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公开(公告)号：US11155337B2
公开(公告)日：2021-10-26
申请号：US16410908
申请日：2019-05-13
Applicant: AIRBUS OPERATIONS S.A.S.
Inventor： Bernard Guering , Laurent Saint-Marc
Abstract: Disclosed herein is a monobloc and removable pedal module for an aircraft rudder bar. The pedal module, which is intended for a rudder bar, includes a pedal, at least one integrated adjustment system, and a connection device which enables a removable connection of the pedal module to be produced. The pedal module is a monobloc component in order to simplify and facilitate its replacement via the removable connection obtained by the connection device.
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公开(公告)号：US20190185130A1
公开(公告)日：2019-06-20
申请号：US16221741
申请日：2018-12-17
Applicant: Airbus Operations S.A.S.
Inventor： Bernard Guering , Laurent Saint-Marc
CPC classification number: B64C1/10 , B64C1/068 , B64C1/14 , B64C1/1415 , B64C1/22 , B64D11/00 , B64D11/0015 , B64D43/00
Abstract: An electrical and electronic bay for an aircraft includes a central area forming a free space, a peripheral side area provided for the arrangement of supporting structures and being placed around said central area, and a lower area placed below the central and peripheral side areas and in which the access opening is placed in said central area. Such an electrical and electronic bay is used in particular to optimize the areas dedicated to the incorporation of electronic equipment in aircraft.
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3.发明申请公开(公告)号：US20190132980A1
公开(公告)日：2019-05-02
申请号：US16173855
申请日：2018-10-29
Applicant: Airbus Operations (S.A.S.)
Inventor： Bernard Guering , Romain Delahaye
Abstract: A supporting structure of optimized volume includes at least two vertical structural elements having a front face and a rear face. Modules including electronic equipment items are fixed onto the front face of the vertical structural elements. Use in particular can be for the integration of avionics modules on aircraft.
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公开(公告)号：US09545992B2
公开(公告)日：2017-01-17
申请号：US14499549
申请日：2014-09-29
Applicant: AIRBUS OPERATIONS S.A.S.
Inventor： Bernard Guering
CPC classification number: B64C3/50 , B64C9/02 , B64C9/06 , B64C9/16 , B64C13/24 , B64C13/28 , B64C13/40 , B64C13/50 , B64C13/504 , Y02T50/32
Abstract: A high-lift trailing edge flap system for an aircraft wing unit is provided. In high-lift trailing edge flap system, the backward movement and the inclination of the trailing edge flap in the extended position are dissociated in order to allow for the incorporation of the actuating mechanism into the wing in the stowed position.
Abstract translation: 提供了一种用于飞机机翼单元的高升力后缘翼片系统。 在高升力后缘翼片系统中，向后移动和后缘翼片处于伸展位置的倾斜被解离，以允许致动机构结合到收起位置的翼中。
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公开(公告)号：US09114880B2
公开(公告)日：2015-08-25
申请号：US14090882
申请日：2013-11-26
Applicant: AIRBUS OPERATIONS (S.A.S.)
Inventor： Bernard Guering
Abstract: The invention relates to a seat back for an aircraft comprising a structural column bearing a plurality of devices for supporting an occupant of the seat, these devices being distributed along the structural column and oriented transversely relatively to the structural column so as to each protrude on either side of this column. This solution can reduce the mass and dimensions, while providing satisfactory comfort for the occupant.
Abstract translation: 本发明涉及一种用于飞行器的座椅靠背，其包括具有多个用于支撑座椅乘员的装置的结构柱，这些装置沿结构柱分布并相对于结构柱横向定向， 这一列的一边。 该解决方案可以降低质量和尺寸，同时为乘客提供令人满意的舒适感。
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Patent Agency Ranking
6.发明申请公开(公告)号：US20140110529A1
公开(公告)日：2014-04-24
申请号：US14062069
申请日：2013-10-24
Applicant: Airbus Operations (S.A.S.)
