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1. 发明申请

US20090065640A1 BRAKING-ENERGY EQUALIZATION SYSTEM 有权
标题翻译：制动能量均衡系统
公开(公告)号：US20090065640A1
公开(公告)日：2009-03-12
申请号：US12168958
申请日：2008-07-08
申请人： Olivier Regis , Kevin Scott , Emmanuel Ray
发明人： Olivier Regis , Kevin Scott , Emmanuel Ray
IPC分类号： B64C25/42
CPC分类号： B60T8/1703 , B64C25/426
摘要： A braking-energy equalization system applied to an aircraft undercarriage, which undercarriage includes at least two sets of landing gear, with each set of landing gear including at least two wheels and with each of wheels being equipped with a brake, wherein the system includes means intended to introduce a delay time to delay the braking of the brakes having a higher braking torque in comparison with the other brakes having a lower braking torque, so as to equalize the braking energies absorbed by the brakes of the landing gear during the landing or during an interrupted takeoff of the aircraft.
摘要翻译：一种应用于飞机起落架的制动能量均衡系统，其底盘包括至少两组起落架，每组起落架包括至少两个车轮，并且每个车轮配备有制动器，其中该系统包括装置旨在引入延迟时间来延迟具有较高制动转矩的制动器的制动，与具有较低制动转矩的其他制动器相比较，以便在着陆期间或期间在等于起落架制动器吸收的制动能量飞机中断起飞。

2. 发明申请

US20090065635A1 Pitch-oscillation limitation system applied to an aircraft 有权
标题翻译：应用于飞机的俯仰振荡限制系统
公开(公告)号：US20090065635A1
公开(公告)日：2009-03-12
申请号：US12168988
申请日：2008-07-08
申请人： OLIVIER REGIS , GREGORY SICAULT , EMMANUEL KOPP
发明人： OLIVIER REGIS , GREGORY SICAULT , EMMANUEL KOPP
IPC分类号： B64C25/26 , B64C25/42
CPC分类号： B64C25/426
摘要： A pitch-oscillation limitation system, applied to an aircraft having main landing gear located toward the center of the aircraft and forward landing gear located under the nose of the aircraft, wherein the system includes means for automatically applying, in the event of sudden braking, time-deferred braking between the wheels of the landing gear under the wings and the wheels of the landing gear under the fuselage, so as to reduce the amplitude of the aircraft's pitching motion.
摘要翻译：一种俯仰振动限制系统，其应用于具有朝向飞机中心的主起落架和位于飞行器的鼻子下方的前起落架的飞机，其中该系统包括在突然制动的情况下自动应用的装置，在机翼下的起落架的轮子与机身下的起落架的轮子之间的时间延迟制动，以便减小飞机的俯仰运动的幅度。

3. 发明授权

US08317131B2 Braking-energy equalization system 有权
标题翻译：制动能均衡系统
公开(公告)号：US08317131B2
公开(公告)日：2012-11-27
申请号：US12168958
申请日：2008-07-08
申请人： Olivier Regis , Kevin Scott , Emmanuel Ray
发明人： Olivier Regis , Kevin Scott , Emmanuel Ray
IPC分类号： B64C25/42
CPC分类号： B60T8/1703 , B64C25/426
摘要： A braking-energy equalization system applied to an aircraft undercarriage, which undercarriage includes at least two sets of landing gear, with each set of landing gear including at least two wheels and with each of wheels being equipped with a brake, wherein the system includes means intended to introduce a delay time to delay the braking of the brakes having a higher braking torque in comparison with the other brakes having a lower braking torque, so as to equalize the braking energies absorbed by the brakes of the landing gear during the landing or during an interrupted takeoff of the aircraft.
摘要翻译：一种应用于飞机起落架的制动能量均衡系统，其底盘包括至少两组起落架，每组起落架包括至少两个车轮，并且每个车轮配备有制动器，其中该系统包括装置旨在引入延迟时间来延迟具有较高制动转矩的制动器的制动，与具有较低制动转矩的其他制动器相比较，以便在着陆期间或期间在等于起落架制动器吸收的制动能量飞机中断起飞。

