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31. 发明专利

JP2001146198A DOOR DEVICE FOR AIRPLANE 失效
公开(公告)号：JP2001146198A
公开(公告)日：2001-05-29
申请号：JP2000308125
申请日：2000-10-06
申请人： EADS AIRBUS GMBH
发明人： PHILIPP RALF , LESSAT WOLFGANG , KALLIES GUENTER
IPC分类号： E05F15/10 , B64C1/14
摘要： PROBLEM TO BE SOLVED: To reduce the manufacturing cost and weight of and ensure easy-to- plan maintenance of a door device for an airplane by reducing the number of kinematic structural elements of a passenger door interior. SOLUTION: An airplane cabin holds a door operating lever 2 placed by a door 1. The door operating lever 2, when operated, releases or operates a safety shaft 4 of a door lock device 5 over a mechanical change range, and after the mechanical locking and unlocking processes, is used as an electric switch 9 for a control and monitor unit. The control and monitor unit provides an electrical regulating signal for a first motor 6 for mechanically unlocking or locking a lift and lock shaft 7 of the door lock device 5 to lift or lower the door 1, and an electrical regulating signal for a second motor 8 for, after the lifting process, turning the door 1 outwardly in parallel with the airplane fuselage and retaining it in an open position, or turning the door 1 inwardly into the airplane fuselage structure to close it.

32. 发明专利

JPH05213277A CARGO LOCKING DEVICE FOR AIRCRAFT 失效
公开(公告)号：JPH05213277A
公开(公告)日：1993-08-24
申请号：JP29881192
申请日：1992-11-09
申请人： AIRBUS GMBH
发明人： RUUTOGAA BOOGENSHIYUTAARU , BERUNTO DANTSUIKU
IPC分类号： B60P7/06 , B64C1/20 , B64D9/00
摘要： PURPOSE: To provide a luggage locking device for an aircraft capable of monitoring a locking state of a luggage at each time. CONSTITUTION: The luggage locking device has an operation of locking a luggage in a range of an aircraft cargo chamber. The device comprises at least a locking element 2 capable of being positioned. The element is relatively movably supported to a frame 3. A sensor 4 connected to a monitoring unit 6 is provided in a range of the frame. The sensor detects at least one locking position capable of discriminating an unlocking position.

33. 发明专利

JPH05159637A CONDUCTIVE CONSTITUENT BODY 失效
公开(公告)号：JPH05159637A
公开(公告)日：1993-06-25
申请号：JP14177792
申请日：1992-06-02
申请人： AIRBUS GMBH
发明人： ZAFUA KIRUMA
IPC分类号： G02B6/44 , H01B11/18 , H01B11/22
摘要： PURPOSE: To provide a conductive structure having at least two independent transmission duct lines by surrounding a photoconductor with an electric conductor, and coaxially installing the same. CONSTITUTION: A photoconductor 2 and an electric conductor 3 are mutually coaxially installed. The photoconductor 2 and the electric conductor 3 are coaxially connected to only one connecting element. The electric conductor 3 surrounds the photoconductor 2. Thereby the high safety, extensive transmission capacity and high mechanical resistance force can be assured.

34. 发明专利

JPH05131991A SUPPORT WALL IN TRANSPORT CABIN OF AIRCRAFT 失效
公开(公告)号：JPH05131991A
公开(公告)日：1993-05-28
申请号：JP12391392
申请日：1992-05-15
申请人： AIRBUS GMBH
发明人： MOHAMAAATO HARARATOOTEERANI
IPC分类号： B64C1/10 , B64C1/22 , B64D9/00
摘要： PURPOSE: To provide a retaining wall for a load of transport cabin in an aircraft securing energy absorption supporting with a cushion. CONSTITUTION: Buffer strips are arranged between two wall plates 2, 3 of each retaining wall. These buffer strips respectively form hollow spring tubes 5 with an elliptical cross-section. The spring tubes 5 having layered constructions 6, 7, 8 are subjected to an impact from a load by supporting with a cushion to absorb energy.

35. 发明专利

JPH04266595A DEVICE FOR SUPPORTING LOAD IN CARGO COMPARTMENT OF AIRCRAFT 失效
公开(公告)号：JPH04266595A
公开(公告)日：1992-09-22
申请号：JP32075691
申请日：1991-12-04
申请人： AIRBUS GMBH
发明人： MOHAMAATO HARARATOOTEERANI
IPC分类号： B64C1/10 , B64C1/22 , B64D9/00
摘要： PURPOSE: To simplify assembly of a support wall and absorb energy by connecting two shock absorbers to an installation rail turnably around a first lateral axis through a holding square bar positioned in between, and supporting a support member for a support wall turnably around a second lateral axis connecting the free ends of bars of the shock absorbers. CONSTITUTION: Two shock absorbers 2, 3 for absorbing energy are fixed to a rail 5 installed on the floor of an aircraft, by bolts 7 through a holding square bar 4, and a support wall is connected to the shock absorbers 2, 3 through a support member 8. The shock absorbers 2, 3 are arranged parallel with each other and turnable in common around a first lateral axis 10. A second lateral axis 11 is provided at the free ends of bars 12, 13 of the shock absorbers 2, 3, and the support member 8 between the bars 12, 13 is turnably held between the shock absorbers 2, 3. The support member 8 is provided with a U-shape receiving part 14 having lateral leg parts 15, 16, and the lower edge part of the support wall is accommodated between the leg parts 15, 16.