Inventor： Bernard Guering
IPC: B64C1/06
CPC classification number: B64C1/061 , B64C1/18 , Y10T29/49622
Abstract: Such a fuselage includes cross-members adapted for the formation of a floor, at least one of said cross-members including an upper part, a lower part, linkage for the lower part to the upper part, and at least one opening for the passage of systems which is delimited between the lower part and the upper part. The upper part of the cross-member is fastened to the fuselage and is dimensioned so as to bear the stresses to which said cross-member may be subjected when the aircraft remains on the ground. The lower part is fastened to the upper part so as to reinforce it such that when assembled, the upper part and the lower part are adapted to bear the stresses to which the cross-member may be subjected in flight conditions of the aircraft.
Abstract translation: 这样的机身包括适于形成地板的横向构件，所述横向构件中的至少一个包括上部，下部，用于下部至上部的连杆，以及用于通道的至少一个开口 在下部和上部之间界定的系统。 横梁的上部被固定在机身上，并且其尺寸设计成当飞机保持在地面上时承受所述横梁可能经受的应力。 下部固定到上部，以便加强它，使得当组装时，上部和下部适于承受跨部件在飞行器的飞行状态下可能受到的应力。
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公开(公告)号：US11453503B2
公开(公告)日：2022-09-27
申请号：US16444419
申请日：2019-06-18
Applicant: AIRBUS OPERATIONS (S.A.S.)
Inventor： Laurent Saint-Marc , Bernard Guering
IPC: B64D13/06 , F16L25/00 , F16L27/11 , F16L27/107 , H05K7/20
Abstract: A coupling is disclosed providing fluidic continuity between first and second orifices of two portions of an air circuit which includes a flexible sleeve, a first frame connected in fluid-tight manner to a first end of the flexible sleeve and having a first opening, and a second frame, connected in fluid-tight manner to a second end of the flexible sleeve and having a second opening. The coupling is deformable so that the flexible sleeve may adapt to the variable spacing between two avionics racks and is able to compensate for a misalignment between the orifices of two portions of an air circuit.
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公开(公告)号：US11167838B2
公开(公告)日：2021-11-09
申请号：US16417744
申请日：2019-05-21
Applicant: Airbus Operations (S.A.S.)
Inventor： Bernard Guering , Laurent Saint-Marc
Abstract: A rudder control unit includes a single-piece main module mobile on a curved support frame. The rudder control unit includes a curved support and guide frame to be mounted in a floor of the aircraft, and a unique main module including the pedals and a set of functionalities, the main module configured such that it is movable and positioned on the support and guide frame using a movement unit, thus making it possible to obtain an extremely simplified architecture with a reduced number of pieces.
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公开(公告)号：US10893624B2
公开(公告)日：2021-01-12
申请号：US16173855
申请日：2018-10-29
Applicant: Airbus Operations (S.A.S.)
Inventor： Bernard Guering , Romain Delahaye
Abstract: A supporting structure of optimized volume includes at least two vertical structural elements having a front face and a rear face. Modules including electronic equipment items are fixed onto the front face of the vertical structural elements. Use in particular can be for the integration of avionics modules on aircraft.
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公开(公告)号：US10392096B2
公开(公告)日：2019-08-27
申请号：US15150674
申请日：2016-05-10
Applicant: Airbus Operations S.A.S.
Inventor： Bernard Guering
Abstract: An access device enables controlled or secure communication between different areas of an enclosure, and in the example illustrated in the present application of an aircraft, while providing reduced size. The access device includes a folding door which, when in folded position, allows at least one of said openings to be closed and, when in deployed position, forms a security vestibule with at least one movable shutter allowing said opening created by the deployment of said folding door to be closed. By superimposing the main components of the security vestibule that said components allow to close, the device frees up the adjoining cabin space when the security vestibule is not in use.
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