公开(公告)号：EP2907744B1

公开(公告)日：2016-11-23

申请号：EP14400009.8

申请日：2014-02-18

申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH

发明人： Markmiller, Johannes

IPC分类号： B64C1/14 ,  B61C17/04 ,  B62K27/16 ,  B61D25/00 ,  B63B19/02 ,  B60J1/02 ,  B62J17/04

CPC分类号： B64C1/1492 ,  B60J1/004 ,  B60J1/007 ,  B62J17/04 ,  B63B19/02 ,  B64C27/04

公开(公告)号：EP3024720A4

公开(公告)日：2016-08-10

申请号：EP14829597

申请日：2014-07-25

申请人： GENTEX CORP

发明人： DRISCOLL DAVID I ,  BUSSCHER BRADLEY L ,  ASH KEVIN L ,  LEVESQUE ANDREW J ,  TEUNE JAMES E ,  KEMPERMAN CHRISTIAN M ,  THEISTE DAVID A ,  MITCHELL ANDREW T

IPC分类号： B64C1/14 ,  B60J3/04 ,  G02F1/153

CPC分类号： B64C1/1492 ,  B60R1/088 ,  B64C1/14 ,  B64C1/1484 ,  G02F1/15 ,  G02F1/153 ,  G02F1/1533 ,  H05K9/0005 ,  Y10T29/49826

摘要： An aircraft window foam mounting assembly having an exterior pressure pane frame including an inner surface and an outer surface. A pressure pane is in abutting contact with the inner surface of the exterior pressure pane frame. A foam bezel is proximate a periphery of the pressure pane and defines an inner opening. The foam bezel includes an inner wall and an outer wall. The inner wall includes a channel. An electrochromic element is disposed in the opening and is configured for reception in the channel of the inner wall. An electrically conductive member is operably coupled to the foam bezel and extends from the inner wall to the outer wall.

公开(公告)号：EP3003855A1

公开(公告)日：2016-04-13

申请号：EP14807595.5

申请日：2014-05-29

申请人： Honda Patents & Technologies North America, LLC

发明人： KONDO, Junichi

IPC分类号： B64C1/14

CPC分类号： B64C1/1492 ,  B63B19/02 ,  B63B2019/0038 ,  B64C1/1484 ,  B64G1/22 ,  B64G1/60 ,  F16B5/02 ,  F16B19/02

摘要： A fastening assembly for a window of a pressurized fuselage of an aircraft includes a fastener received through a mounting hole defined in the window, an edge attachment member fixing the window to the fuselage, and a bushing assembly embedded in the mounting hole. The bushing assembly includes an inner sleeve bushing radially interposed between the fastener and the window and an outer sleeve bushing radially interposed between the inner sleeve bushing and the window. The inner sleeve bushing is formed from relatively less rigid metal compared with metal of the fastener and the outer sleeve bushing is formed from relatively rigid metal compared with material of the window and the metal of the inner sleeve bushing.

公开(公告)号：EP2993125A8

公开(公告)日：2016-04-13

申请号：EP14183457.2

申请日：2014-09-03

申请人： Airbus Operations GmbH

发明人： Knijnenburg, Thorsten, Dipl.-Ing. ,  Poth, Albin, Dipl.-Ing.

IPC分类号： B64C1/14 ,  B64D13/04

CPC分类号： G01L13/06 ,  B64C1/1492 ,  B64D13/04 ,  G01L19/143 ,  Y02T50/44

摘要： The present invention relates to a system for detecting a pressure difference between the interior (8) of a cabin of an aircraft and the exterior (7) of the aircraft. The system (1) comprises a window arrangement (3), which comprises a first windowpane (4) having a first surface (4a) and an opposite second surface (4b) and is adapted to be mounted in an aircraft such that the first surface (4a) of the first windowpane (4) is facing towards the exterior (7) of the aircraft and is subjected to the ambient atmospheric pressure and the second surface (4b) faces towards the interior (8) of a cabin of the aircraft, and a pressure sensor (10) comprising a first pressure port (13). The first windowpane (4) comprises a first air passage opening (11) extending between the first and second surfaces (4a, 4b) of the first windowpane (4), and the pressure sensor (10) is sealingly connected to the first air passage opening (11) such that the first pressure port (13) of the pressure sensor (10) is subjected to pressure acting on the first surface (4a) of the first windowpane (4).

