公开(公告)号：US08650855B2

公开(公告)日：2014-02-18

申请号：US12673828

申请日：2008-07-07

Applicant: Hakim Maalioune

Inventor： Hakim Maalioune

IPC: F02K1/72

CPC classification number: F02K1/763 ,  F02K1/72 ,  F05D2270/303 ,  F05D2270/62

Abstract: The control system of the invention includes at least one actuator (6) for a cowling (2), driven by at least one electric motor (7), and a control means (9) for the electric motor (7). The electric motor control means (9) includes a means for determining and/or estimating the outside temperature of the turbojet engine, the electric motor control means being adapted for adjusting the driving torque supplied by the electric motor on the basis of said outer temperature.

Abstract translation: 本发明的控制系统包括用于由至少一个电动机（7）驱动的整流罩（2）的至少一个致动器（6）和用于电动机（7）的控制装置（9）。 电动机控制装置（9）包括用于确定和/或估计涡轮喷气发动机的外部温度的装置，电动机控制装置适于基于所述外部温度来调节由电动机提供的驱动转矩。

公开(公告)号：US08285467B2

公开(公告)日：2012-10-09

申请号：US12673890

申请日：2008-07-16

Applicant: Hakim Maalioune

Inventor： Hakim Maalioune

IPC: F02K3/02 ,  F02K1/32

CPC classification number: F02K1/763 ,  F02K1/72 ,  F05D2270/62

Abstract: The invention relates to a method for controlling at least one actuator for actuating the cowlings of a thrust inverter in a turbojet engine, the actuator being driven by an electric motor including a relative position sensor providing information on the evolution of the movement thereof, wherein the motor is controlled based on the instantaneous position of the cowling in at least one portion of the movement thereof between an open position and a closed position, the instantaneous position of the cowling being determined from at least one reference position absolute data and relative position data relative to said reference position provided by the relative position sensor of the motor, wherein in case the actuation is resumed after an interruption, a new determination of the reference position is initiated.

Abstract translation: 本发明涉及一种用于控制至少一个致动器的方法，用于致动涡轮喷气发动机中的推力逆变器的整流罩，该致动器由包括相对位置传感器的电动机驱动，该相对位置传感器提供关于其运动演变的信息，其中 基于整流罩在其打开位置和关闭位置之间的运动的至少一部分中的瞬时位置来控制电动机，整流罩的瞬时位置由至少一个参考位置确定绝对数据和相对位置数据相对 到由电动机的相对位置传感器提供的所述参考位置，其中在中断之后恢复启动的情况下，启动对基准位置的新的确定。

公开(公告)号：US20110050277A1

公开(公告)日：2011-03-03

申请号：US12673803

申请日：2008-07-07

Applicant: Hakim Maalioune

Inventor： Hakim Maalioune

IPC: G01R31/34

CPC classification number: F02K1/72 ,  F01D21/003 ,  F02K1/763 ,  F02K1/766 ,  G05B9/02 ,  G05B23/0235 ,  G05B23/0286 ,  Y02T50/671

Abstract: The control system of the invention includes at least one actuator (6) for a cowling (2), driven by at least one electric motor (7), and control means (9) for the electric motor (7) and the actuator (6). The control system includes an electric circuit (C) that comprises: a plurality of electric components; a plurality of measuring means (16-18) adapted for measuring respectively a characteristic magnitude of an electric component or a group of electric components in the electric circuit; a failure detection means (19) adapted for detecting a failure at a component of the electric circuit when the characteristic magnitude measured at said component exceeds a predetermined value or is in a range of predetermined values.

Abstract translation: 本发明的控制系统包括用于由至少一个电动机（7）驱动的整流罩（2）的至少一个致动器（6）和用于电动机（7）和致动器（6）的控制装置（9） ）。 控制系统包括电路（C），其包括：多个电气部件; 多个测量装置（16-18），分别用于测量电路中电气部件或一组电气部件的特征量; 一种故障检测装置，用于当在所述部件上测量的特征量超过预定值或处于预定值的范围内时，检测电路部件的故障。

公开(公告)号：US08955305B2

公开(公告)日：2015-02-17

申请号：US12528945

申请日：2008-02-01

Applicant: Thierry Marin Martinod ,  Hakim Maalioune

Inventor： Thierry Marin Martinod ,  Hakim Maalioune

IPC: F02K1/76

CPC classification number: F02K1/763

Abstract: The invention relates to a method for the self-calibration of electric jacks (6a, 6b) capable of actuating a mobile member (2) of a turbojet nacelle (1) and connected to at least one position measuring member, characterized in that it comprises the steps of: moving the jack(s) into a retracted position corresponding to a first position of the mobile member, storing one or more position values fed back by the position measuring member for the jack(s) in said retracted position; moving the jack(s) into an extended position corresponding to a second position of the mobile member; storing one or mom position values fed back by the position measuring member for the jack(s) in said extended position.

