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1. 发明公开

EP3168133A4 ELASTIC STRUCTURE ANTI-IMPACT FRAME BODY 审中-公开
公开(公告)号：EP3168133A4
公开(公告)日：2018-04-25
申请号：EP15818445
申请日：2015-07-08
申请人： JIANG LIPING
发明人： JIANG LIPING
IPC分类号： B63B43/18 , B63B3/10 , B63B3/14 , B63G9/02
CPC分类号： B63B5/00 , B61D17/00 , B62D21/152 , B63B3/09 , B63B3/10 , B63B5/24 , B63B43/18 , B63B2231/04 , B63B2231/18 , B63B2231/42 , B63B2231/46 , B63B2231/48 , B63B2231/52 , B63B2241/02 , B63G9/02 , B64C1/062 , B64C2001/0072 , B64C2001/0081
摘要： An elastic structure anti-impact frame body for use in ships, automobiles, aircraft, trains, railcars and other moving vehicles, said frame body being a wholly or partially elastic frame, the bearing components constituting the frame body forming an arc-shape or a wave-shaped curve, and the frame body being made of an elastic material. The whole or part of the structure of the elastic structure anti-impact frame body has an elastic deformation function; on the premise that the elastic structure does not affect normal driving or bearing capacity, under the force of an impact on said frame, the frame body will elastically deform within a corresponding safe range, and can cushion and absorb the energy of the impact; the frame body, when releasing the energy of the impact, returns to the original shape, greatly improving the anti-impact security factor.

2. 发明授权

EP2905228B1 Fuselage Airframe and Tank 有权
标题翻译：机身和坦克
公开(公告)号：EP2905228B1
公开(公告)日：2018-01-03
申请号：EP14400007.2
申请日：2014-02-06
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Fink, Axel , Rack, Andreas , Höfer, Philipp
IPC分类号： B64D37/04 , B64D37/06 , B64C1/06 , B64C27/04
CPC分类号： B64C1/061 , B64C1/062 , B64C27/04 , B64D37/04 , B64D37/06 , Y02T50/44
摘要： The invention relates to a fuel tank (19) and a differential frame (3) in a fuselage airframe (1) of a helicopter, the fuel tank (19) being installed between the fuselage lower cover shell (4) and the floor panel (5). The differential frame (3) separates the fuel tank (19) into two individual compartments, the differential frame (3) having a web (15) below the floor panel with a variable-height (23) with a minimum height at the symmetry axis (18) of the fuselage cross-section and a maximum height at lateral frame roots regions (27). A transversal beam (7) is attached at each of its both ends to the differential frame (3) bridging the entire variable-height (23) of the differential frame (3) and the fuel tank (19) with two front and rear fuel bladders (20, 21) covering both individual tank compartments with a middle bladder (22) installed between the transversal beam (7) and the variable-height web (15) of the differential frame (3).

3. 发明公开

EP2457821A3 Compliant panel for aircraft 有权
标题翻译：符合飞机的面板
公开(公告)号：EP2457821A3
公开(公告)日：2017-11-15
申请号：EP12000421.3
申请日：2008-03-06
申请人： The Boeing Company
发明人： Koch, William , Matheson, Donald , Anderson, Barney , Swada, Jeffrey
IPC分类号： B64C1/10 , B64C1/06 , B64C1/12
CPC分类号： B64C1/10 , B64C1/062 , B64C1/12
摘要： A pressurized aircraft having an exterior surface provided by an energy absorbing panel (500), the energy absorbing panel comprising: an interior side (504) subject to the pressure within the aircraft; and an exterior side (502) subject to being struck by an object, the panel being formed of a material that deforms in response to a threshold amount of impact energy caused by an object strike, thereby absorbing and dissipating at least a portion of the impact energy, wherein the interior and exterior sides are formed by opposite facing surfaces of a single monolithic skin and the monolithic skin includes areas of increased thickness (506,508,510,518,520,522).
摘要翻译：一种具有由能量吸收板（500）提供的外表面的加压飞机，所述能量吸收板包括：经受飞机内压力的内侧（504）和受物体撞击的外侧（502），所述面板由响应于由物体撞击引起的阈值量的冲击能量而变形的材料形成，从而吸收和消散至少一部分撞击能量，其中内侧和外侧由单个整体蒙皮的相对表面形成，并且整体蒙皮包括增加厚度的区域（506,508,510,518,520,522）。

4. 发明公开

EP2455285A4 SHOCK ABSORBING STRUCTURE 审中-公开
标题翻译：减震结构
公开(公告)号：EP2455285A4
公开(公告)日：2017-04-05
申请号：EP10799904
申请日：2010-07-15
申请人： MITSUBISHI HEAVY IND LTD
发明人： TANAKA ATSUMI , HIGUCHI NAOKI
IPC分类号： B64D25/00 , B60R19/18 , B64C27/04
CPC分类号： B64C1/062 , B60R19/18 , B64C27/04
摘要： There is a demand for miniaturization of a shock absorbing structure. The shock absorbing stricture is provided with a beam-like structure member having a recess, and a shock absorbing member, one end of which is arranged in the inside of the recess and the other end of which is arranged outside of the recess. As the area of the recess overlaps the place where the structure member supports the structure even at a dead-stroke in which the shock absorbing member is bottomed out, the space inside the recess is not wasted.

