control system, commanding movement of an actuator with the diagnostic computer via the flight control system, measuring performance of the actuator via the diagnostic computer, and comparing the measured performance of the actuator with allowable performance values.

    Abstract translation: 一种用于诊断飞行控制系统的执行器的系统和方法。 该系统和方法包括将诊断计算机连接到飞行控制系统,通过飞行控制系统命令致动器与诊断计算机的运动,通过诊断计算机测量致动器的性能,并将执行器的测量性能与允许的 性能价值。

    ELECTRIC DISTRIBUTED PROPULSION ANTI-TORQUE REDUNDANT POWER AND CONTROL SYSTEM

    公开(公告)号:US20170349276A1

    公开(公告)日:2017-12-07

    申请号:US15598842

    申请日:2017-05-18

    Inventor: Carlos Fenny

    Abstract: The present invention includes an electric distributed propulsion for anti-torque modules for a helicopter and methods of use comprising: two or more generators connected to a main gearbox transmission; at least a first and a second plurality of variable speed motors connected to one or more fixed pitch blades to provide anti-torque thrust connected to the two or more generators, and at least a first and a second yaw control computer independently connected to each of the at least first and second plurality of variable speed motors, wherein each of the first and second yaw control computer serves as a primary and a backup yaw control computer to provide redundant control to both the first and second plurality of variable speed motors.

    VARIABLE STIFFNESS BLANKET WITH VARIABLE HEATING
    10.
    发明申请
    VARIABLE STIFFNESS BLANKET WITH VARIABLE HEATING 有权
    具有可变加热功能的可变刚度滤芯

    公开(公告)号:US20150341989A1

    公开(公告)日:2015-11-26

    申请号:US14283555

    申请日:2014-05-21

    Abstract: A heater system includes a bag forming a cavity, a fluid bladder carried within the cavity and forming a fluidly sealed chamber. The fluid bladder being configured to store electrorheological fluid within a fluidly sealed chamber. The heater system further including an electrical wire in fluid communication with the electrorheological fluid and a heater blanket carried within the cavity. The method includes altering the electrorheological fluid with a current and providing heat with a heater blanket.

    Abstract translation: 加热器系统包括形成空腔的袋,在腔内承载的流体气囊并形成流体密封的室。 流体囊被构造成将电流变流体存储在流体密封的腔室内。 加热器系统还包括与电流变流体流体连通的电线和在腔内承载的加热器毯。 该方法包括用电流改变电流变流体并用加热器毯提供热量。

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