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1. 发明申请

US20100327110A1 GUIDING SYSTEM FOR AIRCRAFT NACELLE MAINTENANCE 有权
标题翻译：飞机维修指导系统
公开(公告)号：US20100327110A1
公开(公告)日：2010-12-30
申请号：US12864925
申请日：2009-01-21
申请人： Pierre Caruel , Jean-Philippe Joret , Peter Segat
发明人： Pierre Caruel , Jean-Philippe Joret , Peter Segat
IPC分类号： B64D27/12 , F01D25/24 , F02K9/00
CPC分类号： B64D29/08
摘要： The invention relates to a nacelle (100) for the turbojet of an aircraft that comprises a downstream structure including: an outer structure (106), a concentric inner structure (109) surrounding a downstream portion (111) of the turbojet and including an upstream section having a relatively small diameter (113) and a downstream section having a relatively large diameter (114), wherein said inner structure (109) defines together with the outer structure (106) an annular flow channel (108); and a guiding system (140) for connecting the inner structure (109) and the downstream portion (111) of the turbojet engine or a portion of a suspension mast; characterised in that the guiding system (140) includes a means for combining a translation and rotation movement of at least a portion of said inner structure (109) between a working position, in which the inner structure (109) is used as a cowling for the turbojet downstream portion (111), and a maintenance position in which the inner structure (109) exposes said turbojet downstream portion (111), thus enabling the movement of said portion if the inner structure (109) along the profile of the upstream section having a relatively small diameter (113), and then of the downstream section having a relatively large diameter (114).
摘要翻译：本发明涉及一种用于飞行器涡轮喷气发动机的机舱（100），其包括下游结构，其包括：外部结构（106），围绕涡轮喷气发动机的下游部分（111）的同心内部结构（109），并且包括上游具有相对较小直径（113）的截面和具有相对较大直径（114）的下游部分，其中所述内部结构（109）与所述外部结构（106）一起限定环形流动通道（108）; 以及用于连接涡轮喷气发动机的内部结构（109）和下游部分（111）或悬架杆的一部分的引导系统（140）其特征在于，所述引导系统（140）包括用于将所述内部结构（109）的至少一部分的平移和旋转运动组合在工作位置之间的装置，其中所述内部结构（109）用作整流罩所述涡轮喷气下游部分（111）以及所述内部结构（109）暴露所述涡轮喷气下游部分（111）的维护位置，从而如果所述内部结构（109）沿着所述上游部分具有相对小的直径（113），然后具有相对较大直径（114）的下游部分。

2. 发明授权

US08448896B2 Guiding system for aircraft nacelle maintenance 有权
标题翻译：飞机机舱维修指导系统
公开(公告)号：US08448896B2
公开(公告)日：2013-05-28
申请号：US12864925
申请日：2009-01-21
申请人： Pierre Caruel , Jean-Philippe Joret , Peter Segat
发明人： Pierre Caruel , Jean-Philippe Joret , Peter Segat
IPC分类号： B64D27/00
CPC分类号： B64D29/08
摘要： A nacelle includes a downstream structure having an outer structure, a concentric inner structure surrounding a downstream portion and an upstream section having a relatively small diameter and a downstream section having a relatively large diameter, the inner and outer structures define an annular flow channel. The nacelle includes a guiding system for connecting the inner structure and downstream portion or a portion of a suspension mast, the system combines a translation and rotation movement of at least a portion of the inner structure between a working position, where the inner structure is used as a cowling for the turbojet downstream portion, and a maintenance position where the inner structure exposes the turbojet downstream portion and enable movement of the portion of the inner structure along the profile of the upstream section having a relatively small diameter, and the downstream section having a relatively large diameter.
摘要翻译：机舱包括具有外部结构的下游结构，围绕下游部分的同心内部结构和具有相对小直径的上游部分和具有相对较大直径的下游部分，内部和外部结构限定环形流动通道。机舱包括用于连接内部结构和下游部分或悬架桅杆的一部分的引导系统，该系统将内部结构的至少一部分的平移和旋转运动组合在使用内部结构的工作位置之间作为用于涡轮喷气下游部分的整流罩，以及内部结构暴露涡轮喷气下游部分并且使内部结构的部分沿着具有相对小直径的上游部分的轮廓能够移动的维护位置，并且下游部分具有一个比较大的直径。