5. 发明公开

EP2922752A4 AN AIRFRAME LEADING EDGE 审中-公开
标题翻译： FLUGWERKANSTRÖMKANTE
公开(公告)号：EP2922752A4
公开(公告)日：2017-01-25
申请号：EP12888908
申请日：2012-11-20
申请人： SAAB AB
发明人： NORDIN PONTUS , STRINDBERG GÖTE
IPC分类号： B64C3/28 , B64C1/06 , B64C1/12 , B64C27/473 , B64D45/00 , F01D5/28
CPC分类号： B64C1/062 , B64C1/12 , B64C3/28 , B64D2045/0095

6. 发明授权

EP2881318B1 Aircraft fuselage 有权转让
标题翻译：机身
公开(公告)号：EP2881318B1
公开(公告)日：2016-07-13
申请号：EP14195253.1
申请日：2014-11-27
申请人： Airbus Operations GmbH , AIRBUS DEFENCE AND SPACE GMBH
发明人： Margull, Lars , Waimer, Matthias , Schatrow, Paul , Bergmann, Tim , Heimbs, Sebastian , Bautz, Brian , Siemetzki, Markus
IPC分类号： B64C1/06
CPC分类号： B64C1/062

7. 发明授权

EP2558360B1 LUFTFAHRZEUGRUMPF MIT EINER INTEGRIERTEN ENERGIEAUFNEHMENDEN VERFORMUNGSSTRUKTUR UND LUFTFAHRZEUG MIT EINEM DERARTIGEN RUMPF 有权转让
标题翻译：具有集成能接收成形结构和飞机这样的船体飞机HULL
公开(公告)号：EP2558360B1
公开(公告)日：2016-04-06
申请号：EP11718921.7
申请日：2011-04-09
申请人： Airbus Defence and Space GmbH
发明人： MAYER, Franziskus , MEISNER, Christoph , STARKE, Peter
IPC分类号： B64C1/06
CPC分类号： B64C1/062

8. 发明授权

EP2563651B1 STRUCTURE DE FUSELAGE D'AÉRONEF COMPORTANT UN DISPOSITIF ABSORBEUR D'ÉNERGIE 有权
标题翻译：船体结构SHOCK EQUIPPED
公开(公告)号：EP2563651B1
公开(公告)日：2016-03-23
申请号：EP11716530.8
申请日：2011-04-22
申请人： European Aeronautic Defence And Space Company Eads France
发明人： GUIMARD, Jean-Mathieu , BERMUDEZ, Michel , MESNAGE, Didier
IPC分类号： B64C1/06
CPC分类号： B64C1/062

9. 发明授权

EP2889212B1 Subfloor structure with an integral hull for a rotary wing aircraft 有权
标题翻译： Unterbodenstruktur mit integrierter SchalefüreinDrehflügelflugzeug
公开(公告)号：EP2889212B1
公开(公告)日：2016-01-06
申请号：EP13400042.1
申请日：2013-12-30
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Fink, Axel
IPC分类号： B64C1/06 , B64C27/04
CPC分类号： B64C1/18 , B64C1/062 , B64C1/064 , B64C1/12 , B64C27/04

10. 发明公开

EP2876042A1 Helicopter Airframe 有权
标题翻译： Hubschrauberflugwerk
公开(公告)号：EP2876042A1
公开(公告)日：2015-05-27
申请号：EP13400030.6
申请日：2013-11-20
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Fink, Axel , Steindl, Christoph
IPC分类号： B64C1/06 , B64C1/18
CPC分类号： B64C1/18 , B64C1/062 , B64C27/04 , B64D37/04 , B64D37/06 , Y02T50/44
摘要： The invention relates to a helicopter airframe (2) with a longitudinal axis comprising: a subfloor structure (15) for supporting cabin floor panels (13) and/or at least one fuel tank bladder (12). Said subfloor structure (15) has a bottom shell (16), longitudinal support beams (21), ribs (20), main frames (23) and floor panels (13). The bottom shell (16) has a flat shell portion (17) and two lateral shell portions (18) extending integrally from said flat shell portion (17) along its longitudinally oriented sides and being curved towards respective front edges of said ribs (20) and main frames (23). The longitudinal support beams (21) are provided with attachments for the floor panels (13), the longitudinal support beams (21) are attached at least partially to the ribs (20) and/or the main frames (23) and the longitudinal support beams (21) are featuring along at least 2/3 of their longitudinal extension a height 2 to 20 times smaller than any distances of any of the floor panels (13) to the bottom shell (16).
摘要翻译：本发明涉及一种具有纵向轴线的直升机机身（2），包括：用于支撑舱室地板（13）和/或至少一个燃料箱气囊（12）的地板底板（15）。所述底板结构（15）具有底壳（16），纵向支撑梁（21），肋（20），主框架（23）和地板镶板（13）。底壳（16）具有平坦壳体部分（17）和两个横向外壳部分（18），其从所述平坦壳体部分（17）沿着其纵向定向的侧面整体延伸并且朝向所述肋条（20）的相应前边缘弯曲，和主框架（23）。纵向支撑梁（21）设置有用于地板镶板（13）的附件，纵向支撑梁（21）至少部分地附接到肋（20）和/或主框架（23）和纵向支撑件梁（21）沿其纵向延伸部的至少2/3的特征是比任何地板镶板（13）到底壳（16）的任何距离小2至20倍的高度。

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