Abstract translation: 本发明涉及一种用于自动校准能够启动涡轮喷气发动机舱（1）的移动构件（2）并连接到至少一个位置测量构件的电动千斤顶（6a，6b）的方法，其特征在于，其包括 步骤：将所述千斤顶移动到对应于所述移动构件的第一位置的缩回位置，将由所述千斤顶的位置测量构件反馈的一个或多个位置值存储在所述缩回位置; 将所述千斤顶移动到对应于所述移动构件的第二位置的延伸位置; 存储由位于所述伸出位置的千斤顶的位置测量构件反馈的一个或多个位置值。

公开(公告)号：US08831900B2

公开(公告)日：2014-09-09

申请号：US12673823

申请日：2008-07-07

Applicant: Hakim Maalioune

Inventor： Hakim Maalioune

IPC: G01D3/00 ,  F02K1/76 ,  F02K1/72 ,  G05B23/02

CPC classification number: F02K1/72 ,  F02K1/763 ,  F02K1/766 ,  F05D2260/80 ,  G05B23/0256 ,  Y02T50/671

Abstract: The invention relates to a system for controlling at least one actuator (6) for thrust reverser cowlings (2) on a turbojet engine, comprising a set of actuator and/or control components with at least one actuator (6) for cowlings (2) driven by at least one electric motor (7) and control means (9) for the electric motor (7). The control means (9) comprise test means (20), with an interface (22) destined for receiving test requests from a user. The test means (20) are designed on reception of a test request to carry out a test cycle on one or more components (7, 6, 15, 18) of the system comprising an isolated actuation to the component(s) (7, 6, 15, 18) with regard to the other components of the system.

Abstract translation: 本发明涉及一种用于控制涡轮喷气发动机上用于推力反向器整流罩（2）的至少一个致动器（6）的系统，包括一组致动器和/或控制部件，其具有用于整流罩（2）的至少一个致动器（6） 由至少一个电动机（7）和用于电动机（7）的控制装置（9）驱动。 控制装置（9）包括具有用于接收来自用户的测试请求的接口（22）的测试装置（20）。 测试装置（20）被设计为接收测试请求，以对系统的一个或多个组件（7,6,15,18）执行测试循环，该组件包括对组件（7）的隔离致动， 6，15，18）关于系统的其他组成部分。

公开(公告)号：US08777155B2

公开(公告)日：2014-07-15

申请号：US13384807

申请日：2010-06-29

Applicant: David Pereira ,  Hakim Maalioune ,  Vincent Le Coq

Inventor： David Pereira ,  Hakim Maalioune ,  Vincent Le Coq

IPC: B64D41/00

CPC classification number: F01D15/10 ,  B64D29/06 ,  B64D41/00 ,  B64D2221/00 ,  F02N11/04

Abstract: The present invention relates to an electric power supply circuit (1) for a turbojet engine nacelle including at least one electric generator (2) mechanically connected to the shaft of a turbojet engine, said generator being capable of directly supplying electric power to a first electric power device other than a simple monitoring or supervising unit, characterized in that said generator is capable of directly supplying electric power to at least one second electric power device other than a monitoring or supervising unit, as well as to a nacelle including such an electric circuit.

Abstract translation: 本发明涉及一种用于涡轮喷气发动机机舱的电力供应回路（1），其包括机械地连接到涡轮喷气发动机的轴的至少一个发电机（2），所述发电机能够直接向第一电动机 除了简单的监视或监督单元之外的功率装置，其特征在于，所述发电机能够直接向除了监视或监督单元之外的至少一个第二电力装置提供电力，以及包括这种电路的机舱 。

公开(公告)号：US20110016846A1

公开(公告)日：2011-01-27

申请号：US12673778

申请日：2008-07-07

Applicant: Hakim Maalioune

Inventor： Hakim Maalioune

IPC: F02K3/02

CPC classification number: G05B23/0291 ,  F02K1/763 ,  F05D2270/094 ,  G05B9/02 ,  G05B2219/42329 ,  Y02T50/671

Abstract: The invention relates to a control system for at least one actuator (6) for the cowlings of a thrust inverter in a turbojet engine, that comprises an assembly of actuation and/or control components. A control means (9) is provided for detecting the failure of an actuation and/or control component (7, 16, 13), for determining the blocking or non-blocking character of the failure for the system operation and, in case of a non-blocking failure, for switching from a nominal operation mode to a failure-adaptation operation mode in which the failure of the actuation and/or control component (7, 16, 13) is compensated at least partially by a modified instruction of the other actuation and/or control components (7, 16, 13).

