专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US07271741B2 Method and device for detecting an overstepping of design loads of the fin of an aircraft 有权
标题翻译：用于检测飞行器翅片的设计载荷超标的方法和装置
公开(公告)号：US07271741B2
公开(公告)日：2007-09-18
申请号：US11143704
申请日：2005-06-03
申请人： Franck Delaplace , Sylvie Marquier , Gérard Mathieu , Gennaro Squeglia
发明人： Franck Delaplace , Sylvie Marquier , Gérard Mathieu , Gennaro Squeglia
IPC分类号： G08B21/00
CPC分类号： B64D43/02 , B64F5/60
摘要： A method and device for detecting an overstepping of design loads of the fin of an aircraft. The device includes a set of information sources and a section for determining, with the aid of information emanating from the set of information sources, a current bending moment. The device further includes a section for determining, with the aid of information emanating from the set of information sources, a current twisting moment, and a section for carrying out a comparison by comparing the pair formed by the current bending moment and the current twisting moment with a safety envelope representing a chart formed in a plane on the basis of pairs of values of bending and twisting moments and defined so that, for any pair which lies outside the safety envelope, there exists a risk of appearance of permanent deformation on the fin. The device further includes a section for determining whether a structural inspection of the fin has to be performed, at least on the basis of a comparison result provided by the comparison section.
摘要翻译：一种用于检测飞行器翅片的设计载荷超标的方法和装置。该装置包括一组信息源和一个部分，用于借助于从该组信息源发出的信息确定当前的弯矩。该装置还包括一个部分，用于借助于从该组信息源发出的信息来确定当前的扭转力矩，以及用于通过比较由当前弯矩和当前扭转力矩形成的对来执行比较的部分其中安全信封代表基于弯曲和扭转力矩值的平面中形成的图表，并且被定义为使得对于位于安全壳体之外的任何一对，存在在翅片上出现永久变形的风险。该装置还包括至少基于由比较部分提供的比较结果来确定是否必须执行散热片的结构检查的部分。

2. 发明授权

US07382283B2 Method and device for detecting an overstepping of design loads of the tailplane of an aircraft 有权
标题翻译：用于检测飞机尾翼设计负荷超标的方法和装置
公开(公告)号：US07382283B2
公开(公告)日：2008-06-03
申请号：US11146105
申请日：2005-06-07
申请人： Franck Delaplace , Sylvie Marquier , Gérard Mathieu , Gennaro Squeglia
发明人： Franck Delaplace , Sylvie Marquier , Gérard Mathieu , Gennaro Squeglia
IPC分类号： G08B21/00
CPC分类号： B64D43/02 , B64F5/60
摘要： Detection of the overstepping of design loads of an aircraft tailplane may include determining current bending and twisting moments applied to the aircraft. The determined bending and twisting moments are compared with a safety envelope to determine the risk of developing permanent deformations on the tailplane. A determination is made as to whether a structural inspection of the tailplane should be performed based on the comparison result.
摘要翻译：检测飞机尾翼的设计负载的超越可以包括确定施加到飞行器的当前弯曲和扭转力矩。将确定的弯曲和扭矩与安全壳进行比较，以确定在尾翼上发生永久变形的风险。根据比较结果确定是否应进行尾翼的结构检查。

