公开(公告)号：EP0330318B1

公开(公告)日：1991-10-23

申请号：EP89300936.5

申请日：1989-01-31

申请人： Aeroquip AG

发明人： Fournier, Paul J. E. ,  Kulikowski, Ernest F.

IPC分类号： B67D5/37 ,  B67D5/377

CPC分类号： B67D7/46 ,  B64F1/28

公开(公告)号：EP0316080A3

公开(公告)日：1990-05-30

申请号：EP88309811.3

申请日：1988-10-19

申请人： Aeroquip AG

发明人： Laipply, Robert A. ,  Fuerst, Phillip G. ,  Mack, Brian A.

IPC分类号： F16L37/28

CPC分类号： F16L37/40 ,  Y10T137/87965

摘要： A coupling for use with pressurized systems permitting coupling of valved coupling parts even though one of the parts may be under high pressure. An axially reciprocal valve (28') which automatically opens upon the coupling halves being connected is guided within a shell (50) within the pressurized coupling half and a sealed relationship between the valve and shell minimizes the area of valve surfaces exposed to the pressurized medium reducing the axial forces imposed upon the valve toward the closed position. A bleed valve (64) communicating with the valve interior permits valve operation with hydraulic systems in the event of seal leakage.

公开(公告)号：EP0309131A3

公开(公告)日：1989-12-20

申请号：EP88308411.3

申请日：1988-09-12

申请人： Aeroquip AG

发明人： Laipply, Robert A. ,  Fournier, Paul J. E.

IPC分类号： F01M11/04

CPC分类号： F01M11/0408 ,  F01M2011/0425

摘要： The invention pertains to an oil drain fitting for internal combustion engines which permits a quick draining of the oil. A body [10] threaded into the conventional oil pan drain hole [9] includes an axial passage [12] having a tubular valve [30] reciprocally mounted therein. The valve [30] is open at its lower end [34] and closed at its inner end [36] having a head [38] which seats against the inner end [16] of the body [10]. The lower end [34] of the valve [30] includes an abutment surface [48] for engagement by a drain conduit fitting for axially displacing the valve [30] inwardly to open the valve and permit flow therethrough. A cap [54] may be mounted on the body to enclose the lower end of the valve when the fitting is not in use.

公开(公告)号：EP0330318A1

公开(公告)日：1989-08-30

申请号：EP89300936.5

申请日：1989-01-31

申请人： Aeroquip AG

发明人： Fournier, Paul J. E. ,  Kulikowski, Ernest F.

IPC分类号： B67D5/37 ,  B67D5/377

CPC分类号： B67D7/46 ,  B64F1/28

摘要： The invention pertains to an automatic shut-off refueling nozzle (10) particularly suitable for use with military vehicles employing a nozzle having a liquid level sensor (20,22) operating a flow valve (12), the nozzle includes a lug plate (60) attachable to the inlet (74) of the tank receptacle being filled wherein once attached to the tank inlet (74) the presence of an operator is not required during refueling. A diverger (26) on the nozzle spout (14) improves flow characteristics within the tank inlet (74) to prevent immature release of the nozzle flow valve (12) and the nozzle prevents contamination during refueling and prevents spillage of volatile fuels even though unattended. An embodiment of the invention utilizes a secondary control valve (138) preventing fluid flow until the nozzle has been fully connected to the tank inlet.

摘要翻译： 本发明涉及一种特别适用于使用具有操作流量阀（12）的液位传感器（20,22）的喷嘴的军用车辆的自动关闭加油喷嘴（10），该喷嘴包括一个凸耳板（60） ），其可连接到正在填充的储罐容器的入口（74），其中一旦连接到罐入口（74），在加油期间不需要操作者的存在。 喷嘴喷口（14）上的分流器（26）改善了罐入口（74）内的流动特性，以防止喷嘴流量阀（12）的不成熟释放，并且喷嘴在加油期间防止污染，并且防止挥发性燃料的溢出，即使无人值守 。 本发明的一个实施例利用二次控制阀（138）来防止流体流动，直到喷嘴已经完全连接到罐入口。

公开(公告)号：EP0286353A1

公开(公告)日：1988-10-12

申请号：EP88303014.0

申请日：1988-04-05

申请人： Aeroquip AG

发明人： Hawley, Frank D. ,  Rogers, Russell L. ,  Allread, Alan R. ,  Fournier, Paul J. E.

