公开(公告)号：JP2011132656A

公开(公告)日：2011-07-07

申请号：JP2010286172

申请日：2010-12-22

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： DELECROIX VINCENT

IPC: D04H18/00

CPC classification number: D04H18/00 ,  D04H18/02

Abstract: PROBLEM TO BE SOLVED: To provide a needling table enabling to obtain a woven fabric structure having edge portions which are perfectly beautiful and can prevent a material from being affected by a creep action. SOLUTION: The circular needling table (10) for needling a woven fabric structure made of a circular fiber preform includes a horizontal circular platen (14) for having a circular fiber preform (12) placed thereon, a driving means for rotation-driving the fiber preform on the axis (16) of the platen, a needling device (22) having a needling head (24) extended over the fan-shaped portion of the platen and driven by movements perpendicular to the platen, and a guide means (38a, 38b) for guiding the fiber preform below the needling head. COPYRIGHT: (C)2011,JPO&INPIT

Abstract translation: 要解决的问题：提供一种能够获得具有完美美观的边缘部分并且可以防止材料受到蠕变作用的织物结构的针刺表。 解决方案：用于针刺由圆形纤维预制件制成的机织织物结构的圆形针刺台（10）包括用于具有放置在其上的圆形纤维预制件（12）的水平圆形台板（14），用于旋转的驱动装置， 在所述压板的轴线（16）上驱动所述纤维预制件，所述针刺装置（22）具有在所述压板的所述扇形部分上延伸并由垂直于所述压板的运动驱动的针刺头（24） （38a，38b），用于将纤维预制件引导到针刺头下方。 版权所有（C）2011，JPO＆INPIT

公开(公告)号：JP2011131879A

公开(公告)日：2011-07-07

申请号：JP2010286412

申请日：2010-12-22

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： THIBAULT JULIEN ,  COLIN EMMANUEL

IPC: B64C25/42 ,  B60T8/17 ,  B60T17/18

CPC classification number: B60T8/1703 ,  B60L7/003 ,  B60T8/885 ,  B60T2270/402 ,  B60T2270/413

Abstract: PROBLEM TO BE SOLVED: To provide an electric brake mechanism for an aircraft where a normal line system and an emergency line system are reduced in risks of common mode failures. SOLUTION: The electric brake mechanism includes a brake control unit having several electromechanical brake actuators (EBAs) for generating brake set values in response to a brake command in a normal mode, a plurality of electromechanical actuator controllers (EMACs) fed with AC power, and the electromechanical actuator controllers include at least one inverter for supplying power to the EBA in response to the brake set value, at least one emergency brake power supply and control unit (EBPCU) fed only with DC power, and the emergency brake power supply and control unit include at least one inverter for supplying power to the several EBAs in response to the brake command, and a protecting means for transmitting to the actuator the power supplied by the EMACs or EBPCU while preventing the flow of power in the mechanism. COPYRIGHT: (C)2011,JPO&INPIT

Abstract translation: 要解决的问题：为普通线路系统和应急线路系统降低共模故障的风险的飞机提供电动制动机构。 解决方案：电动制动机构包括制动控制单元，该制动控制单元具有几个机电制动致动器（EBAs），用于响应于在正常模式下的制动指令产生制动设定值;多个机电致动器控制器（EMAC） 并且所述机电致动器控制器包括至少一个用于响应于所述制动器设定值向所述EBA供电的逆变器，至少一个仅供给直流电力的紧急制动电源和控制单元（EBPCU）以及所述紧急制动功率 供应和控制单元包括至少一个逆变器，用于响应于制动指令向多个EBA供电;以及保护装置，用于在防止机构中的动力流动的同时向致动器传送由EMAC或EBPCU提供的功率。 版权所有（C）2011，JPO＆INPIT

公开(公告)号：JP2011116360A

公开(公告)日：2011-06-16

申请号：JP2010267454

申请日：2010-11-30

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： BASSET MICHEL ,  CHAMAILLARD YANN ,  SORIN ANTHONY ,  LEMAY DAVID

IPC: B60T8/17 ,  B60T8/00 ,  B64C25/44

CPC classification number: B60T1/10 ,  B60T13/586

Abstract: PROBLEM TO BE SOLVED: To minimize wear of a friction element of a braking device of an aircraft.
SOLUTION: This aircraft includes a landing device having each of wheels mounted with a friction brake and an auxiliary brake capable of dissipating energy by a means except friction. When braking is required, whether or not the aircraft is in a braking state for which the friction brake is not indispensable is determined to provide necessary braking by testing a braking parameter. The auxiliary brake is preferentially operated as long as the aircraft remains in the braking state. Only when the aircraft deviates from the braking state, necessary braking is executed by operating the friction brake.
COPYRIGHT: (C)2011,JPO&INPIT

