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1. 发明授权

US4367529A Automatic braking method and apparatus 失效
标题翻译：自动制动方法及装置
公开(公告)号：US4367529A
公开(公告)日：1983-01-04
申请号：US101139
申请日：1979-12-07
申请人： Jean Masclet , Claude Marcheron
发明人： Jean Masclet , Claude Marcheron
IPC分类号： B60T8/58 , B60T8/17 , B60T8/172 , B60T8/1763 , B60T8/32 , B60T8/36 , B60T8/66 , B60T8/70 , B60T13/66 , B64C25/42 , G06F15/50 , B60T8/02
CPC分类号： B60T8/326 , B60T13/662 , B60T8/1703 , B60T8/325 , B60T8/3655 , B64C25/426
摘要： An automatic braking method and apparatus for a vehicle, having particular applicability to aircraft, wherein a program deceleration signal is generated according to a preselected deceleration. A signal which is a function of the actual speed of the vehicle is compared with the program signal, and a difference signal is produced. The difference signal controls the actuation of the braking system of the vehicle to result in braking thereof in accordance with the preselected deceleration.
摘要翻译：一种用于车辆的自动制动方法和装置，其特别适用于飞行器，其中根据预选减速度产生程序减速信号。将作为车辆的实际速度的函数的信号与程序信号进行比较，并产生差分信号。差分信号控制车辆的制动系统的致动，以根据预选的减速度来制动。

2. 发明授权

US4312485A Landing gear with swing-bar and lateral lifting for aircraft 失效
标题翻译：起落架与摆杆和飞机侧向提升
公开(公告)号：US4312485A
公开(公告)日：1982-01-26
申请号：US107877
申请日：1979-12-26
申请人： Jean Masclet , Andre Turiot
发明人： Jean Masclet , Andre Turiot
IPC分类号： B64C25/12
CPC分类号： B64C25/12
摘要： A main landing gear with swing-bar and lateral lifting for aircraft. Two undercarriages are provided which are positioned symmetrically on either side of the longitudinal plane of symmetry of the aircraft, each one having a leg 1 articulated around a lifting axis 5, and a swing bar 16 around a transverse axis 18. The swing bar 16 carries a wheel 21 pivotally mounted around an axis of rotation 19. The maneuvering of the undercarriage and the bracing thereof are insured by a bracing jack 13, and the deflections of swing-bar 16 are damped by a shock absorber 10. The leg 1 of the undercarriage has a first plane of symmetry (X,X) perpendicular to the lifting axis 5 and the longitudinal plane of symmetry of the aircraft and the swing-bar 16 has a second plane of symmetry (Y,Y) defined by the transverse axis 18 of the axis of rotation 19.
摘要翻译：主起落架带有摆杆和侧向提升飞机。提供两个底架，其对称地位于飞行器的纵向对称平面的任一侧上，每个具有围绕提升轴线5铰接的腿部1和围绕横向轴线18的摆动杆16.摆动杆16承载围绕旋转轴线19枢转地安装的轮21.起落架及其支撑的操纵由支撑插座13保证，摆杆16的偏转由减震器10阻尼。起落架具有垂直于提升轴线5的第一对称平面（X，X），并且飞机的纵向对称平面和摆杆16具有由横向轴线18限定的第二对称平面（Y，Y）的旋转轴线19。

3. 发明授权

US4189192A Apparatus for adjusting the application of brakes to the wheels of various types of vehicles 失效
标题翻译：用于调节制动器对各种车辆的车轮的应用的装置
公开(公告)号：US4189192A
公开(公告)日：1980-02-19
申请号：US914299
申请日：1978-06-09
申请人： Jean Masclet
发明人： Jean Masclet
IPC分类号： B60T8/173 , B60T8/1761 , B60T8/32 , B60T8/08
CPC分类号： B60T8/325 , B60T8/173 , B60T8/17613
摘要： An apparatus for adjusting the braking force of brakes applied to vehicle wheels in which the brakes are operated under the control of an electromagnet as a function of the deceleration and acceleration of the wheels. For a given braking signal, the braking force is eliminated when the deceleration of the braked wheel exceeds a predetermined threshold value, which may occur, for example, when the wheel starts to freely skid, and the reapplication of the braking force is delayed for a period of time proportional to the magnitude of deceleration of the wheel and inversely proportional to the subsequent magnitude of acceleration of the wheel when it picks up speed only when such acceleration exceeds a threshold which permits the wheel to gain speed irrespective of the frictional adherence of the wheel to the ground.
摘要翻译：一种用于调节施加到车轮的制动器的制动力的装置，其中制动器在电磁体的控制下作为车轮的减速和加速度的函数来操作。对于给定的制动信号，当制动车轮的减速度超过例如当车轮开始自由滑动时可能发生的预定阈值时，制动力被消除，并且制动力的再次施加被延迟与车轮减速度的大小成比例的时间段，当车轮的加速度的后续幅度仅当该加速度超过允许车轮获得速度而不考虑摩擦附着力的阈值时，与车轮的加速度的后续幅度成反比。车轮到地面。