3. 发明授权

US07164366B2 Process and device for detecting on an aircraft an overshoot of design loads at the level of a structural part of said aircraft 有权
标题翻译：用于在飞机上检测在所述飞行器的结构部分的水平面上的设计载荷的过冲的过程和装置
公开(公告)号：US07164366B2
公开(公告)日：2007-01-16
申请号：US10998811
申请日：2004-11-30
申请人： Franck Delaplace , Sylvie Marquier , Gérard Mathieu , Gennaro Squeglia
发明人： Franck Delaplace , Sylvie Marquier , Gérard Mathieu , Gennaro Squeglia
IPC分类号： G08B21/00
CPC分类号： B64D45/00 , B64D2045/0085 , B64F5/60
摘要： A process and device for detecting on an aircraft an overshoot of design loads at the level of a structural part of the aircraft. The detection device includes a speed measuring device for measuring an effective speed of the aircraft. A first comparator compares the measured effective speed with a maximum speed relating to the current flight configuration of the aircraft. A vertical load measuring device measures a vertical load factor of the aircraft, and a second comparator compares the measured vertical load factor with a limit value of the vertical load factor. An inspection determining device determines whether a structural inspection needs to be performed at the level of the structural part, based of the results of the first and second comparisons.
摘要翻译：一种用于在飞行器的结构部分的水平面上检测设计负载的过冲的过程和装置。检测装置包括用于测量飞行器的有效速度的速度测量装置。第一比较器将测量的有效速度与与飞机的当前飞行配置相关的最大速度进行比较。垂直负载测量装置测量飞行器的垂直载荷系数，第二比较器将测量的垂直载荷系数与垂直载荷系数的极限值进行比较。检查确定装置基于第一和第二比较的结果来确定是否需要在结构部件的水平执行结构检查。

4. 发明授权

US07281683B2 Process for aiding the takeoff of an aircraft 有权
标题翻译：帮助飞机起飞的过程
公开(公告)号：US07281683B2
公开(公告)日：2007-10-16
申请号：US11111927
申请日：2005-04-22
申请人： Franck Delaplace , Gérard Mathieu , Nicolas Daniel
发明人： Franck Delaplace , Gérard Mathieu , Nicolas Daniel
IPC分类号： B64C13/00
CPC分类号： G05D1/0083
摘要： An aircraft takeoff process may include applying a pitch command deflecting an adjustable horizontal tailplane of the aircraft by a predetermined angle. Thereafter, the pitch command is corrected in accordance with the deviation between a takeoff rotation speed and a stall reference speed VRref of the aircraft.
摘要翻译：飞机起飞过程可以包括应用将飞行器的可调节水平尾翼偏转预定角度的俯仰指令。此后，根据飞行器的起飞转速和失速基准速度VRref之间的偏差校正俯仰指令。

5. 发明授权

US06241183B1 Method for controlling an aeroplane control surfaces to counter ground lateral drift 有权
标题翻译：控制飞机控制面以抵抗地面横向漂移的方法
公开(公告)号：US06241183B1
公开(公告)日：2001-06-05
申请号：US09341292
申请日：1999-09-14
申请人： Gérard Mathieu
发明人： Gérard Mathieu
IPC分类号： B64C1300
CPC分类号： G05D1/0204 , B64C9/12 , B64C13/16 , G05D1/0083
摘要： A control process for the control surfaces of an aircraft to prevent lateral deviation of the trajectory on the ground during a landing or interrupted takeoff, in which the spoilers are extended asymmetrically.
摘要翻译：用于飞机的控制表面的控制过程，以防止在着陆或中断起飞期间地面上的轨迹的横向偏移，其中扰流板不对称地延伸。

6. 发明授权

US08777097B2 Set of blanks, box and box production method 有权
标题翻译：一套空白，盒子和盒子的制作方法
公开(公告)号：US08777097B2
公开(公告)日：2014-07-15
申请号：US12679802
申请日：2008-09-04
申请人： Sébastien Jacomelli , Gérard Mathieu
发明人： Sébastien Jacomelli , Gérard Mathieu
IPC分类号： B65D5/32 , B31B17/00
CPC分类号： B65D5/328 , B31B50/20 , B31B50/25 , B31B50/28 , B31B50/72 , B31B50/81 , B31B2105/00 , B31B2105/0022 , B31B2120/002
摘要： The invention relates to a set (22) of blanks for forming a packaging box, a method and a corresponding box. The set includes two corrugated board blanks, namely: a first blank (2′) including flaps connected to one another by first fold lines (9′), one side of said blank having no folds; and a second blank (12′) including panels (13′, 14′, 15′, 16′) connected to one another by third fold lines (19′), the panels of the second blank being stacked respectively on the part of the first blank having no folds. Two non-adjacent flaps (3′, 5′) of the first blank are glued to two respective facing panels (13′, 15′) of the second blank, thereby preventing the relative movement thereof during folding or during the formation of the box when the blanks are wound around a volume having pre-determined dimensions. At least two-thirds of the third fold lines (19′) of the second blank are substantially aligned in relation to the first fold lines of the first blank, the lower part (23) of one or more of said third lines including a cut or collapsed portion opposite the corresponding first fold line.
摘要翻译：本发明涉及一种用于形成包装盒的坯料（22），方法和相应的盒子。该组件包括两个波纹板坯件，即：第一坯件（2'），包括通过第一折叠线（9'）彼此连接的折翼，所述坯料的一侧不具有折痕; 和包括通过第三折线（19'）彼此连接的面板（13'，14'，15'，16'）的第二坯料（12'），第二坯料的板分别堆叠在第一个空白没有折叠。第一坯料的两个不相邻的折板（3'，5'）被胶合到第二坯料的两个相应的相对面板（13'，15'），从而防止在折叠期间或在形成盒子期间的相对移动当坯料围绕具有预定尺寸的体积缠绕时。第二坯料的第三折线（19'）的至少三分之二相对于第一坯料的第一折线基本上对准，一条或多条所述第三条线的下部（23）包括切割或与相应的第一折线相对的折叠部分。

