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    SIMPLEX FLIGHT CONTROL COMPUTER TO BE USED IN A FLIGHT CONTROL SYSTEM
    1.
    发明申请
    SIMPLEX FLIGHT CONTROL COMPUTER TO BE USED IN A FLIGHT CONTROL SYSTEM 审中-公开

    公开(公告)号：WO2022074470A1

    公开(公告)日：2022-04-14

    申请号：PCT/IB2021/055452

    申请日：2021-06-21

    申请人： THALES CANADA INC.

    发明人： CADOTTE, Patrick ,  LIESK, Torsten ,  CLÉMENT, Frédérick

    IPC分类号： B64C13/00 ,  B64C19/00 ,  B64D45/00 ,  G06F11/30

    摘要： A simplex Flight Control Computer (FCC) to be used in a flight control system comprising the simplex Flight Control Computer and at least one neighboring flight control computer is disclosed. The simplex flight control computer comprises an input providing module for receiving sensor data, system data as well as data generated by at least one given neighboring flight control computer; a processing unit for executing a command partition and a monitor partition, wherein the processing unit receives the sensor data, the system data and the data generated by each of the at least one given neighboring flight control computer; wherein the monitor partition is used for monitoring the data generated by each of the at least one given neighboring flight control computer and for providing to each of the at least one neighboring flight control computer a signal indicative of said monitoring, and wherein the command partition is used for generating command signals; a hardware monitoring module for providing a corresponding validity signal indicative of a health of the flight control computer; an output cutoff module receiving each corresponding Flight Control Computer validity signal as well as enable signals generated by each monitor partition; the output cutoff module providing an enable signal in accordance with a predetermined enabling strategy; and an enable switch operatively connected to the output cutoff module and to the processing unit and for providing a received signal originating from the command partition according to the enable signal.

    AN ACTUATOR MECHANISM
    2.
    发明申请
    AN ACTUATOR MECHANISM 审中-公开

    公开(公告)号：WO2022019852A1

    公开(公告)日：2022-01-27

    申请号：PCT/TR2021/050354

    申请日：2021-04-15

    申请人： TUSAS- TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI

    发明人： CAMLICA, Fahri Bugra

    IPC分类号： H01L41/09 ,  H02N2/00 ,  F03G7/06 ,  B64C9/00 ,  B64C13/00

    摘要： The invention relates to a body (2), at least one actuator (3) produced from an electro¬ active polymer material that changes form due to electrical energy, thereby actuating the body (2), at least two strengtheners (4) allowing the actuator (3) to change its form, each holding the actuator (3) from a different side, and are positioned oppositely on the body (2), at least one retainer tip (5) holding the actuator (3) from at least one side thereof.

    IN-FLIGHT STABILIZATION OF AN AIRCRAFT
    3.
    发明申请
    IN-FLIGHT STABILIZATION OF AN AIRCRAFT 审中-公开

    公开(公告)号：WO2021118925A1

    公开(公告)日：2021-06-17

    申请号：PCT/US2020/063598

    申请日：2020-12-07

    申请人： BETA AIR, LLC

    发明人： LIST, Alexander ,  FERRIER, Lochie ,  CLARK, Kyle

    IPC分类号： B64C13/00

    摘要： A system for in-flight stabilization including a plurality of flight components mechanically coupled to an aircraft, wherein the plurality of flight components includes a first flight component and a second flight component opposing the first flight component. The system further comprises a sensor mechanically coupled to the aircraft, wherein the sensor is configured to detect a failure event of a first flight component. The system comprises a vehicle controller communicatively connected to the sensor and is configured to receive the failure datum of the first flight component from the sensor, initiate an automatic response as a function of the failure datum. Initiating the automatic response further includes determining an autorotation inducement action for the second flight component to perform and commanding the second flight component to perform the autorotation inducement action.

    AN ACTUATING SYSTEM
    4.
    发明申请
    AN ACTUATING SYSTEM 审中-公开

    公开(公告)号：WO2021040657A1

    公开(公告)日：2021-03-04

    申请号：PCT/TR2020/050751

    申请日：2020-08-25

    申请人： TUSAS- TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI

    发明人： AKMAN, Yunus

    IPC分类号： B64C13/00

    摘要： The present invention relates to a body (2) suitable for use at landing gears and/or control surfaces of air vehicles; at least a first chamber (3) extending in the body (2) in its entire length; at least a second chamber (4) removably attached to the first chamber (3); at least a first motor (5) located in the first chamber (3) and providing power generation; a first gear path (6) which is located on outer perimeter of the first chamber (3) such that it almost completely surrounds the first chamber (3) that moves when the first gear path (6) is triggered; at least one shaft (7) which is located in the second chamber (4) and is rotatable around its own axis upon being triggered by the first motor (5); and at least a second motor (8) which is located on the body (2), provides energy production when the first motor (5) is deactivated by the control unit (K), and is operated by the control unit (K).

