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    Grinding module, a grinding machine and a method for grinding
    21.
    发明授权
    Grinding module, a grinding machine and a method for grinding 有权

    公开(公告)号：US11491606B2

    公开(公告)日：2022-11-08

    申请号：US15770151

    申请日：2015-10-21

    Applicant: ST ENGINEERING AEROSPACE LTD.

    Inventor： Yong Wee Liu

    IPC: B24B41/06 ,  B24B41/02 ,  B24B21/16 ,  B24B19/00 ,  B24B47/12

    Abstract: According to various embodiments, there is provided a grinding module including a base; a cylinder mounted to the base with a longitudinal axis of the cylinder arranged at least substantially perpendicular to a surface of the base, wherein the cylinder is rotatable about the longitudinal axis of the cylinder, and wherein a cylindrical surface of the cylinder is adapted to receive a grinding belt; a linear actuator mounted to the base with a centreline of linear motion of the linear actuator arranged to intersect the longitudinal axis of the cylinder; and a holder connected to the linear actuator, the holder adapted to hold a workpiece with a surface of the workpiece facing the cylindrical surface of the cylinder, wherein the linear actuator is adapted to move the holder relative to the cylinder along the centreline of linear motion of the linear actuator, and wherein the cylindrical surface of the cylinder is adapted to define a curved profile so that the grinding belt is adapted to grind and shape the surface of the workpiece to conform to the curved profile.

    System for configuring an aircraft in a single-pilot mode or a two-pilot mode
    22.
    发明授权
    System for configuring an aircraft in a single-pilot mode or a two-pilot mode 有权

    公开(公告)号：US11834151B2

    公开(公告)日：2023-12-05

    申请号：US17416335

    申请日：2019-12-19

    Applicant: SAFRAN ELECTRONICS & DEFENSE ,  ST ENGINEERING AEROSPACE Ltd

    Inventor： Eric Walter ,  Loïc Fougeres ,  Mikaël Diaz ,  Philippe Tranie ,  Ng Kwee Chye ,  Tay Siew Liong

    IPC: B64C13/12

    CPC classification number: B64C13/12

    Abstract: A configuration system (80) arranged to configure an aircraft in a single-pilot mode and a two-pilot mode, comprising:



    acquisition means (84) and authentication means (83) arranged to acquire and authenticate a configuration order that defines the selected mode and controls the configuration system (80) to configure the aircraft in the selected mode;
    first activation means (85) arranged to activate equipment dedicated to piloting by a single-pilot on board when the aircraft is configured in single-pilot mode, and to deactivate dedicated equipment when the aircraft is configured in two-pilot mode;
    verification means (87) arranged to, when the aircraft is configured in the single-pilot mode, verify that single-pilot flight conditions are met and inform the sole pilot on board and a ground station of the results of these checks.

    AERIAL VEHICLE
    24.
    发明申请
    AERIAL VEHICLE 审中-公开

    公开(公告)号：US20200172238A1

    公开(公告)日：2020-06-04

    申请号：US16612347

    申请日：2017-05-09

    Applicant: ST ENGINEERING AEROSPACE LTD.

    Inventor： Keen Ian CHAN

    IPC: B64C29/02 ,  B64C39/08 ,  B64F5/10 ,  B64C11/46

    Abstract: An aerial vehicle may include a first wing structure. The aerial vehicle may further include a first propeller and a second propeller disposed along the first wing structure. The aerial vehicle may further include a second wing structure disposed to intersect the first wing structure to form a cross configuration. The aerial vehicle may further include a third propeller and a fourth propeller disposed along the second wing structure. In a hovering orientation of the aerial vehicle, respective propeller rotational axes of the first and second propellers may be angled off-vertical in respective planes which may be perpendicular to a transverse axis of the first wing structure, and respective propeller rotational axes of the third and fourth propellers may be angled off-vertical in respective planes which may be perpendicular to a transverse axis of the second wing structure.

    AIRPORT GROUND COLLISION ALERTING SYSTEM
    25.
    发明申请
    AIRPORT GROUND COLLISION ALERTING SYSTEM 有权

    公开(公告)号：US20230038694A1

    公开(公告)日：2023-02-09

    申请号：US17757876

    申请日：2019-12-27

    Applicant: ST Engineering Aerospace Ltd.

    Inventor： Chi Hui Frederic FOO ,  Chuan Jen Peter LIEW ,  Saik Kong Ronald TAN ,  Wei Ling Michelle QUEK ,  Manjunath Ganesh TIRUVANMIYUR

    IPC: G08G5/04 ,  G08G5/00 ,  G08G5/06

    Abstract: An airport ground collision alerting system and a method of operating an airport ground collision alerting system. The airport ground collision alerting system comprises an automatic dependent surveillance-broadcast, ADS-B, receiver; a first database coupled to the ADS-B receiver and configured for look-up of aircraft type data based on aircraft ID data received via the ADS-B receiver and for storing aircraft position and heading data received via the ADS-B receiver; a second database configured to store digital map data for one or more airports; a processor unit coupled to the first and second databases and an application programming interface, API, configured to couple the airport ground collision alerting system to a display device.

    Aerial vehicle
    26.
    发明授权
    Aerial vehicle 有权

    公开(公告)号：US11479351B2

    公开(公告)日：2022-10-25

    申请号：US16612347

    申请日：2017-05-09

    Applicant: ST ENGINEERING AEROSPACE LTD.

    Inventor： Keen Ian Chan

    IPC: B64C29/02 ,  B64F5/10 ,  B64C11/46 ,  B64C39/08

    Abstract: An aerial vehicle may include a first wing structure. The aerial vehicle may further include a first propeller and a second propeller disposed along the first wing structure. The aerial vehicle may further include a second wing structure disposed to intersect the first wing structure to form a cross configuration. The aerial vehicle may further include a third propeller and a fourth propeller disposed along the second wing structure. In a hovering orientation of the aerial vehicle, respective propeller rotational axes of the first and second propellers may be angled off-vertical in respective planes which may be perpendicular to a transverse axis of the first wing structure, and respective propeller rotational axes of the third and fourth propellers may be angled off-vertical in respective planes which may be perpendicular to a transverse axis of the second wing structure.

    METHOD FOR PILOTING AN AIRCRAFT
    27.
    发明申请
    METHOD FOR PILOTING AN AIRCRAFT 有权

    公开(公告)号：US20220063836A1

    公开(公告)日：2022-03-03

    申请号：US17415482

    申请日：2019-12-19

    Applicant: SAFRAN ELECTRONICS & DEFENSE ,  ST ENGINEERING AEROSPACE Ltd

    Inventor： Eric WALTER ,  Julien FARJON ,  Mikaël DIAZ ,  Nicolas CADALEN ,  Philippe TRANIE ,  Ng KWEE CHYE ,  Hoon TA HUANG JACKSON

    IPC: B64D45/00 ,  G05D1/00

    Abstract: A method for piloting a pre-existing aircraft comprising the following steps: integrating an alternative piloting system (1) into the pre-existing aircraft; connecting the aircraft (200) and a ground station in which a ground pilot (207) is positioned; when the aircraft is in a normal state, having the aircraft piloted by a nominal crew; using detection means to detect the occurrence of an emergency situation and, when the occurrence of the emergency is detected: making the ground pilot (207) operational, so that the ground pilot can produce an aircraft ground piloting set-point; transmitting the ground piloting setpoint to the aircraft; using the alternative piloting system to acquire and transmit the ground piloting setpoint to the aircraft flight control system.

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