Abstract translation: 要解决的问题：为了减少飞机的制动装置的摩擦元件的磨损。 解决方案：该飞机包括一个着陆装置，其具有安装有摩擦制动器的每个车轮和能够通过除摩擦之外的装置消耗能量的辅助制动器。 当需要制动时，无论飞行器是否处于不必要的摩擦制动器的制动状态，都被确定为通过测试制动参数来提供必要的制动。 只要飞机保持在制动状态，辅助制动器就优先操作。 只有当飞机偏离制动状态时，通过操作摩擦制动器来执行必要的制动。 版权所有（C）2011，JPO＆INPIT

公开(公告)号：JP2010255174A

公开(公告)日：2010-11-11

申请号：JP2010100123

申请日：2010-04-23

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： FILLION ARNAUD

IPC: D06M13/02 ,  D06M13/513

CPC classification number: C04B35/806 ,  C04B35/83 ,  F16D69/023 ,  H05B6/108 ,  H05B6/362

Abstract: PROBLEM TO BE SOLVED: To provide a method and apparatus for densifying a porous product with improvement of densification of the porous substrate by using a film boiling process, in particular, to provide a method and apparatus permitting more complete densification of a substrate (i.e., densification closer to the surface of the substrate).
SOLUTION: The method permits more complete densification of a substrate (preform) 110 by selectively providing a barrier 100 that reduces cooling of the surface of the substrate 110 being densified caused by contact with the relatively cool boiling liquid precursor of the densifying material, such as carbon. In particular, the contact between the substrate 110 and the liquid precursor is reduced by utilizing a structure forming an insulator gas layer between one or two physical barriers (such as a mesh material) 100 or the substrate 110 with the liquid precursor (such as a plate spaced apart from the surface of the porous substrate). The barrier 100 is moved into optional position before the applied power level increases sharply near the end of the film boiling densification process.
COPYRIGHT: (C)2011,JPO&INPIT

Abstract translation: 待解决的问题：提供一种通过使用薄膜沸腾方法提高多孔基材的致密化来增强多孔产品的方法和装置，特别是提供一种允许更完全致密化基材的方法和装置 （即，更靠近基板表面的致密化）。 解决方案：该方法允许通过选择性地提供阻挡层100来更准确地致密化基底（预成型件）110，阻挡层100减少由致密材料的相对冷的沸腾的液体前体的接触引起的致密化的基底110的表面的冷却 ，如碳。 特别地，通过利用在一个或两个物理屏障（例如网状材料）100或衬底110之间形成绝缘体气体层的结构与液体前体（例如， 板与多孔基材的表面间隔开）。 在施加的功率水平在薄膜沸腾致密化过程结束附近急剧增加之前，阻挡层100移动到可选择的位置。 版权所有（C）2011，JPO＆INPIT

公开(公告)号：JP2010143575A

公开(公告)日：2010-07-01

申请号：JP2009289532

申请日：2009-12-21

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： NIERLICH FLORENT ,  LEYNAERT FRANCOIS-NOEL

IPC: B64C25/24 ,  H02M7/155

CPC classification number: B64C25/24 ,  B64C13/50 ,  B64C13/504 ,  B64C25/26 ,  B64D2221/00 ,  H02J4/00 ,  Y02T50/44 ,  Y10T307/398

Abstract: PROBLEM TO BE SOLVED: To improve the safety of a maintenance operator performing work regarding an actuator, and to reduce a loss in an inverter.
SOLUTION: The power distribution architecture for distributing power to electromechanical actuators (105, 106, 108; 205, 206, 208; 109A, 109B, 209A, 209B) of the aircraft includes at least one of power distribution elements (150, 250, 160, 260) for distributing power to the electromechanical actuators connected to the architecture, and the architecture receives power from at least one of power distribution buses (PW1, PW2) of the aircraft. A DC network 500 in which a voltage is variably controlled is inserted between the power distribution bus of the aircraft and the power distribution element.
COPYRIGHT: (C)2010,JPO&INPIT

