会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 7. 发明申请
    • HYDRAULIC UNIT OF A HYDRAULIC VEHICLE BRAKE SYSTEM
    • 液压车辆刹车系统液压单元
    • US20100263368A1
    • 2010-10-21
    • US12305704
    • 2007-11-30
    • Bernhard GnammAndreas Weh
    • Bernhard GnammAndreas Weh
    • F15B7/10
    • B60T8/3685
    • The invention relates to a hydraulic unit of a vehicle hydraulic brake system having a hydraulic block, a storage unit, and a holding unit. The storage unit is inserted into the hydraulic block, and the holding unit is adjusted for holding the hydraulic block locally fixed to an associated vehicle. The storage unit is constructed with a holding surface which forms a section of the outer side of the hydraulic unit, and the holding unit engages with the holding surface of the storage unit in order to hold the hydraulic block locally fixed above the storage unit. Furthermore, the invention also relates to a storage unit where one outer surface of the storage unit which forms an outer side of the hydraulic unit is constructed as a holding surface for attaching the hydraulic block in the vehicle.
    • 本发明涉及具有液压块,存储单元和保持单元的车辆液压制动系统的液压单元。 存储单元被插入到液压块中,并且保持单元被调节以将液压块保持在局部固定到相关联的车辆上。 存储单元构造有形成液压单元的外侧的一部分的保持表面,并且保持单元与存储单元的保持表面接合,以将液压块保持在局部固定在存储单元上方。 此外,本发明还涉及一种存储单元,其中形成液压单元的外侧的存储单元的一个外表面被构造为用于将液压块连接在车辆中的保持表面。
    • 9. 发明申请
    • HYDRAULIC SYSTEM FOR AIRCRAFT
    • 航空液压系统
    • US20090242694A1
    • 2009-10-01
    • US12413818
    • 2009-03-30
    • Hiroki Oyama
    • Hiroki Oyama
    • B64C13/36F16L55/04F15B7/10
    • F15B1/022F15B20/004F15B2211/212F15B2211/8633F15B2211/8757
    • A hydraulic system for aircraft operating devices provides a secondary pressure source for direction and deceleration control in case of loss of pressure from a primary pressure source. The system includes multiple pressure accumulators that include a primary accumulator, which supplies pressurized fluid to a first actuator, and first and second secondary accumulators, which supply pressurized fluid to second and third actuators, respectively. If the primary accumulator is disabled, the first secondary accumulator will supply pressurized fluid to the first actuator. If the first secondary accumulator is disabled, the second secondary accumulator will supply pressurized fluid to the second actuator. By providing multiple, substantially independent accumulators, direction and deceleration control is maintained even in the event of loss of the primary accumulator.
    • 用于飞机操作装置的液压系统在来自主压力源的压力损失的情况下提供用于方向和减速控制的二次压力源。 该系统包括多个压力蓄能器,其包括向第一致动器供应加压流体的主蓄能器,以及分别向第二和第三致动器供应加压流体的第一和第二次级蓄能器。 如果主蓄能器被禁用,则第一副蓄能器将向第一致动器供给加压流体。 如果第一次级蓄能器被禁用,则第二辅助蓄能器将向第二致动器供应加压流体。 通过提供多个基本独立的蓄能器,即使在主蓄能器损失的情况下也能够保持方向和减速控制。
    • 10. 发明授权
    • Hydraulic pressure generator with vibration damping
    • 液压发电机具有减振功能
    • US5878578A
    • 1999-03-09
    • US700461
    • 1996-09-13
    • Leonardo Cadeddu
    • Leonardo Cadeddu
    • B60T11/16B60T11/18F15B7/10
    • B60T11/18B60T11/16
    • A hydraulic pressure generator having a body (1) with a first bore (11) therein for receiving a cylinder (21) of a piston assembly (2) to define a pressure chamber (12). The cylinder (21) has a second bore (211) for receiving an auxiliary piston (22) which defines a variable volume compensation chamber (23). The compensation chamber encloses a deformable member (5) which is adapted to exert an elastic force between the auxiliary piston (22) and a closed end (210) of cylinder (21). The compensation chamber (23) communicates with the pressure chamber (12) through a restriction (221) formed in a longitudinal duct (222) of the auxiliary piston (22). A sealing member (4) borne by a portion (222) of the auxiliary piston (22) closes the pressure chamber (12) such that the elastomeric member (5) dampens pressure differences between the pressure chamber (12) and compensation chamber (23).
    • PCT No.PCT / EP96 / 03880 Sec。 371日期1996年9月13日 102(e)1996年9月13日PCT PCT 1996年9月4日PCT公布。 公开号WO97 / 18115 PCT 日期1997年5月22日一种液压发生器,其具有主体(1),其中具有第一孔(11),用于容纳活塞组件(2)的气缸(21)以限定压力室(12)。 气缸(21)具有用于容纳限定可变体积补偿室(23)的辅助活塞(22)的第二孔(211)。 补偿室包围可变形构件(5),该可变形构件适于在辅助活塞(22)和气缸(21)的封闭端(210)之间施加弹性力。 补偿室23通过形成在辅助活塞(22)的纵向管道(222)中的限制(221)与压力室(12)连通。 由辅助活塞(22)的部分(222)承载的密封构件(4)封闭压力室(12),使得弹性构件(5)抑制压力室(12)和补偿室(23)之间的压力差 )。