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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
摘要： 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
CPC分类号： B64C1/10 , B64C1/068 , B64C1/14 , B64C1/1415 , B64C1/22 , B64D11/00 , B64D11/0015 , B64D43/00
摘要： 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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公开(公告)号：US11407515B2
公开(公告)日：2022-08-09
申请号：US16524689
申请日：2019-07-29
摘要： To facilitate assembly of an aircraft cockpit, a cockpit module includes an instrument panel to support at least one screen and an air conditioning distribution block bordering the instrument panel and integral with a rear face of it. The air conditioning distribution block includes an air distributor, an excess air collector, and air distribution channels each including a first end communicating with the air distributor and a second end communicating with the excess air collector, each distribution channel being equipped with an air outlet arranged between its first and second ends.
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公开(公告)号：US20180370655A1
公开(公告)日：2018-12-27
申请号：US16014629
申请日：2018-06-21
摘要： A tool for transporting and installing an insulation blanket in a single piece on a component, for example of an aircraft. The component can have a double-curvature surface like a sealed back which makes the installation difficult given the planar nature of the blanket. The transporting and installing tool operates like an umbrella without fabric at which the ribs are provided with removable attachment devices allowing removable fixing to the insulation blanket. The tool is simple and easy to handle for rapid installation that can be carried out by a single operator.
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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
IPC分类号： B64D13/06 , F16L25/00 , F16L27/11 , F16L27/107 , H05K7/20
摘要： 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
摘要： 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：US11542010B2
公开(公告)日：2023-01-03
申请号：US16703733
申请日：2019-12-04
摘要： An aircraft portion having a floor and a fuselage structure forming an arch above the floor is disclosed in which a monument is mounted within the fuselage. The monument is suspended from the fuselage structure by at least one suspension point, so that most of the weight of the monument is taken up by the fuselage structure. The monument includes a circular or a round section configured to take up the vertical forces than the horizontal floor, which bends under vertical loads.
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公开(公告)号：US10899451B2
公开(公告)日：2021-01-26
申请号：US15986068
申请日：2018-05-22
摘要： An aircraft is disclosed having a lifting body housing a passenger cabin including a forward portion bounded laterally by at least one portion of a leading edge of the lifting body. The passenger cabin includes at least one lateral luggage storage device housed in the concavity formed by the leading edge portion and includes an opening towards the interior of the passenger cabin.
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公开(公告)号：US10822073B2
公开(公告)日：2020-11-03
申请号：US15377646
申请日：2016-12-13
摘要： An aircraft control comprises a mobile pedal and comprises a cylinder coupled to the pedal such that a displacement of the pedal according to at least a first direction reduces the volume of a first chamber of the cylinder. A control device comprises a fluid type bus system connecting two aircraft controls. Additionally, an aircraft is equipped with such a control device.
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公开(公告)号：US20190300140A1
公开(公告)日：2019-10-03
申请号：US16363543
申请日：2019-03-25
摘要： Attempts are increasingly being made to optimize space in the flight decks of aircraft to reduce the overall volume thereof with a view to increasing that of the profit-making zones such as the cabin. To this end, the present disclosure relates to a nose section of an aircraft including a cockpit separated from a cabin by a bulkhead. The bulkhead includes a recess projecting from the surface of the bulkhead on the cabin side, laterally offering hollow zones closed by at least one closure wall to create at least one storage compartment. The volume gained in the cabin allows for the storage of cockpit equipment, thus allowing cockpit volume to be optimized.
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