4. 发明授权

US08132757B2 Pitch-oscillation limitation system applied to an aircraft 有权
标题翻译：应用于飞机的俯仰振荡限制系统
公开(公告)号：US08132757B2
公开(公告)日：2012-03-13
申请号：US12168988
申请日：2008-07-08
申请人： Olivier Regis , Gregory Sicault , Emmanuel Kopp
发明人： Olivier Regis , Gregory Sicault , Emmanuel Kopp
IPC分类号： B64F1/02
CPC分类号： B64C25/426
摘要： A pitch-oscillation limitation system, applied to an aircraft having main landing gear located toward the center of the aircraft and forward landing gear located under the nose of the aircraft, wherein the system includes means for automatically applying, in the event of sudden braking, time-deferred braking between the wheels of the landing gear under the wings and the wheels of the landing gear under the fuselage, so as to reduce the amplitude of the aircraft's pitching motion.
摘要翻译：一种俯仰振动限制系统，其应用于具有朝向飞机中心的主起落架和位于飞行器的鼻子下方的前起落架的飞机，其中该系统包括在突然制动的情况下自动应用的装置，在机翼下的起落架的轮子和机身下的起落架的车轮之间的时间延迟制动，以便减小飞机的俯仰运动的幅度。

5. 发明授权

US5511430A Method and device for detecting that the design loads of an aircraft have been exceeded 失效
标题翻译：用于检测飞机的设计负载已经被超过的方法和装置
公开(公告)号：US5511430A
公开(公告)日：1996-04-30
申请号：US350082
申请日：1994-11-29
申请人： Thierry Delest , Olivier Regis , Patrick Schuster
发明人： Thierry Delest , Olivier Regis , Patrick Schuster
IPC分类号： G01G19/07 , G05D1/00 , G01M5/00
CPC分类号： G05D1/0066 , G01G19/07
摘要： The invention relates to a method for detecting that the design loads of an aircraft have been exceeded during landing.According to the invention:--in a preliminary step:the load criteria (C1, C2, . . . , Cp) are defined; andthe laws of variation of the allowable values (C1ad, C2ad, . . . , Cpad) of these load criteria (C1, C2, . . . , Cp) are determined, as a function of input parameters (P1, P2, . . . , Pn); and--at the moment of landing:the values of the said input parameters (P1, P2, . . . , Pn) and of the said load criteria (C1, C2, . . . , Cp) are measured;the allowable values (C1ad, C2ad, . . . , Cpad) of the said load criteria (C1, C2, . . . , Cp) are calculated;for each of the said load criteria (C1, C2, . . . , Cp), the measured effective value (C1m, C2m, . . . , Cpm) is compared with the calculated allowable value (C1ad, C2ad, . . . , Cpad); andit is determined whether a structural inspection must be carried out.
摘要翻译：本发明涉及一种用于检测在着陆期间飞机的设计载荷已被超过的方法。根据本发明：在初步步骤中：定义负载标准（C1，C2，...，Cp）; 并且确定这些负载标准（C1，C2，...，Cp）的允许值（C1ad，C2ad，...，Cpad）的变化规律，作为输入参数（P1，P2，...）的函数。 ...，Pn）; 并且在着陆时刻：测量所述输入参数（P1，P2，...，Pn）的值和所述负载标准（C1，C2，...，Cp）的值; 计算所述负载标准（C1，C2，...，Cp）的允许值（C1ad，C2ad，...，Cpad）对于每个所述负载标准（C1，C2，...，Cp），将测量的有效值（C1m，C2m，...，Cpm）与计算的允许值（C1ad，C2ad，...， Cpad）; 确定是否必须进行结构检查。

6. 发明授权

US07552629B2 Movable tyre test bench and method therefor 有权
标题翻译：可移动轮胎试验台及其方法
公开(公告)号：US07552629B2
公开(公告)日：2009-06-30
申请号：US10588907
申请日：2005-02-09
申请人： Olivier Regis , Nicolas Lastere , Gerard Sevelinge
发明人： Olivier Regis , Nicolas Lastere , Gerard Sevelinge
IPC分类号： G01M17/02
CPC分类号： G01M17/02
摘要： A mobile test rig for tires, composed of a self-driven platform capable of following rectilinear and circular trajectories and including: a test instrument module for a wheel-tire assembly to be tested that permits the assembly to be orientated in all directions, to lean the assembly and apply a vertical effort to the assembly, first swivelling axles, equipped with suspensions and driving wheels, a processing unit associated to a memory, and a control of the test cycle permitting orientation of the assembly to be controlled, as well as a load applied to the assembly.
摘要翻译：一种用于轮胎的移动式测试台，由能够跟随直线和圆形轨迹的自驱动平台组成，包括：用于待测试的轮胎轮胎组件的测试仪器模块，其允许组装在所有方向上定向到倾斜组装并对组装施加垂直的努力，第一旋转轴，配备悬架和驱动轮，与存储器相关联的处理单元，以及允许控制组件的取向的测试循环的控制，以及施加到组件的负载。