4. 发明授权

US4071284A Method and apparatus for effecting double-acting braking 失效
标题翻译：用于双作用制动的方法和装置
公开(公告)号：US4071284A
公开(公告)日：1978-01-31
申请号：US775636
申请日：1977-03-08
申请人： Jean Masclet , Marcel Schott
发明人： Jean Masclet , Marcel Schott
IPC分类号： B60T8/94 , B60T17/18 , B60T17/22 , B64C25/42 , B60T7/12
CPC分类号： B64C25/42 , B60T17/18 , B60T17/22 , B60T8/94
摘要： A method and apparatus for effecting double-acting braking for a wheel or a set of wheels permitting compensation of failures of at least one of the braking circuits of a double-acting braking arrangement of the type comprising at least two sets of braking members and two braking circuits for each brake. A single control action achieved by a single actuating member acts simultaneously on the two braking circuits of each of the brakes and in the case of a failure of one of the two braking circuits resulting in a drop in pressure in the failed braking circuit and consequently in a reduction of the braking torque applied by the brake, the remaining circuit has its pressure increased whereby the braking torque is automatically increased by a predetermined value. For this purpose the control action is applied simultaneously to two relays having at least two operating pressure levels, each relay acting on one of the two sets of braking members via the two braking circuits. Detectors are provided in the respective circuits for detecting failures that may occur in the circuits, the detector associated with one of the circuits controlling the power level of the relay connected to the other circuit and vice versa, whereby the pressure level of the relay associated with the braking circuit that remains in operation is increased when a failure is detected in the other circuit.
摘要翻译：一种用于对车轮或一组车轮进行双作用制动的方法和装置，允许补偿至少一个制动电路的制动电路的故障，所述双作用制动装置包括至少两组制动构件和两组制动构件每个制动器的制动电路。通过单个致动构件实现的单个控制动作同时作用在每个制动器的两个制动电路上，并且在两个制动电路之一的故障的情况下导致失效的制动电路中的压力下降，并且因此在减少由制动器施加的制动转矩，剩余电路的压力增加，由此制动转矩自动增加预定值。为此，控制动作同时应用于具有至少两个操作压力水平的两个继电器，每个继电器经由两个制动电路作用在两组制动构件中的一组上。在各个电路中提供检测器，用于检测电路中可能发生的故障，检测器与控制连接到另一电路的继电器的功率电平的电路之一相关联，反之亦然，因此与当在另一个电路中检测到故障时，保持运行的制动电路增加。

5. 发明授权

US4034958A Independent device for opening and closing rotary valves by remote control 失效
标题翻译：用于通过遥控器打开和关闭旋转阀的独立装置
公开(公告)号：US4034958A
公开(公告)日：1977-07-12
申请号：US575060
申请日：1975-05-06
申请人： Jean Masclet
发明人： Jean Masclet
IPC分类号： F15B15/06 , F15B15/08 , F16K31/163 , F16K31/124 , F16K31/54
CPC分类号： F15B15/065 , F16K31/1635
摘要： A device for opening and closing a rotary valve by remote control comprising a cylinder having a main bore in which a movable unit is slidably mounted in fluid tight manner and which can be displaced in opposite directions by a pressurized fluid supplied by either of two pressurized fluid sources which can be remotely actuated in independent fashion. A sequencing mechanism is mounted in the cylinder for simultaneously applying the pressurized fluid from an activated source to a corresponding end face of the movable unit while connecting the other end face with the atmosphere. The movement of the slidable unit is transmitted to the rotary valve through a rack and pinion arrangement and a linkage composed of cranks and a connecting rod so arranged that when the valve is in either of its end positions it cannot produce movement of the linkage due to alignment of the axis of rotation of the pinion and the connection points of the rod to the cranks.
摘要翻译：一种用于通过遥控器打开和关闭旋转阀的装置，包括具有主孔的气缸，其中可移动单元以流体密封的方式可滑动地安装，并且可以通过由两个加压流体中的任一个供应的加压流体在相反的方向上移位可以独立的方式远程启动。排列机构安装在气缸中，用于将加压流体从活化源施加到可移动单元的相应端面，同时将另一端面与大气连接。可滑动单元的运动通过齿条和小齿轮装置传递到旋转阀，并且由曲柄和连杆组成的连杆被布置成使得当阀处于其任一端时，由于不能产生由于小齿轮的旋转轴线和杆的连接点对曲柄的对准。