36. 发明专利

JPH04226848A DEVICE FOR ADJUSTING AND CLAMPING WORKPIECE 失效
公开(公告)号：JPH04226848A
公开(公告)日：1992-08-17
申请号：JP13303691
申请日：1991-06-04
申请人： AIRBUS GMBH
发明人： UERUNERU BURUNSU , HERUMUUTO AITSUKUHORUSUTO , ENNO UIRUKEN
IPC分类号： B23Q3/02 , B23Q1/03 , B23Q1/54 , B23Q3/08 , B25B11/00
摘要： PURPOSE: To adjust each location of clamp elements for a plate by supporting adjusting elements of a clamp head so as to move each other on a circular flat guide part, disposing a first adjusting element within a guide groove of a substrate and disposing a second adjusting element so as to move on a guide groove of the first adjusting element. CONSTITUTION: A workpiece to be worked is held by negative pressure clamping devices and each negative pressure clamping device is fixed to a substrate. At this time, a clamp head 1 has two adjusting elements 3, 4 and the adjusting elements 3, 4 are supported so as to move each other on circular flat guide parts 10, 11. Further, the first adjusting element 3 is disposed within a guide groove of a substrate 2 and the second adjusting element 4 is disposed so as to move on a guide groove 17 of the first adjusting element 3. These guide grooves 17 intersect and form an intersecting angle of 90 deg. each other.

37. 发明授权

US6434968B2 Cooling air arrangement for a heat exchanger of an aircraft air conditioning unit 有权
标题翻译：飞机空调机组热交换器的冷却空气布置
公开(公告)号：US6434968B2
公开(公告)日：2002-08-20
申请号：US81831001
申请日：2001-03-27
申请人： AIRBUS GMBH
发明人： BUCHHOLZ UWE ALBERT , KELNHOFER JUERGEN
IPC分类号： B64D13/00 , B64D13/08 , F25D9/00 , F25D17/04
CPC分类号： B64D13/08 , B64D13/00
摘要： A cooling air arrangement for an aircraft air conditioning unit includes an air inlet, a heat exchanger, an outlet plenum, first and second air outlet channels branching from the plenum, and a fan arranged in the first outlet channel. During flight of the aircraft, external ram air driven into the air inlet flows primarily through the second outlet channel. During ground operation, the fan primarily sucks cooling air through the first outlet channel, which merges back into the second outlet channel at an air mixing junction that functions as an injector nozzle and a non-return flap valve. The first outlet channel is provided in a spiral housing of the fan, or in a smooth curved duct. The air inlet and outlet of the cooling air arrangement, and the air outlet of the air cycle machine, are oriented in the same direction, e.g. the flight forward direction.
摘要翻译：用于飞机空调单元的冷却空气装置包括空气入口，热交换器，出口增压室，从集气室分支的第一和第二空气出口通道以及布置在第一出口通道中的风扇。在飞行器飞行期间，驱动进入进气口的外部冲压空气主要流经第二出口通道。在地面操作期间，风扇主要通过第一出口通道吸入冷却空气，其在作为喷射器喷嘴和止回阀瓣的空气混合接合处合并回第二出口通道。第一出口通道设置在风扇的螺旋壳体中，或设置在光滑的弯曲管道中。冷却空气装置的空气入口和出口以及空气循环机的空气出口沿相同的方向定向，例如，向前飞行方向。

