公开(公告)号：US12012199B2

公开(公告)日：2024-06-18

申请号：US17536726

申请日：2021-11-29

申请人： The Boeing Company

发明人： Daren Evans ,  Nick A. Kovaltchouk ,  Joshua R. Holcomb

IPC分类号： B64C1/14

CPC分类号： B64C1/1476

摘要： A windshield assembly comprises a support panel, a windshield, and a frame, surrounding the windshield. The frame comprises a frame inboard leg, which is in contact with an inboard windshield surface. A hinge pivotally couples a frame-inboard-leg top portion of the frame inboard leg to the support panel and has a pivot axis. A channel is provided in the support panel. At least a portion of the frame-inboard-leg bottom portion, at least a portion of the frame-inboard-leg first lateral portion, and at least a portion of the frame-inboard-leg second lateral portion are located in the channel. The channel comprises a channel base leg. A seal is located in the channel between the channel base leg and the frame inboard leg.

公开(公告)号：US11767096B2

公开(公告)日：2023-09-26

申请号：US17530607

申请日：2021-11-19

申请人： THE BOEING COMPANY

发明人： Matthew W. Walter

IPC分类号： B64C1/32 ,  B64C1/14

CPC分类号： B64C1/32 ,  B64C1/1476

摘要： A system for initiating a canopy release signal for a canopy of an aircraft includes a first striker secured to the canopy, and a first initiator assembly secured to a fuselage of the aircraft. The first initiator assembly has a protrusion. The first striker is configured to be rotated against the protrusion of the first initiator assembly. The canopy release signal is output in response to the first striker rotating against the protrusion of the first initiator assembly.

公开(公告)号：US20190185132A1

公开(公告)日：2019-06-20

申请号：US16221028

申请日：2018-12-14

申请人： Airbus Operations SAS

发明人： Bernard GUERING ,  Romain DELAHAYE

IPC分类号： B64C1/14 ,  B64C1/06

CPC分类号： B64C1/1476 ,  B64C1/061 ,  B64C2001/0045 ,  B64D2011/0061

摘要： A nose section of an aircraft comprising a centered flight deck, making it possible to offer a direct forward field of view towards the outside of the aircraft, the forward visibility of the pilot towards the outside taking priority, and an indirect lateral field of view afforded by image displays displaying images representing the lateral environment of the centered pilot and obtained from an image capturing device.

公开(公告)号：US20180258691A1

公开(公告)日：2018-09-13

申请号：US15595222

申请日：2017-05-15

申请人： Textron Aviation Inc.

发明人： Cody Thomas Baggett ,  Michael Carl Dextradeur

IPC分类号： E06B9/303 ,  E06B9/327 ,  E06B9/323 ,  B64C1/14

CPC分类号： E06B9/322 ,  B64C1/1476 ,  B64C1/1484 ,  E06B9/264 ,  E06B9/307 ,  E06B9/327 ,  E06B9/388 ,  E06B2009/2643 ,  E06B2009/3222

摘要： Embodiments of the present disclosure include an enclosed venetian-blind shade for a window having a plurality of blinds with an adjustable pitch, a transparent pane and a reveal arranged in front of the blinds that enclose one side of the blinds, and a handle assembly to move and secure the blinds in place. An aircraft window shade includes a plurality of blinds coupled to a wire loop, a drive shaft with a gear coupled to the wire loop, and a rotatable dial that interconnects with the gear such that rotation of the dial alters a pitch of the blinds. A window shade system for directing and blocking light from an aircraft window includes a plurality of blinds coupled to a pulley assembly for adjusting a pitch of the blinds, a handle assembly for raising/lowering the blinds, and a carriage assembly for securing the blinds.

公开(公告)号：US10063047B2

公开(公告)日：2018-08-28

申请号：US14633392

申请日：2015-02-27

申请人： PPG INDUSTRIES OHIO, INC.

发明人： Nicolas B. Duarte ,  Yu Jiao ,  Khushroo H. Lakdawala ,  Arthur C. Scott ,  Monroe A. Stone

IPC分类号： H05B1/02 ,  H02H9/02 ,  B64D15/12 ,  B64C1/14 ,  H05B3/86

CPC分类号： H02H9/02 ,  B64C1/1476 ,  B64D15/12 ,  H05B1/0236 ,  H05B3/86 ,  H05B2203/016 ,  H05B2203/035

摘要： A system for monitoring performance of an aircraft windshield includes a sensor comprising a sensory contact and an evaluation unit. The sensory contact is in physical contact with one or more components of the windshield, and generates a signal representative of the performance of the component(s) of the windshield. An electrical connector is secured to the surface of the windshield facing the interior of the aircraft. The signal from the sensory contact passes through the connector to the evaluation unit. The evaluation unit acts on the signal to determine the performance of the component(s) of the windshield, wherein the evaluation unit is spaced from and out of physical contact with the windshield and the electrical connector, and is in electrical contact with the electrical connector.