6. 发明授权

US4025238A Apparatus for eliminating the effects of cavitation in a main pump 失效
标题翻译：用于消除主泵空化影响的装置
公开(公告)号：US4025238A
公开(公告)日：1977-05-24
申请号：US569087
申请日：1975-04-17
申请人： Jean Masclet
发明人： Jean Masclet
IPC分类号： F04B1/20 , F04B23/02 , F04B23/10 , F04B23/04 , B67D5/62
CPC分类号： F04B23/02 , F04B1/2064 , F04B23/106
摘要： Apparatus for eliminating cavitation in a main pump in which the rotor of a supercharging pump is connected to the rotor of the main pump such that the latter rotor drives the rotor of the supercharging pump. Permanent communication is established between the delivery side of the supercharging pump and the induction inlet of the main pump. A hydraulic fluid reservoir is connected to the inlet of the supercharging pump and it is also connected to the delivery side of the supercharging pump through the intermediary of a valve which controls the flow of hydraulic fluid to the reservoir from the delivery side of the supercharging such that when the pressure at the induction inlet of the main pump exceeds a predetermined value flow is established to the reservoir in order to avoid the appearance of cavitation in the main pump. Leakage flow within the main pump is also recycled to the reservoir continuously through the valve.
摘要翻译：用于消除主泵中气蚀的装置，其中增压泵的转子连接到主泵的转子，使得后者的转子驱动增压泵的转子。在增压泵的输出侧和主泵的进气口之间建立永久的通信。液压油容器连接到增压泵的入口，并且还通过阀门连接到增压泵的输出侧，该阀控制从增压装置的输送侧到储液器的液压流体的流动，当主泵的入口处的压力超过预定值时，建立到储存器的流动，以避免在主泵中出现空化现象。主泵内的泄漏流量也通过阀门连续循环使用。

7. 发明授权

US4312429A Hydraulic braking device for a load subjected to shocks and vibrations 失效
标题翻译：用于受冲击和振动的载荷的液压制动装置
公开(公告)号：US4312429A
公开(公告)日：1982-01-26
申请号：US107876
申请日：1980-04-02
申请人： Jean Masclet , Andre Turiot
发明人： Jean Masclet , Andre Turiot
IPC分类号： F16F9/20 , F16F9/512 , F16L3/20 , F16F9/49
CPC分类号： F16L3/20 , F16F9/20 , F16F9/512
摘要： A hydraulic braking device for a load subjected to shocks and vibrations for the stabilization of loads in thermal or nuclear generating stations.The braking device has a cylinder 1 in which there slides the piston 4 of a rod 7 bearing two flap valves 18 and 19 to brake the passage at high speed of hydraulic fluid from one chamber 15 or 16 to the other. These valves communicate with a reservoir 17, pressurized by springs 31 to 34 and accumulate the expansions of the fluid. A secondary rod 29 which has displacements with respect to rod 7 which are reduced relative to the displacement of piston of reservoir 27 with respect to this rod 7 serves as a leak indicator.Application to the stabilization of loads such as high-temperature steam conduits in thermal or nuclear generating stations.
摘要翻译：用于承受冲击和振动的负载用于稳定热发电站或核发电站负载的液压制动装置。制动装置具有气缸1，其中滑动具有两个活门阀18和19的杆7的活塞4，以将来自一个室15或16的高速液压流体的通道制动到另一个。这些阀与储存器17连通，由储存器17通过弹簧31至34加压并积聚流体的膨胀。相对于杆7具有相对于储存器27的活塞相对于该杆7的位移而减小的次级杆29用作泄漏指示器。适用于热或核发电站的高温蒸汽管道等负荷的稳定化。

8. 发明授权

US4284255A Shock absorbers and shock absorber struts, notably for aerodyne landing gear 失效
标题翻译：减震器和减震器支柱，特别适用于空中起落架
公开(公告)号：US4284255A
公开(公告)日：1981-08-18
申请号：US117657
申请日：1980-02-01
申请人： Jean Masclet , Jacques Veaux
发明人： Jean Masclet , Jacques Veaux
IPC分类号： B64C25/60 , F16F9/06 , F16F9/512 , B64C25/22
CPC分类号： B64C25/60 , F16F9/06 , F16F9/512
摘要： Shock absorbers and shock absorber jacks each of which comprises a shaft containing a low-pressure chamber and sliding in a first chamber of a first cylinder which is separated from another or second chamber which contains a high-pressure chamber, by means of a partition which is traversed by a grooved shaft borne by a separator piston in the other chamber and guided in a sleeve borne by the partition. In the event of the penetration of the shaft into the first cylinder at a rate of very much higher than normal, then the two grooves in the shaft communicate with each other and permit the flow of oil from the first chamber towards the second chamber and towards the low-pressure chamber because of a radial passage through the sleeve near the partition.
摘要翻译：减震器和减震器千斤顶各自包括一个包含低压室的轴，并在第一气缸的第一室中滑动，第一气缸与包含高压室的另一个或第二室分离，借助于隔板，由在另一个室中由分离器活塞承载的带槽的轴横穿，并在由隔板承载的套筒中引导。在以比正常高得多的速率将轴穿入第一气缸的情况下，轴中的两个沟槽彼此连通并且允许油从第一室朝向第二室流动并且朝向低压室由于径向通过套筒靠近隔板。

