公开(公告)号：US20090050742A1

公开(公告)日：2009-02-26

申请号：US12192148

申请日：2008-08-15

申请人： Cyril Bonnaud ,  Thomas Stevens ,  Frederic Roche ,  Stephane Dostes

发明人： Cyril Bonnaud ,  Thomas Stevens ,  Frederic Roche ,  Stephane Dostes

IPC分类号： B64C23/06

CPC分类号： B64C23/06 ,  B64D2033/024 ,  Y02T50/162

摘要： An aircraft with an outer surface from which flows an aerodynamic stream of cold air and includes at least one hot gas outlet, characterized in that it includes at least one device (16) for generating aerodynamic disturbances so as to mix hot gas and cold air, whereby the at least one device is connected to an outer surface (10) for protection against the heat and/or close to a hot gas outlet (12).

摘要翻译： 一种具有外表面的飞机，其中流动有空气动力的冷空气流并且包括至少一个热气体出口，其特征在于，其包括至少一个用于产生空气动力学干扰以便混合热气体和冷空气的装置（16） 由此所述至少一个装置连接到用于防止热量和/或接近热气体出口（12）的外表面（10）。

公开(公告)号：US20090048724A1

公开(公告)日：2009-02-19

申请号：US12162466

申请日：2007-02-13

申请人： Nicolas Caule

发明人： Nicolas Caule

IPC分类号： G05D1/00

CPC分类号： B64C25/426 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/025

摘要： Method and system for predicting the possibility of complete stoppage of an aircraft on a landing runway. According to the invention: a) the altitude (H) of the aircraft (2) is measured and the horizontal distance (D) separating said aircraft (2) from the proximal end threshold (4) of the landing runway (1) is calculated; b) an estimated finishing position (21) of said aircraft on said landing runway (1) is calculated on the basis of the altitude (H) and of the horizontal distance (D) determined in a), as well as on the basis of the angle of approach (α); and c) said estimated finishing position (21) calculated in b) is utilized to determine said possibility.

摘要翻译： 用于预测在着陆跑道上完全停止飞机的可能性的方法和系统。 根据本发明：a）测量飞机（2）的高度（H），并计算将所述飞机（2）与着陆跑道（1）的近端阈值（4）分开的水平距离（D） ; b）基于在a）中确定的高度（H）和水平距离（D）以及基于在（a）中确定的水平距离（D））计算所述飞机在所述着陆跑道（1）上的估计完成位置（21） 接近角（α）; 和c）用b）中计算出的所述估计完成位置（21）来确定所述可能性。

公开(公告)号：US20090045981A1

公开(公告)日：2009-02-19

申请号：US12191481

申请日：2008-08-14

申请人： David Jean ,  Laetitia Lambinet ,  Remi Cabaret

发明人： David Jean ,  Laetitia Lambinet ,  Remi Cabaret

IPC分类号： G08B21/00 ,  G06F15/16

CPC分类号： H04L67/12

摘要： A system and a method for data transmission between at least one display screen and a remote client system. A first request to send a message via a first communication protocol is caused to be displayed on the display screen, and the message is transmitted to the remote client system via a second communication protocol. A control unit monitors the remote client system. The system induces the generation, and display on the display screen, of a request for confirmation of the first request, by the intermediary of a communication interface, which interface is designed to receive and generate messages in the first communication protocol, as well as to receive and generate messages suitable for being received by the control unit.

摘要翻译： 一种在至少一个显示屏和远程客户端系统之间进行数据传输的系统和方法。 使得经由第一通信协议发送消息的第一请求被显示在显示屏幕上，并且该消息经由第二通信协议被发送到远程客户端系统。 控制单元监视远程客户端系统。 该系统通过通信接口的中介，在显示屏幕上产生和显示对第一请求的确认请求，该通信接口被设计为在第一通信协议中接收和生成消息，以及 接收并产生适合于由控制单元接收的消息。

公开(公告)号：US20090045287A1

公开(公告)日：2009-02-19

申请号：US12106485

申请日：2008-04-21

申请人： Mathieu BELLEVILLE

发明人： Mathieu BELLEVILLE

IPC分类号： B64C1/00

CPC分类号： B64D27/14 ,  B64D2027/005 ,  Y02T50/66

摘要： Aircraft with reduced environmental impact.According to the invention, the engines (6) are mounted at the rear (2R) of the fuselage (2) of said aircraft in such a way that the propellers (8, 9) of said engines (6) are plumb with non-structural removable surfaces (14).