IPC分类号： B67D5/37

CPC分类号： B67D7/42 ,  B64F1/28 ,  Y10T137/6881 ,  Y10T137/88054

摘要： A fueling nozzle (10) for pressurized fuel systems having a body (12) connectable to a tank inlet. The body includes an axially displaceable valve (112) movable between a closed retracted position and an extended open position. Connection of the body to the tank inlet occurs upon rotation of the connection sleeve (68) and positioning of the valve is achieved by a rotatable cam sleeve (36) having a cam slot (46) in which a valve-mounted follower (142) is located. An interlock (82) senses mounting of the body on the tank inlet permitting rotation of the connection sleeve in a locking direction and upon the connection sleeve being fully rotated to a locked condition a second interlock (98) permits rotation of the cam sleeve and valve movement from the closed to the open position. The nozzle is characterized by reduced flow resistance characteristics and safe operation.

摘要翻译： 一种用于加压燃料系统的燃料喷嘴（10），其具有可连接到罐入口的主体（12）。 主体包括可在闭合缩回位置和延伸打开位置之间移动的可轴向移动的阀（112）。 当连接套筒（68）旋转时，主体与罐入口的连接发生，并且通过具有凸轮槽（46）的可旋转的凸轮套筒（36）实现阀的定位，在该凸轮槽内安装有阀安装的从动件（142） 位于。 互锁（82）感测到主体在罐入口上的安装，允许连接套筒沿锁定方向旋转，并且在连接套筒完全旋转到锁定状态时，第二互锁（98）允许凸轮套筒和阀 运动从关闭到打开位置。 喷嘴的特点是流动阻力特性降低，安全运行。

公开(公告)号：EP0245927A3

公开(公告)日：1988-09-21

申请号：EP87302178

申请日：1987-03-13

申请人： Aeroquip AG

发明人： Smith, Donald E. ,  Haunhorst, Greg A.

IPC分类号： B66C01/34 ,  B64D01/22

CPC分类号： B64D1/22 ,  B66C1/34

摘要： A releasable self-resetting cargo hook for heli­copters and other aircraft for supporting suspended loads. The cargo hook apparatus includes a pivotally supported load arm (78) maintained in its load supporting condition by a pivotally mounted latch arm (100) whose posi­tion, in turn, is controlled by a pivotally mounted latch (120). The position of the latch (120) is determined by a pivotally mounted lock arm lever (142) whose normal position is determined by a stop pin (156) and which is operated by a release mechanism (146). The interconnection between the latch (120) and lock arm lever (142) is through a cam slot (132) defined on the latch (120) receiving a lock arm lever follower (150), and the cam slot-follower relationship prevents impact forces imposed on the cargo hook structure from inad­vertently producing lock arm lever rotation and latch movement.

公开(公告)号：EP0160758B1

公开(公告)日：1988-08-10

申请号：EP84303084.2

申请日：1984-05-08

申请人： Aeroquip AG

发明人： Haubert, Steven D. ,  Indrelunas, Stephen T.

IPC分类号： F16L33/20

CPC分类号： F16L33/2078 ,  Y10T29/49913 ,  Y10T29/49927

公开(公告)号：EP0163386A3

公开(公告)日：1987-04-01

申请号：EP85302300

申请日：1985-04-02

申请人： AEROQUIP AG

发明人： Hughes, Brett A. ,  Gilbert, David L. ,  Ellerbrock, Eugene A.

IPC分类号： F16L33/20

CPC分类号： F16L33/2073 ,  Y10S285/903

摘要： The invention pertains to the attachment of a wrenching nut to a metal conduit wherein torque forces can be applied to the conduit through the nut. An annular nut member is located upon a conduit and the conduit is radially deformed to force the conduit material into engagement with keying surfaces defined upon the nut. Conduit deformation occurs on both sides of the nut for axial positioning thereof, as well as establishing a torque transmitting relationship between the nut and conduit.

公开(公告)号：EP0152212A3

公开(公告)日：1986-10-08

申请号：EP85300523

申请日：1985-01-25

申请人： AEROQUIP AG

发明人： Fournier, Paul J. E.

IPC分类号： F16L17/06

CPC分类号： F16J15/025 ,  F16L17/073

摘要： The invention pertains to a face seal having lateral portions bridged by segments homogeneously defined by the elastomer material of the seal. The circumferentially spaced bridge segments define voids between the lateral portions providing clearance to accommodate the seal material during swelling, and also permit the seal to be manufactured slightly "oversize" to compensate for shrinkage without adversely affecting its sealing abilities and operation.

公开(公告)号：EP0095231B1

公开(公告)日：1986-06-11

申请号：EP83301702.3

申请日：1983-03-25

申请人： Aeroquip AG

发明人： Graves, Robert W.

IPC分类号： F16L27/02

CPC分类号： F16L27/0857