7. 发明申请

US20080282789A1 Movable Tyre Test Bench and Method Therefor 有权
标题翻译：可移动轮胎试验台及其方法
公开(公告)号：US20080282789A1
公开(公告)日：2008-11-20
申请号：US10588907
申请日：2005-02-09
申请人： Olivier Regis , Nicolas Lastere , Gerard Sevelinge
发明人： Olivier Regis , Nicolas Lastere , Gerard Sevelinge
IPC分类号： G01M17/02
CPC分类号： G01M17/02
摘要： A mobile test rig for tires, composed of a self-driven platform capable of following rectilinear and circular trajectories and including: a test instrument module for a wheel-tire assembly to be tested that permits the assembly to be orientated in all directions, to lean the assembly and apply a vertical effort to the assembly, first swivelling axles, equipped with suspensions and driving wheels, a processing unit associated to a memory, and a control of the test cycle permitting orientation of the assembly to be controlled, as well as a load applied to the assembly.
摘要翻译：一种用于轮胎的移动式测试台，由能够跟随直线和圆形轨迹的自驱动平台组成，包括：用于待测试的轮胎轮胎组件的测试仪器模块，其允许组装在所有方向上定向到倾斜组装并对组装施加垂直的努力，第一旋转轴，配备悬架和驱动轮，与存储器相关联的处理单元，以及允许控制组件的取向的测试循环的控制，以及施加到组件的负载。

8. 发明授权

US08340838B2 Differential braking system 有权
标题翻译：差速制动系统
公开(公告)号：US08340838B2
公开(公告)日：2012-12-25
申请号：US12168975
申请日：2008-07-08
申请人： Olivier Regis , Kevin Scott , Gregory Sicault
发明人： Olivier Regis , Kevin Scott , Gregory Sicault
IPC分类号： B64C19/00 , B64C25/42 , G06F17/00 , B62D6/00
CPC分类号： B64C25/48 , B60T8/1703
摘要： A braking system for the landing gear of an aircraft, which landing gear includes a bogey containing at least four wheels, each equipped with a brake, with the bogey having at least two axles that are connected to the aircraft by a telescoping strut, wherein when the aircraft makes a low-speed turn around a center of rotation, the straight line linking the center of rotation of the turn to the barycenter of the landing gear does not pass between the front wheels and the rear wheels of the landing gear which system further includes means for applying differential braking between the front wheels and the rear wheels of the landing gear.
摘要翻译：一种用于飞机起落架的制动系统，该起落架包括一个包含至少四个轮子的铲斗，每个车架都配备有一个制动器，其中该装置具有至少两个通过伸缩支柱连接到飞行器的轴，其中当飞机围绕旋转中心进行低速转弯，将转弯旋转中心连接到起落架的重心的直线不会通过起落架的前轮和后轮之间，该系统进一步包括用于在起落架的前轮和后轮之间施加差速制动的装置。

9. 发明申请

US20090069958A1 SYSTEME DE FREINAGE DIFFERENTIEL 有权
标题翻译：系统差异不明显
公开(公告)号：US20090069958A1
公开(公告)日：2009-03-12
申请号：US12168975
申请日：2008-07-08
申请人： OLIVIER REGIS , KEVIN SCOTT , GREGORY SICAULT
发明人： OLIVIER REGIS , KEVIN SCOTT , GREGORY SICAULT
IPC分类号： B64C25/48 , G06F17/00
CPC分类号： B64C25/48 , B60T8/1703
摘要： A braking system for the landing gear of an aircraft, which landing gear includes a bogey containing at least four wheels, each equipped with a brake, with the bogey having at least two axles that are connected to the aircraft by a telescoping strut, wherein when the aircraft makes a low-speed turn around a center of rotation, the straight line linking the center of rotation of the turn to the barycenter of the landing gear does not pass between the front wheels and the rear wheels of the landing gear which system further includes means for applying differential braking between the front wheels and the rear wheels of the landing gear.
摘要翻译：一种用于飞机起落架的制动系统，该起落架包括一个包含至少四个轮子的铲斗，每个车架都配备有一个制动器，其中该装置具有至少两个通过伸缩支柱连接到飞行器的轴，其中当飞机围绕旋转中心进行低速转弯，将转弯旋转中心连接到起落架的重心的直线不会通过起落架的前轮和后轮之间，该系统进一步包括用于在起落架的前轮和后轮之间施加差速制动的装置。

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