9. 发明授权

US4241814A Mechanical-hydraulic damper for a load subject to shocks and vibrations 失效
标题翻译：用于受冲击和振动的负载的机械液压阻尼器
公开(公告)号：US4241814A
公开(公告)日：1980-12-30
申请号：US886347
申请日：1978-03-14
申请人： Jean Masclet
发明人： Jean Masclet
IPC分类号： F16F9/00 , F16D57/06 , F16F9/12 , F16F9/14 , F16L3/20 , F16L3/202 , F16L3/217 , F16L55/02 , G21D1/02
CPC分类号： F16L3/202 , F16D57/06 , F16F9/12 , F16F9/14 , F16L3/20 , F16L3/217 , F16L55/02 , G21D1/02 , F16F2232/06 , Y02E30/40 , Y10T74/1872
摘要： A mechanical-hydraulic damper for a load which is subject to shocks and vibrations, comprising a co-operating pair of elements, the first of the pair of elements being mounted in a body for relative axial movement in relation to the body and the second of the pair of elements being rotatably mounted in the body and so coupled to the first element that relative axial movement of the first element causes rotation of the second element which is coupled to a hydraulic system which resists sudden or rapid rotation of the second element. The pair of co-operating elements may comprise a screw-nut assembly. The hydraulic system may comprise a reversible pump driven by the rotatable element and pumping hydraulic fluid round a closed circuit including a throttling orifice. Alternatively the hydraulic system may comprise a rotary laminar hydraulic damper filled with high viscosity oil.
摘要翻译：一种用于承受冲击和振动的负载的机械液压阻尼器，包括一对配合的元件，所述一对元件中的第一个元件安装在主体中，用于相对于主体相对轴向移动，第二个元件所述一对元件可旋转地安装在所述主体中并且联接到所述第一元件，所述第一元件的相对轴向运动引起所述第二元件的旋转，所述第二元件联接到抵抗所述第二元件的突然或快速旋转的液压系统。一对协作元件可以包括螺母 - 螺母组件。液压系统可以包括由可旋转元件驱动的可逆泵，并且在包括节流孔的闭合回路的周围泵送液压流体。或者，液压系统可以包括填充有高粘度油的旋转层流液压阻尼器。

10. 发明授权

US4189117A Retractable fuselage mounted undercarriage 失效
标题翻译：可伸缩机身安装起落架
公开(公告)号：US4189117A
公开(公告)日：1980-02-19
申请号：US882640
申请日：1978-03-02
申请人： Jean Masclet , Andre Turiot
发明人： Jean Masclet , Andre Turiot
IPC分类号： B64C25/10 , B64C25/12
CPC分类号： B64C25/10 , B64C2025/125
摘要： A retractable fuselage mounted undercarriage comprising a leg casing mounted to pivot on a main universal joint about an axis which extends longitudinally of the aircraft, the leg casing mounting a wheel assembly which can pivot on the leg casing, a lateral deflection shock absorber and a manoeuvreing and wind bracing jack each connected to the leg casing by a joint and each connected to the fuselage by a joint, the main universal joint being mounted to pivot on the fuselage about an inclined retraction axis which does not pass through the point where the shock absorber is connected to the fuselage, so that, during lowering and retraction of the undercarriage effected by extending or retracting the manoeuvreing and wind bracing jack, the shock absorber acts as a directer bar and orientates the axis of the leg casing, which leg casing is rotated as the main universal joint pivots on the fuselage about the inclined retraction axis.
摘要翻译：一种可缩回的机身安装的底架，包括一个腿部外壳，该腿部外壳安装成围绕一个沿着飞行器纵向延伸的轴线在主万向接头上枢转，该腿部外壳安装一个可在腿部壳体上枢转的车轮组件，一个侧向偏转减震器和一个操纵杆和风力支撑千斤顶，各自通过接头连接到腿部壳体，并且每个通过接头连接到机身，主通用接头被安装成绕机身枢转，该倾斜回缩轴线不穿过减震器连接到机身，使得在通过延伸或缩回操纵杆和风支撑吊架来实现底架的降低和缩回期间，减震器用作定向杆，并且使腿部壳体旋转的腿部壳体的轴线因为主通用接头在机身上围绕倾斜的回退轴线枢转。

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