Abstract translation: 要解决的问题：为了提高维护操作员对执行机构进行工作的安全性，并减少逆变器的损耗。 解决方案：用于向飞机的机电致动器（105,106,108; 205,206,208,109A，109B，209A，209B）分配功率的配电架构包括功率分配元件（150， 250,160,260），用于将功率分配给连接到所述架构的所述机电致动器，并且所述架构从所述飞行器的配电总线（PW1，PW2）中的至少一个接收功率。 其中电压被可变地控制的DC网络500被插入在飞机的配电总线和配电元件之间。 版权所有（C）2010，JPO＆INPIT

公开(公告)号：JP2009220809A

公开(公告)日：2009-10-01

申请号：JP2009061524

申请日：2009-03-13

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： TREYZ ALAIN

IPC: B64D33/00 ,  F15B21/04

CPC classification number: B01D29/15 ,  B01D29/902 ,  B01D35/153 ,  B01D35/306 ,  B01D35/31 ,  B01D2201/4023 ,  B01D2201/4046 ,  B01D2201/4076

Abstract: PROBLEM TO BE SOLVED: To provide a filter device without such a problem that a vessel is attached in a state that a cartridge is unmounted, or only the vessel is detached and the cartridge remains at detachment.
SOLUTION: The vessel (3) is fitted internally with a pin (6) of elastically deformable material comprising firstly a key (8) that extends toward an opening of the vessel (3) and includes a curved end (9) that projects beyond an edge of the vessel (3), and secondly a finger (10) that extends toward the bottom of the vessel (3), and is oriented toward the center thereof, so that when the cartridge (4) is put into the vessel (3), the finger (10) is pushed back by the cartridge (4) and forces the key (8) to retract so that its curved end no longer projects radially from the vessel (3), the cartridge (4) fitted with an external obstacle (14) that co-operates with one end of the finger (10) in order to prevent the cartridge (4) from being withdrawn from the vessel (3).
COPYRIGHT: (C)2010,JPO&INPIT

Abstract translation: 要解决的问题：为了提供一种过滤器装置，没有这样的问题，即在卸载盒的状态下或仅仅拆卸容器并且盒保持分离的状态下容器被安装。 解决方案：容器（3）内部装配有可弹性变形材料的销（6），其首先包括朝向容器（3）的开口延伸的键（8），并且包括弯曲端（9），其中 突出于容器（3）的边缘之外，其次是朝着容器（3）的底部延伸的手指（10），并且朝向其中心定向，使得当盒（4）被放入 手指（10）被盒（4）推回并迫使钥匙（8）缩回，使得其弯曲的端部不再从容器（3）径向伸出，所以盒（4）装配 具有与手指（10）的一端配合的外部障碍物（14），以防止药筒（4）从容器（3）中取出。 版权所有（C）2010，JPO＆INPIT

公开(公告)号：JP2008302925A

公开(公告)日：2008-12-18

申请号：JP2008149730

申请日：2008-06-06

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： PRADIER JEAN-CLAIR ,  MAES BERTRAND

IPC: B60C23/04 ,  B64C25/36

CPC classification number: B60C23/0408 ,  B60C23/043 ,  B60C23/0444

Abstract: PROBLEM TO BE SOLVED: To provide a particular constitution for a communication device capable of more sufficiently protecting the communication device.
SOLUTION: In the undercarriage for the aircraft having at least one shaft having at least one wheel mounted so as to be rotated on the shaft, the undercarriage for the aircraft has a communication device for connecting a sensor mounted onto a rim part of the wheel to a stationary processing means mounted onto the aircraft. The communication device is provided with a rotation antenna mounted onto the rim part of the wheel so as to be rotated with the rim part of the wheel and connected to the sensor; and a stationary antenna facing to the rotation antenna such that the rotation antenna and the stationary antenna are in an electro-magnetic relationship. The stationary antenna is connected to the processing means, and the stationary antenna and the rotation antenna are extended to an inner side of the wheel facing to the undercarriage for the aircraft.
COPYRIGHT: (C)2009,JPO&INPIT

Abstract translation: 要解决的问题：为能够更充分地保护通信设备的通信设备提供特定的结构。 解决方案：在具有至少一个轴的飞机的起落架中，至少一个轴安装成在轴上旋转，用于飞机的起落架具有连接装置，用于连接安装在 将车轮安装到飞机上的固定处理装置。 通信装置设置有旋转天线，其安装在车轮的轮辋部分上，以便与车轮的轮辋部分一起旋转并连接到传感器; 以及面向旋转天线的固定天线，使得旋转天线和固定天线处于电磁关系。 固定天线连接到处理装置，固定天线和旋转天线延伸到面向飞机起落架的轮的内侧。 版权所有（C）2009，JPO＆INPIT