公开(公告)号：US20180136733A1

公开(公告)日：2018-05-17

申请号：US15353374

申请日：2016-11-16

申请人： THE BOEING COMPANY

发明人： James P. Schalla ,  Calsee N. Robb ,  William A. Harkness ,  Buddy L. Sharpe ,  Heidi J. Kneller

IPC分类号： G06F3/01 ,  G06K9/00 ,  B64D13/00 ,  B64D11/00 ,  B64D47/02 ,  B64C1/14

CPC分类号： G06F3/017 ,  B64C1/1476 ,  B64D11/0015 ,  B64D13/00 ,  B64D47/02 ,  B64D2011/0053 ,  B64D2013/003 ,  G06F3/0304 ,  G06K9/00355

摘要： An aircraft is provided that includes a passenger service unit for a passenger seated in a seat in its cabin. The aircraft includes a camera configured to acquire an image of the passenger, and a control module configured to at least receive the image of the passenger. The control module is configured to receive non-tactile gesture preference data and dominant hand data, and access a non-tactile gesture data store that includes a plurality of images of non-tactile hand signals or non-tactile hand gestures. Based on the foregoing, the control module is configured to generate non-tactile gesture data in accordance with and indicative of a non-tactile hand signal or a non-tactile gesture made by the passenger. And the control module is configured to control one or more cabin systems including in at least one instance the passenger service unit based on the non-tactile gesture data.

公开(公告)号：US20170363001A1

公开(公告)日：2017-12-21

申请号：US15185027

申请日：2016-06-17

申请人： MARVIN HILL

发明人： MARVIN HILL

IPC分类号： F02C7/055 ,  B64C1/14 ,  B64D33/02

CPC分类号： F02C7/055 ,  B64C1/1476 ,  B64D33/02 ,  B64D45/00 ,  B64D2033/022

摘要： The present invention relates to aircraft engine shield placed over the front of the jet turbines and across the wind shield, made up of heavy duty metal or other suitable material to prevent bird strikes, having small air gaps which not only prevents birds from entry but also prevents any other external particle either small or large to enter the wind shield or front turbines which in turn protects the air craft from any problem,

公开(公告)号：US20170073086A1

公开(公告)日：2017-03-16

申请号：US15264913

申请日：2016-09-14

申请人： Airbus Operations S.A.S.

发明人： Phillip Vigneau

IPC分类号： B64F5/00 ,  F16B47/00

CPC分类号： F16B47/00 ,  B64C1/14 ,  B64C1/1476 ,  B64F1/005 ,  B64F5/50 ,  B64F5/60

摘要： A shutter for masking a surface allowing radiation, to pass at least partially. includes a panel and a skirt forming, with the panel, an enclosure which, when applied to the surface, prevents the passage of at least a determined radiation, and at least one partial vacuum-based fixing system for temporarily fixing the enclosure onto said surface to which it is intended to be applied. The fixing system includes at least one vacuum pump fixed onto the panel in such a way as to be able to be handled from the outside of said enclosure and to create the vacuum in at least one sucker fixed onto the panel on the side of said enclosure, and the dome of which is turned toward the outside of the enclosure. The vacuum pump has a handle having a pushbutton making it possible, each time it is pressed, to suck air into the sucker or suckers.

摘要翻译： 用于遮蔽允许辐射的表面的快门至少部分地通过。 包括面板和裙部，其与所述面板形成为当应用于所述表面时防止至少确定的辐射通过的外壳以及用于将所述外壳临时固定到所述表面上的至少一个部分真空基固定系统 其意图应用于其中。 固定系统包括固定在面板上的至少一个真空泵，以便能够从所述外壳的外部处理并在固定到所述外壳的侧面上的面板上的至少一个吸盘中产生真空 ，其圆顶转向外壳的外部。 真空泵具有手柄，其具有按钮，每次按压时可以将空气吸入吸盘或吸盘。

公开(公告)号：US20160236766A1

公开(公告)日：2016-08-18

申请号：US14977941

申请日：2015-12-22

申请人： MITSUBISHI AIRCRAFT CORPORATION

发明人： Taketoshi YAMAURA ,  Katsuya KITAZUME ,  Masaki HASHIMOTO

IPC分类号： B64C1/14 ,  B64D45/02

CPC分类号： B64C1/1492 ,  B64C1/14 ,  B64C1/1476 ,  B64D15/12 ,  B64D45/02 ,  H05B3/84 ,  H05B2203/002 ,  H05B2203/013

摘要： The present invention provides a windshield of an aircraft, including a plurality of conductive members that are disposed along an in-plane direction of the windshield, and are wire-connected together, wherein the plurality of conductive members are heaters that generate heat when supplied with an alternating current, and the conductive members are wire-connected such that induced currents induced in the respective conductive members by a magnetic field in association with a lightning current are circulated between the conductive members.

摘要翻译： 本发明提供了一种飞机的挡风玻璃，其包括沿着挡风玻璃的面内方向设置的多个导电构件，并且线连接在一起，其中多个导电构件是当被供应时产生热量的加热器 交流电，并且导电构件被引线连接，使得在导电构件之间循环通过与雷电电流相关联的磁场在各个导电构件中感应的感应电流。

公开(公告)号：US09387919B2

公开(公告)日：2016-07-12

申请号：US13628145

申请日：2012-09-27

申请人： Airbus Operations (SAS)

发明人： Bernard Guering

IPC分类号： B64C1/06 ,  B64C1/14

CPC分类号： B64C1/061 ,  B64C1/1476

摘要： An aircraft nose structure comprising frames (2, 4, 6), a lower windshield frame member (12) and an upper windshield frame member (14) which are adapted to receive a windshield. The lower windshield frame member (12) has an arcuate shape with two branches which are connected together by a tie-rod (26).

摘要翻译： 一种飞机鼻梁结构，其包括适于接收挡风玻璃的框架（2,4,6），下部挡风玻璃框架构件（12）和上部挡风玻璃框架构件（14）。 下挡风玻璃框架构件（12）具有弓形形状，其中两个分支通过连杆（26）连接在一起。