摘要翻译： 降低环境影响的飞机。 根据本发明，发动机（6）以这样的方式安装在所述飞行器的机身（2）的后部（2R）处，使得所述发动机（6）的螺旋桨（8,9） 结构可移除表面（14）。

公开(公告)号：US20090026780A1

公开(公告)日：2009-01-29

申请号：US11914081

申请日：2006-04-27

申请人： Pascal Claraz ,  Jean-Marc Datas

发明人： Pascal Claraz ,  Jean-Marc Datas

IPC分类号： B66C13/04

CPC分类号： B66C13/04

摘要： A sling device for a piece, including a sling provided with a non-extending piece and a section with spring means permitting an elastic lengthening or shortening under load of a limited given amplitude for the sling in response to a limited given change in load on the piece.

摘要翻译： 一种用于零件的吊索装置，包括具有不延伸件的吊索和具有弹簧装置的部分，其允许在有限的给定振幅的载荷下对吊索进行弹性拉长或缩短，以响应于对载荷的有限的给定变化 片。

公开(公告)号：US20090018710A1

公开(公告)日：2009-01-15

申请号：US12088307

申请日：2006-09-27

申请人： Patrick Marey ,  Pierre-Numa Lavigne ,  Alain Locatelli ,  Dominique Garel

发明人： Patrick Marey ,  Pierre-Numa Lavigne ,  Alain Locatelli ,  Dominique Garel

IPC分类号： G06F17/00

CPC分类号： G05B15/02

摘要： The disclosed embodiments concerns a device and method for controlling equipment having a plurality of subassemblies and provided with a storage unit storing at least one set of information relating to the subassemblies, a connection being used for extracting the set of coded information.According to the disclosed embodiments, the set of information received by means of the connection is recorded in a first file on a recording medium, and then, from at least a second file previously recorded on the recording medium, the characteristics of the coding are determined in order to identify this information. The content of the first file is analysed using the characteristics, and the result thus obtained is recorded in a third file on the recording medium.

摘要翻译： 所公开的实施例涉及用于控制具有多个子组件的设备的设备和方法，并且设置有存储单元，该存储单元存储与子组件相关的至少一组信息，用于提取编码信息集合的连接。 根据所公开的实施例，通过连接接收的信息集合被记录在记录介质上的第一文件中，然后，从先前记录在记录介质上的至少第二文件确定编码的特性 以便识别此信息。 使用特征分析第一文件的内容，并将由此获得的结果记录在记录介质上的第三文件中。

公开(公告)号：US20090015438A1

公开(公告)日：2009-01-15

申请号：US12145849

申请日：2008-06-25

申请人： Boris SORBIER ,  Pierre CAMPAGNE ,  Baptiste MAYLIN

发明人： Boris SORBIER ,  Pierre CAMPAGNE ,  Baptiste MAYLIN

IPC分类号： G08B23/00

CPC分类号： G08G5/0078 ,  G08G5/0021 ,  G08G5/0086

摘要： The invention relates to a method for managing an interruption of emission, in an aircraft, of an acoustic message comprising an information item about a state of part of the said aircraft and/or about its environment, characterized in that, the acoustic message being structured into one or more successive acoustic fragments each representative of the said information item, the said method comprises the steps: of delaying (E3), starting from a given moment, the execution of a decision to interrupt the emission of the acoustic message until the end of emission of an acoustic fragment that is in the course of emission at the said given moment, and of executing (E4) the said interruption decision.