7. 发明授权

US08359129B2 Method and device for controlling the thrust of a multi-engine aircraft 有权
标题翻译：用于控制多发飞机的推力的方法和装置
公开(公告)号：US08359129B2
公开(公告)日：2013-01-22
申请号：US12162774
申请日：2007-03-08
申请人： Benoît Lemaignan , Gérard Mathieu
发明人： Benoît Lemaignan , Gérard Mathieu
IPC分类号： G05D1/00
CPC分类号： G05D1/0072 , B64D31/10
摘要： A method and device control the thrust of a multi-engine aircraft. At least one engine command is determined by a command determining unit, with the determined command commanding each engine that has not failed to deliver a thrust substantially equal to a reduced thrust value. A command application unit is configured to apply the determined command to each aircraft engine that has not failed. The reduced thrust value is determined, by a weight determining device, according to the current weight of the aircraft and according to a reduced thrust value FOEI, which is calculated by a thrust calculation unit.
摘要翻译：一种方法和装置控制多发飞机的推力。由命令确定单元确定至少一个发动机命令，其中所确定的命令命令每个发动机未失效地将推力基本上等于减小的推力值。命令应用单元被配置为将所确定的命令应用于未失败的每个飞机引擎。减重推力值由重量确定装置根据飞行器的当前重量并根据由推力计算单元计算的减小的推力值FOEI来确定。

8. 发明授权

US07237852B2 Method and device for controlling and braking an aircraft running on the ground 有权
标题翻译：用于控制和制动在地面上运行的飞机的方法和装置
公开(公告)号：US07237852B2
公开(公告)日：2007-07-03
申请号：US11101414
申请日：2005-04-08
申请人： Rémi Bellouard , Gérard Mathieu
发明人： Rémi Bellouard , Gérard Mathieu
IPC分类号： B60T8/86
CPC分类号： B64C25/48
摘要： Method and device for controlling and braking an aircraft running on the groundAccording to the invention, the aircraft (1) comprises two close undercarriage wheel assemblies (2D, 2G) and two distant undercarriage wheel assemblies (3D, 3G), the biggest of the braking commands (FD, FG) can, under certain conditions, be applied not only to the corresponding two undercarriage wheel assemblies, but also to the close undercarriage wheel assembly corresponding to the smallest braking command.
摘要翻译：用于控制和制动在地面上运行的飞行器的方法和装置根据本发明，飞机（1）包括两个紧密的底盘轮组件（2D，2G）和两个远距离的底盘轮组件（3D，3G）在一定条件下，最大的制动指令（FD，FG）不仅可以应用于相应的两个底盘轮组件，还可以应用于与最小制动指令相对应的紧密的底盘轮组件。