公开(公告)号：EP2740662A3

公开(公告)日：2015-11-11

申请号：EP13195305.1

申请日：2013-12-02

申请人： Airbus Operations

发明人： Dazet, Francis

IPC分类号： B64C1/14

CPC分类号： B64C1/1492

摘要： Cette verrière d'aéronef comprenant au moins une glace (1), un encadrement (4) contre lequel ladite glace est en appui, au moins une bride (5) de serrage de ladite glace contre ledit encadrement, et au moins une cavité (6) délimitée entre ladite glace, ledit encadrement et ladite bride.
Un profilé (7) remplit sensiblement ladite cavité (6) et présente sur au moins une partie de sa périphérie des reliefs (9, 10) en forme de cannelures qui définissent avec une surface en regard des chicanes formant joint.

公开(公告)号：EP2665395A4

公开(公告)日：2015-10-14

申请号：EP12734318

申请日：2012-01-13

申请人： AEROSPACE TECHNOLOGIES GROUP INC

发明人： KNOWLES BYRON R

IPC分类号： A47H5/032 ,  B64C1/14 ,  E06B9/262 ,  E06B9/327 ,  E06B9/74

CPC分类号： A47H5/0325 ,  B64C1/1492 ,  E06B9/262 ,  E06B9/327 ,  E06B9/74 ,  E06B2009/2625

公开(公告)号：EP2879951A2

公开(公告)日：2015-06-10

申请号：EP13745762.8

申请日：2013-07-25

申请人： PPG Industries Ohio, Inc.

发明人： JIAO, Yu ,  DUARTE, Nicolas ,  STONE, Monroe A.

IPC分类号： B64C1/14

CPC分类号： B64C1/1484 ,  B64C1/1476 ,  B64C1/1492 ,  B64D2045/0085

摘要： A network system for monitoring and storing data of aircraft intelligent windows or windshields to provide useable life of, provide real life performance of, and/or measure characteristics and/or properties of, the windshields forwards the data from sensors mounting the windshield to a window sensing hub having a microprocessor programed to receive and process the data to determine the performance of the windshield and formatting the data in accordance to a preset program, wherein the program includes providing data from the sensors that measures characteristics and properties of the windshield that are active during the period in which the data is taken. An aircraft central maintenance system connected to the window sensing hub receives the formatted information from the window sensing hub and unfiltered or unformatted information, wherein the unfiltered information from the windshield is acted on by the central maintenance system to provide an estimated useable life of the windshield.

公开(公告)号：EP2562078A4

公开(公告)日：2014-09-24

申请号：EP11771694

申请日：2011-01-24

申请人： MITSUBISHI AIRCRAFT CORP

发明人： YOKOI TAKASHI

IPC分类号： B64C1/14 ,  C03C27/12

CPC分类号： B64C1/1492 ,  B32B17/10045 ,  B32B17/10174 ,  B32B17/10293 ,  B32B17/10761 ,  B32B17/1077 ,  B32B27/308 ,  B32B2250/02 ,  B64C1/1476

公开(公告)号：EP1481892B2

公开(公告)日：2014-07-09

申请号：EP04076364.1

申请日：2004-05-06

申请人： The Boeing Company

发明人： Wood, Jeffrey H. ,  Sewell, Terry A.

IPC分类号： B64C1/14

CPC分类号： B64C1/1492

公开(公告)号：EP2740662A2

公开(公告)日：2014-06-11

申请号：EP13195305.1

申请日：2013-12-02

申请人： Airbus Operations

发明人： Dazet, Francis

IPC分类号： B64C1/14

CPC分类号： B64C1/1492

摘要： Cette verrière d'aéronef comprenant au moins une glace (1), un encadrement (4) contre lequel ladite glace est en appui, au moins une bride (5) de serrage de ladite glace contre ledit encadrement, et au moins une cavité (6) délimitée entre ladite glace, ledit encadrement et ladite bride.
Un profilé (7) remplit sensiblement ladite cavité (6) et présente sur au moins une partie de sa périphérie des reliefs (9, 10) en forme de cannelures qui définissent avec une surface en regard des chicanes formant joint.

摘要翻译： 盖子具有窗口（1）和窗口支撑的框架（4）。 安装支架（5）用于将窗户紧靠框架。 空腔（6）在窗，框架和支架之间界定。 一组金属形部分（7）适于大致填充空腔。 该组部分在其周边的一部分上呈现一组浮雕，例如纵向挡板（9,10）。 该组部分限定了与形成纵向挡板的密封件相对的表面。 这些部分由合成材料制成。