摘要翻译： 本发明涉及一种用于管理飞机中的发射中断的方法，该声音消息包括关于所述飞行器的一部分的状态和/或其环境的信息项，其特征在于，声音消息被构造 分成代表所述信息项的一个或多个连续的声音片段，所述方法包括以下步骤：从给定时刻开始延迟（E3）执行决定以中断声音消息的发射直到结束 在所述给定时刻处于发射过程中的声音片段的发射，以及执行（E4）所述中断判定。

公开(公告)号：US20090014590A1

公开(公告)日：2009-01-15

申请号：US12145040

申请日：2008-06-24

申请人： Jaouen Ponsart ,  Jerome Gras

发明人： Jaouen Ponsart ,  Jerome Gras

IPC分类号： B64C1/14 ,  E05B57/00

CPC分类号： B64C1/1446 ,  E05B53/003 ,  E05C1/14 ,  E05F15/53 ,  E05Y2900/502 ,  E05Y2900/612 ,  E06B5/01 ,  Y10T70/5168 ,  Y10T292/0972 ,  Y10T292/0976 ,  Y10T292/57

摘要： The present invention relates to a hatch (1) provided with at least one locking socket, equipped with first actuation means (108) making it possible to urge a flexible linear pulling member (104), connected to the socket, in an unlocking direction (126), by abutting against a stop member (132) secured to the member (104), at a distance from a second member end (128) of said member (104), in which the means (108) can be controlled from a first side (140) of the hatch, and equipped with second actuation means (110) making it possible to urge the member (104) in the direction (126), which means (110) are connected to the second end (128) and can be controlled from a second side (158) of the hatch.

摘要翻译： 本发明涉及一种设置有至少一个锁定插座的舱口（1），其具有第一致动装置（108），使得能够在解锁方向上推动连接到插座的柔性线性牵引构件（104） 与所述构件（104）的第二构件端（128）相距一定距离处，抵靠固定到所述构件（104）上的止动构件（132），其中所述构件（108）可以从所述构件 并且装备有第二致动装置（110），使得能够沿着方向（126）推动构件（104），该装置（110）连接到第二端（128），并且 可以从舱口的第二侧（158）控制。

公开(公告)号：US20090010174A1

公开(公告)日：2009-01-08

申请号：US12146853

申请日：2008-06-26

申请人： Franck DESSERTENNE

发明人： Franck DESSERTENNE

IPC分类号： H04L12/26

CPC分类号： H04L43/50 ,  H04L2012/4028 ,  H04L2012/6459

摘要： The object of the invention is a method and a device for exchanging diagnostic data for simulation of computer networks of aircraft. Diagnostic data exchange is achieved in a network between a network node and a diagnostic terminal connected to the network. The network node is capable of receiving simulation commands in real time and diagnostic commands. According to the invention, the network node is capable of receiving simulation commands according to at least one predetermined time period, time-based segregation being achieved for emission of diagnostic data relative to processing of simulation commands.

摘要翻译： 本发明的目的是用于交换用于模拟飞行器计算机网络的诊断数据的方法和装置。 在网络节点和连接到网络的诊断终端之间的网络中实现诊断数据交换。 网络节点能够实时接收模拟命令和诊断命令。 根据本发明，网络节点能够根据至少一个预定时间段接收模拟命令，实现相对于仿真命令的处理发射诊断数据的基于时间的偏析。

公开(公告)号：US20090007567A1

公开(公告)日：2009-01-08

申请号：US12160190

申请日：2007-01-18

申请人： Alain Porte ,  Damien Prat

发明人： Alain Porte ,  Damien Prat

IPC分类号： F02C7/141 ,  F02K3/06 ,  F02K3/115

CPC分类号： F02C7/141 ,  F02K3/06 ,  F02K3/075 ,  F02K3/115 ,  Y02T50/675

摘要： The invention concerns a precooler (30) having an annular cross-sectional shape about the axis (L-L) of the pod and arranged inside the rear part (10R) of the inner shroud (10) in external contact with the cold flow (9) exiting the fan duct channel (13) and in close contract with the cooling air stream (29) drawn from said cold flow (9).

摘要翻译： 本发明涉及一种预冷器（30），其具有围绕容器的轴线（LL）的环形横截面形状，并且布置在内部护罩（10）的与冷流（9）外部接触的后部（10R）的内部， 离开风扇管道通道（13）并与从所述冷流（9）抽出的冷却空气流（29）紧密接合。