9. 发明申请

US20100264200A1 SET OF BLANKS, BOX AND BOX PRODUCTION METHOD 有权
标题翻译：一套空白，盒子和盒子生产方法
公开(公告)号：US20100264200A1
公开(公告)日：2010-10-21
申请号：US12679802
申请日：2008-09-04
申请人： Sébastien Jacomelli , Gérard Mathieu
发明人： Sébastien Jacomelli , Gérard Mathieu
IPC分类号： B65D5/32 , B31B17/00
CPC分类号： B65D5/328 , B31B50/20 , B31B50/25 , B31B50/28 , B31B50/72 , B31B50/81 , B31B2105/00 , B31B2105/0022 , B31B2120/002
摘要： The invention relates to a set (22) of blanks for forming a packaging box, a method and a corresponding box. The set includes two corrugated board blanks, namely: a first blank (2′) including flaps connected to one another by first fold lines (9′), one side of said blank having no folds; and a second blank (12′) including panels (13′, 14′, 15′, 16′) connected to one another by third fold lines (19′), the panels of the second blank being stacked respectively on the part of the first blank having no folds. Two non-adjacent flaps (3′, 5′) of the first blank are glued to two respective facing panels (13′, 15′) of the second blank, thereby preventing the relative movement thereof during folding or during the formation of the box when the blanks are wound around a volume having pre-determined dimensions. At least two-thirds of the third fold lines (19′) of the second blank are substantially aligned in relation to the first fold lines of the first blank, the lower part (23) of one or more of said third lines including a cut or collapsed portion opposite the corresponding first fold line.
摘要翻译：本发明涉及一种用于形成包装盒的坯料（22），方法和相应的盒子。该组件包括两个波纹板坯件，即：第一坯件（2'），包括通过第一折叠线（9'）彼此连接的折翼，所述坯料的一侧不具有折痕; 和包括通过第三折线（19'）彼此连接的面板（13'，14'，15'，16'）的第二坯料（12'），第二坯料的板分别堆叠在第一个空白没有折叠。第一坯料的两个不相邻的折板（3'，5'）被胶合到第二坯料的两个相应的相对面板（13'，15'），从而防止在折叠期间或在形成盒子期间的相对移动当坯料围绕具有预定尺寸的体积缠绕时。第二坯料的第三折线（19'）的至少三分之二相对于第一坯料的第一折线基本上对准，一条或多条所述第三条线的下部（23）包括切割或与相应的第一折线相对的折叠部分。

10. 发明授权

US06643568B2 System for automatically controlling lift-augmentation devices of an aircraft during take-off 有权
标题翻译：起飞时自动控制飞机起升装置的系统
公开(公告)号：US06643568B2
公开(公告)日：2003-11-04
申请号：US09988264
申请日：2001-11-19
申请人： Dominique Chatrenet , Gérard Mathieu , Fernando Alonso , Martine Cart-Lamy
发明人： Dominique Chatrenet , Gérard Mathieu , Fernando Alonso , Martine Cart-Lamy
IPC分类号： G06F1900
CPC分类号： G05D1/0661 , G05D1/0077
摘要： A system for automatically controlling lift augmentation devices of an aircraft, during a phase of take-off by the aircraft, includes a controllable actuator that shifts the lift-augmentation devices, and a control unit for generating control demands to control the actuator to bring the lift-augmentation devices into a defined position. The control unit further includes a detector that detects actual take-off by the air craft and, if appropriate, signals such detection to the control unit. At start of the take-off phase, the lift-augmentation device are brought into a first position, in which they are deployed. The control unit generates, at least when the detector signals the actual take-off, a control demand making it possible to bring the lift-augmentation devices into a second position, in which the lift-augmentation devices are retracted by comparison with the first position.
摘要翻译：一种用于在飞行器起飞阶段期间自动控制升降机增强装置的系统，包括可升降增加装置移动的可控致动器，以及用于产生控制要求以控制致动器带动升降装置进入限定位置。控制单元还包括检测器，其检测飞行器的实际起飞，并且如果适当的话，将这种检测信号发送到控制单元。在起飞阶段开始时，提升装置进入其展开的第一位置。控制单元至少在检测器发出实际的起飞时产生控制要求，从而使提升增加装置能够进入第二位置，在第二位置，提升增加装置与第一位置相比缩回。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式