3. 发明申请

US20120217320A1 THRUST INVERTER 有权
标题翻译：逆变器
公开(公告)号：US20120217320A1
公开(公告)日：2012-08-30
申请号：US13510352
申请日：2010-10-26
申请人： Guy Bernard Vauchel , Pierre Caruel , Andre Baillard , Peter Segat
发明人： Guy Bernard Vauchel , Pierre Caruel , Andre Baillard , Peter Segat
IPC分类号： B63H11/10
CPC分类号： F02K1/72 , B64D29/06 , B64D29/08 , F01D25/24 , F01D25/243 , F01D25/28 , F02C7/20 , F02K1/54 , F02K1/64 , F02K1/68 , F05D2250/34
摘要： The present invention relates to a thrust inverter for a turbojet engine nacelle (1) including at least one outer cowl (11) that is movable between a closed position and a thrust inversion position, said movable cowl also being able to be opened into a supporting position towards which said movable cowl is hinged and guided through the use of a guiding means that is suitable to said movable cowl and located substantially on a pylon, to which the nacelle is intended to be attached and at least one front frame (15) capable of being mounted downstream from an air blower housing for said turbojet engine and directly or indirectly holds at least one flow diversion means (12). Said thrust inverter is characterized in that the front frame is detachably connected to the housing in a translatable manner along at least one related guiding member (17) once said front frame is detached from the housing.
摘要翻译：本发明涉及一种用于涡轮喷气发动机机舱（1）的推力逆变器，其包括至少一个能够在关闭位置和推力倒置位置之间移动的外罩（11），所述可动罩也能够被打开成支撑所述可移动整流罩铰接并引导通过使用适于所述可移动整流罩并且基本上位于所述机舱旨在附接的塔架上的导向装置的位置，以及至少一个前框架（15）能够被安装在用于所述涡轮喷气发动机的鼓风机壳体的下游，并且直接或间接保持至少一个分流装置（12）。所述推力逆变器的特征在于，一旦所述前框架与壳体分离，前框架可沿着至少一个相关的引导构件（17）以可平移的方式可拆卸地连接到壳体。

4. 发明授权

US09212689B2 Bent connecting rod fitted with at least one self-aligning means 有权
标题翻译：弯曲连杆装配有至少一个自对准装置
公开(公告)号：US09212689B2
公开(公告)日：2015-12-15
申请号：US13257381
申请日：2010-03-09
申请人： Guy Bernard Vauchel , Peter Segat , Andre Baillard , Georges Alain Bouret
发明人： Guy Bernard Vauchel , Peter Segat , Andre Baillard , Georges Alain Bouret
IPC分类号： F16C7/04 , F02K1/12 , F02K1/70 , F02K1/72 , F16C7/06
CPC分类号： F16C7/04 , F02K1/1261 , F02K1/70 , F02K1/72 , F16C7/06 , Y10T74/2142
摘要： The invention relates to a bent connecting rod (31) for linking a first assembly to a second assembly which are movable relative to each other and through which a flow in the space defined thereby passes. The rod has at least one first and one second pivot point (35, 38) that are designed so as to enable the pivotal movement of the connecting rod (31) relative to said first and second assemblies, respectively, the bent connecting rod (31) being suitably positionable such that the bend (40) is located upstream from said flow relative to said second pivot point (38), said second pivot point (38) being suitably built into the second movable assembly, characterized in that the bent connecting rod (31) includes at least two portions (33, 37) linked together by at least one self-aligning means (39a, 39b).
摘要翻译：本发明涉及一种用于将第一组件连接到第二组件的弯曲连接杆（31），所述第二组件可相对于彼此移动，通过该连接杆限定的空间中的流动通过该连接杆。杆具有至少一个第一和第二枢转点（35,38），其被设计成能够使得连杆（31）相对于所述第一和第二组件分别枢转运动，弯曲的连接杆（31））适当地定位，使得弯曲部（40）相对于所述第二枢转点（38）位于所述流动的上游，所述第二枢转点（38）适当地内置在第二可移动组件中，其特征在于，弯曲的连接杆（31）包括通过至少一个自对准装置（39a，39b）连接在一起的至少两个部分（33,37）。

5. 发明申请

US20120006000A1 BENT CONNECTING ROD FITTED WITH AT LEAST ONE SELF-ALIGNING MEANS 有权
标题翻译：弯曲连接杆配有至少一个自我调节装置
公开(公告)号：US20120006000A1
公开(公告)日：2012-01-12
申请号：US13257381
申请日：2010-03-09
申请人： Guy Bernard Vauchel , Peter Segat , Andre Baillard , Georges Alain Bouret
发明人： Guy Bernard Vauchel , Peter Segat , Andre Baillard , Georges Alain Bouret
IPC分类号： F02K1/72 , F02K1/12 , F16C7/02
CPC分类号： F16C7/04 , F02K1/1261 , F02K1/70 , F02K1/72 , F16C7/06 , Y10T74/2142
摘要： The invention relates to a bent connecting rod (31) for linking a first assembly to a second assembly which are movable relative to each other and through which a flow in the space defined thereby passes. The rod has at least one first and one second pivot point (35, 38) that are designed so as to enable the pivotal movement of the connecting rod (31) relative to said first and second assemblies, respectively, the bent connecting rod (31) being suitably positionable such that the bend (40) is located upstream from said flow relative to said second pivot point (38), said second pivot point (38) being suitably built into the second movable assembly, characterized in that the bent connecting rod (31) includes at least two portions (33, 37) linked together by at least one self-aligning means (39a, 39b).
摘要翻译：本发明涉及一种用于将第一组件连接到第二组件的弯曲连接杆（31），所述第二组件可相对于彼此移动，通过该连接杆限定的空间中的流动通过该连接杆。杆具有至少一个第一和第二枢转点（35,38），其被设计成能够使得连杆（31）相对于所述第一和第二组件分别枢转运动，弯曲的连接杆（31））适当地定位，使得弯曲部（40）相对于所述第二枢转点（38）位于所述流动的上游，所述第二枢转点（38）适当地内置在第二可移动组件中，其特征在于，弯曲的连接杆（31）包括通过至少一个自对准装置（39a，39b）连接在一起的至少两个部分（33,37）。

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