Abstract translation: 本发明涉及一种用于至少一个用于涡轮喷气发动机中的推力逆变器的整流罩的致动器（6）的控制系统，其包括致动和/或控制部件的组件。 提供控制装置（9），用于检测致动和/或控制部件（7,16,13）的故障，用于确定用于系统操作的故障的阻塞或非阻塞特性，并且在 用于从标称操作模式切换到故障适应操作模式的非阻塞故障，其中致动和/或控制部件（7,16,13）的故障至少部分地由另一个的修改指令补偿 致动和/或控制部件（7,16,13）。

公开(公告)号：US20100107598A1

公开(公告)日：2010-05-06

申请号：US12528945

申请日：2008-02-01

Applicant: Thierry Marin Martinod ,  Hakim Maalioune

Inventor： Thierry Marin Martinod ,  Hakim Maalioune

IPC: F02K3/02 ,  G01D18/00

CPC classification number: F02K1/763

Abstract: The invention relates to a method for the self-calibration of electric jacks (6a, 6b) capable of actuating a mobile member (2) of a turbojet nacelle (1) and connected to at least one position measuring member, characterised in that it comprises the steps of: moving the jack(s) into a retracted position corresponding to a first position of the mobile member, storing one or more position values fed back by the position measuring member for the jack(s) in said retracted position; moving the jack(s) into an extended position corresponding to a second position of the mobile member; storing one or mom position values fed back by the position measuring member for the jack(s) in said extended position.

Abstract translation: 本发明涉及一种用于自动校准能够启动涡轮喷气发动机舱（1）的移动构件（2）并连接到至少一个位置测量构件的电动千斤顶（6a，6b）的方法，其特征在于，其包括 步骤：将所述千斤顶移动到对应于所述移动构件的第一位置的缩回位置，将由所述千斤顶的位置测量构件反馈的一个或多个位置值存储在所述缩回位置; 将所述千斤顶移动到对应于所述移动构件的第二位置的延伸位置; 存储由位于所述伸出位置的千斤顶的位置测量构件反馈的一个或多个位置值。

公开(公告)号：US09109538B2

公开(公告)日：2015-08-18

申请号：US13578270

申请日：2011-02-03

Applicant: Hakim Maalioune

Inventor： Hakim Maalioune

IPC: F02C9/00 ,  F02C7/00 ,  F02K1/15 ,  F02K1/76

CPC classification number: F02K1/15 ,  F02K1/763 ,  Y02T50/671 ,  Y02T50/677

Abstract: The invention relates to a system (10) for controlling an aircraft propelled by at least one jet engine housed in a nacelle, characterised in that said system includes: a full authority electronic control unit (100) of the jet engine, intended for monitoring the jet engine, suitable for monitoring and controlling at least one electrical device of the nacelle; and an electric power unit (200) of the nacelle, external to said full authority electronic control unit of the jet engine for monitoring the jet engine, suitable for managing the electric power supply of said electrical device of the nacelle.

Abstract translation: 本发明涉及一种用于控制由容纳在机舱中的至少一个喷气发动机推进的飞行器的系统（10），其特征在于，所述系统包括：喷气发动机的全权限电子控制单元（100），用于监视 喷气发动机，适用于监控和控制机舱的至少一个电气装置; 以及所述机舱的电力单元（200），其位于用于监视所述喷气发动机的所述用于监视所述喷气发动机的所述全权限电子控制单元的外部，适于管理所述机舱的所述电气装置的电力供应。

公开(公告)号：US08975911B2

公开(公告)日：2015-03-10

申请号：US12673803

申请日：2008-07-07

Applicant: Hakim Maalioune

Inventor： Hakim Maalioune

IPC: G01R31/34 ,  F02K1/72 ,  F01D21/00 ,  F02K1/76 ,  G05B9/02 ,  G05B23/02

CPC classification number: F02K1/72 ,  F01D21/003 ,  F02K1/763 ,  F02K1/766 ,  G05B9/02 ,  G05B23/0235 ,  G05B23/0286 ,  Y02T50/671

Abstract: The control system of the invention includes at least one actuator (6) for a cowling (2), driven by at least one electric motor (7), and control means (9) for the electric motor (7) and the actuator (6). The control system includes an electric circuit (C) that comprises: a plurality of electric components; a plurality of measuring means (16-18) adapted for measuring respectively a characteristic magnitude of an electric component or a group of electric components in the electric circuit; a failure detection means (19) adapted for detecting a failure at a component of the electric circuit when the characteristic magnitude measured at said component exceeds a predetermined value or is in a range of predetermined values.

Abstract translation: 本发明的控制系统包括用于由至少一个电动机（7）驱动的整流罩（2）的至少一个致动器（6）和用于电动机（7）和致动器（6）的控制装置（9） ）。 控制系统包括电路（C），其包括：多个电气部件; 多个测量装置（16-18），分别用于测量电路中电气部件或一组电气部件的特征量; 一种故障检测装置，用于当在所述部件上测量的特征量超过预定值或处于预定值的范围内时，检测电路部件的故障。