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1. 发明授权

US4537374A Structural supports and aircraft landing gears including such supports 失效
标题翻译：结构支撑和飞机起落架包括这种支架
公开(公告)号：US4537374A
公开(公告)日：1985-08-27
申请号：US405647
申请日：1982-08-05
申请人： Pierre Barnoin , Jacques M. N. Mens , Gilbert Merle
发明人： Pierre Barnoin , Jacques M. N. Mens , Gilbert Merle
IPC分类号： B64C25/58 , B64C25/60 , F16F7/12
CPC分类号： B64C25/60 , F16F7/125
摘要： A structural support comprises inner and outer elements which are telescopingly engaged, a cage secured to the inner element and having apertures in which balls are disposed which are disposed radially between the two elements, and a frangible connection securing the two elements against relative axial movement. In the locked relative positions of the elements, the outer element has locally an increased internal diameter portion and the balls are radially disposed in this position or are moved into the portion on being subjected to an axial force which breaks the frangible connection, so that the relative axial movement of the elements results in the ball plastically deforming the outer element and absorbing energy from the force to protect the body carried by the support. The support can be used to provide a brace operating as a strut and/or a tie, or a shock absorber, or, by mounting a damping piston slidably in the inner tubular element can provide a shock absorbing piston and cylinder unit. The outer tubular element may itself form an external cylinder or may be a liner in an external cylinder.
摘要翻译：结构支撑件包括可伸缩地接合的内部和外部元件，固定到内部元件的笼，并且具有设置在其中径向位于两个元件之间的球的孔，以及将两个元件抵抗相对轴向移动的易碎连接。在元件的锁定的相对位置中，外部元件具有局部增加的内径部分，并且球径向地设置在该位置或者在经受破坏易碎连接的轴向力的部分中移动到该部分中，使得元件的相对轴向运动导致球塑性地使外部元件变形并且从力吸收能量以保护由支撑件承载的身体。支撑件可用于提供作为支柱和/或连接件或减震器操作的支架，或者通过可滑动地安装在内部管状元件中的阻尼活塞可以提供减震活塞和气缸单元。外部管状元件本身可以形成外部圆筒，或者可以是外部圆筒中的衬套。

2. 发明授权

US4558837A Skid landing gear provided with components having a device for absorbing energy by plastic deformation and/or for limiting stress, and components of this type 失效
标题翻译：提供具有通过塑性变形吸收能量和/或限制应力的装置的组件的这种类型的组件
公开(公告)号：US4558837A
公开(公告)日：1985-12-17
申请号：US559549
申请日：1983-12-08
申请人： Jacques M. N. Mens , Pierre Barnoin , Michel J. L. Martin
发明人： Jacques M. N. Mens , Pierre Barnoin , Michel J. L. Martin
IPC分类号： B64C25/52 , B64C27/33
CPC分类号： B64C25/00 , B64C25/52 , B64C2025/325
摘要： Skid landing gear provided with components having a device for absorbing energy by plastic deformation and/or for limiting stress, and components of this type.According to the invention, each of two undercarriage parts comprises a skid 170 connected to the structure to two crosspieces 175 and 176 that are hinged on the structure about an axis parallel to the hinge axis on the structure of the other crosspiece of the same undercarriage part, and at least one component 181 that has a main mechanical and/or hydraulic function, such as a strut, a cross-bracing or control jack, a shock absorber or a shock absorber jack, the component being provided with a device for absorbing energy by plastic deformation and/or for limiting stress, and is connected on the one hand to a crosspiece 176 of the respective undercarriage part and on the other hand either to the corresponding skid 170 or to the structure of the aerodyne.The invention is especially suited to use on helicopters.
摘要翻译：提供具有通过塑性变形吸收能量和/或限制应力的装置的组件的这种类型的组件。根据本发明，两个底架部件中的每一个包括连接到两个横梁175和176的结构的滑动件170，该两个横梁175和176围绕平行于铰链轴线的轴线铰接在同一起落架部件的另一横梁的结构上以及具有主要机械和/或液压功能的至少一个部件181，例如支柱，交叉支撑或控制千斤顶，减震器或减震器千斤顶，该部件设置有用于吸收能量的装置通过塑性变形和/或限制应力，并且一方面连接到相应起落架部分的横档176，或者另一方面连接到相应的滑块170或与空气的结构。本发明特别适用于直升机。

3. 发明授权

US4473203A Disengageable control column for a copilot of an aircraft 失效
标题翻译：飞机副驾驶失控控制栏
公开(公告)号：US4473203A
公开(公告)日：1984-09-25
申请号：US482172
申请日：1983-04-05
申请人： Pierre Barnoin , Jacques M. Cas
发明人： Pierre Barnoin , Jacques M. Cas
IPC分类号： B64C13/12 , G05G9/047 , G05G11/00 , B64C13/14
CPC分类号： B64C13/12 , G05G11/00 , G05G9/047 , G05G2009/04718 , Y10T74/20213 , Y10T74/20636
摘要： The invention relates to a control column (2) for a copilot of an aircraft, coupled for control of roll and pitch by a linkage (5) to the pilot's control column (1). This linkage comprises two parallel rods (6,7) pivoted on the one hand to the column (1) and on the other hand to a member (13) connected to the column (2) by a double universal joint (14, 17). When operative, the column (2) is locked to the member (13) by a lock bolt (19). This control column can be put out of action by releasing the said bolt and can be secured by hooking to a fixed point, in which case the double universal joint (14, 17) ensures its disconnection from the column (1) and thus prevents any misoperation.
摘要翻译：本发明涉及一种用于飞机的副驾驶的控制柱（2），其通过联动装置（5）与飞行员的控制塔（1）联接以控制滚动和俯仰。该联动装置包括两个平行的杆（6,7），一方面枢转到柱（1），另一方面由两个万向节（14,17）连接到柱（2）的构件（13）。当操作时，柱（2）通过锁定螺栓（19）锁定到构件（13）。该控制柱可以通过释放所述螺栓而失去作用，并且可以通过钩住固定点来固定，在这种情况下，双万向接头（14,17）确保其与柱（1）断开，从而防止任何误操作

4. 发明授权

US4053126A Helicopter cabin and method of making same 失效
标题翻译：直升机舱及其制造方法
公开(公告)号：US4053126A
公开(公告)日：1977-10-11
申请号：US633439
申请日：1975-11-19
申请人： Maurice Louis Duret , Pierre Barnoin
发明人： Maurice Louis Duret , Pierre Barnoin
IPC分类号： B29C41/00 , B22D13/02 , B29B7/00 , B29C31/00 , B29C33/04 , B29C39/00 , B29C39/10 , B29C39/26 , B29C41/04 , B29C41/06 , B29C41/20 , B29C41/46 , B29C70/26 , B29C70/70 , B29C70/74 , B64C1/00 , B64C1/12 , B64C27/04 , B29D3/00 , B29C5/04
CPC分类号： B29C70/742 , B29C33/04 , B29C41/20 , B29C41/46 , B29C70/26 , B29C70/70 , B64C1/00 , B29C41/04 , B29L2031/3085 , B29L2031/3088 , B64C2001/0072 , B64C27/04 , Y02T50/433
摘要： The present invention relates to a process for making a thin-walled composite structure having resistance profiled elements, wherein a rotational-moulding mould is made, in the shape of said structure, then resistant profiled elements made of heat-conductive material are positioned in said mould, in order to form a main resistant frame-work for said structure, after which a suitable synthetic material is introduced into the mould and the known operations of rotational moulding are carried out. The structure thus produced may be used for the construction of aerodynes, and in particular in helicopter construction.

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