38. 发明授权

US6389826B2 High capacity air conditioning system with redundant staged recirculation air mixing for an aircraft 有权
标题翻译：大容量空调系统，具有冗余分段循环空气混合的飞机
公开(公告)号：US6389826B2
公开(公告)日：2002-05-21
申请号：US80248801
申请日：2001-03-08
申请人： AIRBUS GMBH
发明人： BUCHHOLZ UWE ALBERT , SCHERER THOMAS
IPC分类号： B64D13/02 , B64D13/04 , B64D13/06 , B64D13/08 , F25B9/00 , F28B9/00 , B64D13/00 , F24F3/00 , F25D21/00
CPC分类号： B64D13/06 , B64D2013/064 , B64D2013/0688 , Y02T50/56
摘要： In an air conditioning system for an aircraft, two pre-mixing units respectively mix cold air from two air conditioning units with recirculated fuselage interior air from two recirculation units, to prepare two pre-mixed air flows that are both directed into and mixed together in a common air distribution mixing chamber, from which mixed air distribution lines branch off to respectively associated separate air conditioning zones within the fuselage. Post-mixing units are respectively interposed in the mixed air distribution lines and respectively mix additional quantities of recirculated fuselage interior air into the mixed air distribution lines. Thereby, the admixture of recirculated air is divided into at least two stages, the system provides redundant failure tolerant operation, and the danger of ice formation in the air lines is reliably prevented even while the air conditioning units provide cold air at a temperature below the water freezing point.
摘要翻译：在用于飞机的空调系统中，两个预混合单元分别将来自两个空调单元的冷空气与来自两个再循环单元的再循环的机身内部空气混合，以制备两个预混合空气流，两个预混合空气流被引导并混合在一起共同的空气分配混合室，混合空气分配管线从该分配混合室分支到机身内的分别相关联的分离的空调区域。后混合单元分别插入混合空气分配管线中，并将额外量的再循环的机身内部空气混合到混合空气分配管线中。因此，再循环空气的混合物分为至少两个阶段，该系统提供冗余的容错操作，并且即使在空调单元提供低于水凝固点。

39. 发明申请

US20010054228A1 Method and apparatus for assembling a three-dimensional structural component 有权
标题翻译：用于组装三维结构部件的方法和装置
公开(公告)号：US20010054228A1
公开(公告)日：2001-12-27
申请号：US09919388
申请日：2001-07-31
申请人： DaimlerChrysler Aerospace Airbus GmbH
发明人： Joachim Lehmker , Karl-Heinz Muehlnickel , Udo-Henning Stoewer , Ruediger Vollmerhaus
IPC分类号： B23P021/00
CPC分类号： B64F5/10 , B21J15/10 , B21J15/142 , B23P19/04 , B23P2700/01 , B64C1/068 , B64C2001/0027 , Y10T29/49622 , Y10T29/49778 , Y10T29/4978 , Y10T29/4981 , Y10T29/49899 , Y10T29/49901 , Y10T29/49904 , Y10T29/49998 , Y10T29/5177 , Y10T29/53004 , Y10T29/53061 , Y10T29/53091 , Y10T29/53313 , Y10T29/53957 , Y10T29/53961
摘要： Three-dimensional large scale bodies such as jumbo aircraft fuselages (14) are assembled in body sections around a central longitudinal assembly core (1) which itself is mounted at its ends and accessible all around along its length. Robots carrying tools for holding, transporting and precisely positioning preassembled wall shell sections, are movable along the central core (1). First, at least one floor grid (2 or 3) is releasably mounted to the core. Then, side wall shell sections (4, 5) are secured to the floor grids. Then, top and bottom wall shell sections (10, 8) are secured to the side wall shell sections (4, 5) to form a body section (BS) of the large scale body (14). Neighboring body sections are secured to each other along cross-seams. Upon completion, the floor grids are released from the core (1) and the core is removed preferably withdrawn longitudinally from the assembled large component or body.
摘要翻译：三维大型机体如巨型飞机机身（14）组装在中央纵向组件芯（1）周围的主体部分中，中心纵向组件芯（1）本身安装在其端部，并沿着其长度可以全方位访问。携带用于保持，运输和精确定位预组装的壁壳部分的机器人可沿着中心芯（1）移动。首先，至少一个地板格栅（2或3）可释放地安装到芯部。然后，侧壁壳体部分（4,5）固定到地板网格上。然后，顶壁和底壁壳体部分（10,8）固定到侧壁壳体部分（4,5）上以形成大型机体（14）的主体部分（BS）。相邻的主体部分沿着交叉接缝彼此固定。完成后，地板网格从芯部（1）中释放出来，并且芯部被优选地从组装的大部件或主体纵向取出。

40. 发明申请

WO2009095306A9 VARIABLE SEAT SEPARATION ADJUSTMENT IN AN AIRPLANE 审中-公开
标题翻译：平面上的可变座椅距离调整
公开(公告)号：WO2009095306A9
公开(公告)日：2009-09-24
申请号：PCT/EP2009050404
申请日：2009-01-15
申请人： AIRBUS GMBH , GONNSEN JOHANNES , GAERTNER JENS
发明人： GONNSEN JOHANNES , GAERTNER JENS
IPC分类号： B64D11/06
CPC分类号： B64D11/00 , B64D11/00155 , B64D11/06 , B64D11/0601 , B64D11/064
摘要： According to an exemplary embodiment of the invention, a system for the simultaneous longitudinal movement of a plurality of selected seats or seat rows in an airplane is provided, a drive device being provided to move the seats, wherein the movement of the seats is done according to a change in a seating space configuration plan.
摘要翻译：根据本发明，用于在飞机的若干选择的座椅或座椅排同时纵向移位一个系统，其中的驱动装置被提供用于移动所述座椅的实施例，其特征在于，根据在座位配置规划的改变座椅的位移来完成。

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