    AIRCRAFT PASSENGER CABIN AIRFLOW METERING
    6.
    发明申请
    AIRCRAFT PASSENGER CABIN AIRFLOW METERING 审中-公开

    公开(公告)号：WO2018132096A1

    公开(公告)日：2018-07-19

    申请号：PCT/US2017/013058

    申请日：2017-01-11

    申请人： PATS AIRCRAFT, LLC

    发明人： PAQUETTE, Tobias

    IPC分类号： F16K17/16 ,  B64C1/00 ,  B64C1/18 ,  B64C13/00 ,  B64C13/02 ,  B64C13/04

    CPC分类号： B64C1/18 ,  B64C1/00 ,  B64C2001/009 ,  F16K17/16

    摘要： An aircraft passenger cabin airflow metering apparatus and system is provided. The apparatus includes a blowout disc designed to release at a predetermined air pressure differential on opposite sides of the blowout disc. The blowout disc may include a cutout to allow a desired amount of airflow during normal operation. The apparatus is affixed to an existing structure in a frame bay at the perimeter of the passenger cabin floor level of the aircraft. The airflow metering system includes a combination of airflow metering apparatuses placed within discrete rooms of an aircraft passenger cabin to achieve positive pressure in the passenger cabin and the desired amount of airflow exhaust from the passenger cabin during normal operation across all areas of the aircraft and to also achieve the desired amount of airflow during abnormal operation when the air pressure on either side of the airflow metering apparatus exceeds a predetermined threshold.

    DISPOSITIF DE CODAGE D'INFORMATIONS ENTRE UNE PLURALITÉ D'INTERRUPTEURS D'UN LEVIER DE MANŒUVRE ET UN DISPOSITIF DE COMMANDE
    8.
    发明申请
    DISPOSITIF DE CODAGE D'INFORMATIONS ENTRE UNE PLURALITÉ D'INTERRUPTEURS D'UN LEVIER DE MANŒUVRE ET UN DISPOSITIF DE COMMANDE 审中-公开
    用于在多个扳手的扳手和控制装置之间编码信息的装置

    公开(公告)号：WO2018087353A1

    公开(公告)日：2018-05-17

    申请号：PCT/EP2017/079017

    申请日：2017-11-13

    申请人： RATIER-FIGEAC

    发明人： DE LA BARDONNIE, Jean

    IPC分类号： H03M11/24 ,  B64C13/00 ,  H03M1/78

    摘要： L'invention concerne un dispositif (1) de codage d'informations entre une pluralité d'interrupteurs (P1...Pn) normalement fermés placés sur un levier de manœuvre (2) et un dispositif (9) de commande, lesdits interrupteurs étant connectés en série entre une ligne de tension (3) et une ligne de mesure (5), chaque interrupteur (Pi) étant associés à une résistance (Ri) unique connectée entre la borne de l'interrupteur la plus proche d'une source de tension (Vcc) et la ligne de mesure. Le dispositif de codage permet ainsi d'obtenir une hiérarchie des interrupteurs.

    摘要翻译： 本发明涉及一种用于在多个信息之间编码信息的设备（1）。 开关（P1 ... Pn）的常闭（E S）PLAC（E S）上的操作杆（2）和设备（9），用于控制，所述开关E中的线之间的作为E连接（E S）系列相关 电压（3）和测量线（5），每个开关（Pi）与其相关联; 连接在最靠近电压源（Vcc）的开关的端子与测量线之间的单个电阻器（Ri）。 编码设备因此可以获得开关的层次结构。

    ARCUATE MOTION ACTUATOR AND FIN SERVO BASED ON PIEZO-ELECTRIC MOTORS
    10.
    发明申请
    ARCUATE MOTION ACTUATOR AND FIN SERVO BASED ON PIEZO-ELECTRIC MOTORS 审中-公开
    基于压电马达的ARCUATE MOTION ACTUATOR和FIN SERVO

    公开(公告)号：WO2017149541A1

    公开(公告)日：2017-09-08

    申请号：PCT/IL2017/050262

    申请日：2017-03-01

    申请人： NANOMOTION ,  KARASIKOV, Nir

    发明人： KARASIKOV, Nir

    IPC分类号： B64C11/16 ,  B64C27/00 ,  F42B15/00 ,  B64C13/00

    摘要： A flap actuator for adjusting the orientation of a flap or the like, the actuator. The actuator includes: a static arcuate member having a radius of curvature; a piezoelectric motor biased to be in operable contact with the static arcuate member; a housing for housing the piezoelectric motor; and a flap orientation shaft operably connecting between the housing and the flap. The distance between the shaft and the static arcuate member is essentially equal to the radius of curvature of the static arcuate member.

    摘要翻译： 用于调节襟翼等的定向的襟翼致动器，致动器。 致动器包括：具有曲率半径的静态弓形构件; 压电马达，其被偏压以与所述静态弓形构件可操作地接触; 用于容纳压电马达的壳体; 以及可操作地连接在壳体和翼片之间的翼片定向轴。 轴和静态弧形构件之间的距离基本上等于静态弧形构件的曲率半径。