公开(公告)号：JP2007246079A

公开(公告)日：2007-09-27

申请号：JP2007061521

申请日：2007-03-12

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： DELLAC STEPHANE ,  JACQUET ARNAUD ,  ESTEBAN ANTOINE

IPC: B64C25/42

CPC classification number: B64C25/426 ,  G08G5/065

Abstract: PROBLEM TO BE SOLVED: To improve management for braking of an aircraft by achieving new possibility of tracking the course of the aircraft in an airport. SOLUTION: According to this braking management method for the aircraft 1 in taxing in the airport, based on the characteristics of a sequence of movement of the aircraft along at least one given course 3, 4 for advancing the aircraft in the airport, the aircraft includes a procedure of estimating the information on braking (F1, F2, ...) actually executed to advance in the application of sequence of movement. COPYRIGHT: (C)2007,JPO&INPIT

Abstract translation: 要解决的问题：通过在机场跟踪飞机过程的新可能性来改善飞机制动的管理。

解决方案：根据飞机1在机场征税的制动管理方法，根据航空器沿着至少一个给定航线3,4的行进顺序的特点，用于在机场内推进飞机， 该飞机包括估计实际执行的制动信息（F1，F2，...）的过程，以便在运动顺序的应用中前进。 版权所有（C）2007，JPO＆INPIT

公开(公告)号：JP2007170668A

公开(公告)日：2007-07-05

申请号：JP2006344119

申请日：2006-12-21

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： BUCHETON DANIEL ,  CHARUEL HERVE

IPC: F16H25/20 ,  H02K7/06 ,  H02K7/106

CPC classification number: F16H25/205 ,  B64C25/30 ,  F16H2025/2059 ,  F16H2025/2075 ,  Y10T74/18576 ,  Y10T74/186

Abstract: PROBLEM TO BE SOLVED: To provide an actuator which, even in the event of a main connecting rod malfunction, does not oppose continued movement. SOLUTION: The telescopic actuator comprises a cylinder (1) in which the main connecting rod (2) is mounted to slide telescopically along a sliding axis (X) between a retracted position and an extended position. The actuator includes an auxiliary rod (20) mounted to slide telescopically in the main rod (2) along the sliding axis (X) between a retracted position and an extended position, and controlled retaining means (30, 31, 32, 33) for retaining the auxiliary rod (20) in the retracted position inside the main rod (2). COPYRIGHT: (C)2007,JPO&INPIT

Abstract translation: 要解决的问题：提供即使在主连杆故障的情况下也不反对持续运动的致动器。 解决方案：伸缩式致动器包括一个气缸（1），主连接杆（2）安装在该气缸中，以便在缩回位置和伸出位置之间沿着滑动轴线（X）可伸缩地滑动。 所述致动器包括辅助杆（20），所述辅助杆（20）安装成沿着所述滑动轴线（X）在缩回位置和延伸位置之间可伸缩地在所述主杆（2）中滑动，以及被控制的保持装置（30,31,32,33），用于 将辅助杆（20）保持在主杆（2）内部的缩回位置。 版权所有（C）2007，JPO＆INPIT

公开(公告)号：JP2007155130A

公开(公告)日：2007-06-21

申请号：JP2006315974

申请日：2006-11-22

Applicant: Messier Bugatti ,  メシエ−ブガッティMessier Bugatti

Inventor： PERRAULT MAURICE ,  PHILIPPE CHICO

IPC: F16D65/18 ,  F16D65/28 ,  B64C25/42 ,  F16D55/38 ,  F16F15/08

CPC classification number: F16D55/36 ,  F16D65/18 ,  F16D2121/24

Abstract: PROBLEM TO BE SOLVED: To provide an electromechanical aircraft brake comprising a support 7 carrying at least one electromechanical actuator 8. SOLUTION: In this electromechanical brake comprising a pusher 13 being axially displaceable towards friction elements in order to apply a braking force selectively to the friction elements 11, the actuator is mounted on the support via a connection member 20, 30 allowing at least a portion of the actuator carrying the pusher to tilt angularly. COPYRIGHT: (C)2007,JPO&INPIT

Abstract translation: 要解决的问题：提供一种机电飞行器制动器，其包括承载至少一个机电致动器8的支撑件7.解决方案：在该机电制动器中，包括可朝向摩擦元件轴向移位的推动器13，以便施加 选择性地向摩擦元件11施加制动力，致动器经由连接构件20,30安装在支撑件上，允许承载推动器的致动器的至少一部分倾斜地倾斜。 版权所有（C）2007，JPO＆INPIT