DEVICE FOR MEASURING PARAMETER PARTICULARLY RELATING TO WHEEL OF AIRCRAFT OR VEHICLE

    公开(公告)号:JPH06211011A

    公开(公告)日:1994-08-02

    申请号:JP31574192

    申请日:1992-10-30

    Applicant: LABINAL

    Abstract: PURPOSE: To obtain a tire pressure measuring apparatus having a high reliability and a sufficient accuracy and allowing the cost down by transferring a pressure signal from a pressure sensor subject to drift conditioned by temp., together with a temp. signal to a processor for computing corrections to the pressure measuring signal value from signal values representative of the interference. CONSTITUTION: A pressure sensor 1 attached to the rim of a wheel sends data through a line 2 to a processor electronic circuit 3, the processor converts the data from the sensor 1 to binary signals, and the signals are sent through coupling means 5 having a rotary transformer over a line 4 to a computer 6. According to commands from the electronic circuit 3, the pressure first measured by the sensor 1 and factors then measured by the sensor 1 such as temp. are recorded. The data are conditioned by the processor electronic circuit 3 and sent to the computer 6 which corrects the signals according to received temp. values and corrects measured pressure parameters and processor means process them.

    MOISTURE REMOVING DEVICE FOR LIGHT OIL FED TO DIESEL ENGINE

    公开(公告)号:JPH01310160A

    公开(公告)日:1989-12-14

    申请号:JP8988989

    申请日:1989-04-11

    Applicant: LABINAL

    Inventor: JIYAAN PAAJIYU

    Abstract: PURPOSE: To prevent suction of water and air by detecting that the volume of water separated from the diesel oil in a water collecting tank is above a warning threshold and actuating an electric draining pump at engine start-up. CONSTITUTION: Diesel oil G in a tank 1 is driven by a diesel oil extraction pump 4 to circulate in a supply pipe 2, a sink tank (water collecting tank) 3 and a return pipe 6, and supplied to a diesel engine M by a diesel engine injection pump 5. At that time, as a second switch 13 is opened by a an ignition key 14, a draining pump 9 is not actuated so that a non-return valve 11 is closed and no outside air 10 is sucked. When the engine M is actuated, the second switch 13 is closed by the key 14. When the boundary surface S of the water E in the water collecting tank 3 is above a warning threshold it is detected by a floater 7. A first switch 8 is closed. The draining pump 9 is driven to drain water. When actuation is finished, the switch 13 is opened. Thus, it is possible to prevent water or air from being sucked into the engine.

    ELECTRIC CONNECTOR
    14.
    发明专利

    公开(公告)号:JPH1021989A

    公开(公告)日:1998-01-23

    申请号:JP3814297

    申请日:1997-02-21

    Abstract: PROBLEM TO BE SOLVED: To provide an electric connector durable in the surrounding environments for specified use by improving the combination and arrangement of constituent elements. SOLUTION: This electric connector 30 may comprises a housing 32, a contact 34, auxiliary locks 36, 38, grommets 40, 42, a back plate 44, a bolt 46, a contact taking out tool 48, and a splash guard 50. The housing 32 contains an aperture 52 to receive the contact 34. The contact 34 is bent and connected with a wire 60 to compose a contact-wire assembled body 61. The grommets 40, 42 are installed in a recessed part in the rear face of the housing 32. The grommets 40, 42 form a rather reliable weather resistant seal. The housing 32 and the back plate 44 are so designed as to expose the grommets 40, 42 to compressive force in order to improve the sealing property of the grommets 40, 42.

    STRUCTURE OF ROTATING DEVICE OF LANDING GEAR

    公开(公告)号:JPH0648396A

    公开(公告)日:1994-02-22

    申请号:JP21637191

    申请日:1991-08-02

    Applicant: LABINAL

    Abstract: PURPOSE: To readily mount and demount with a simple structure of a rotary apparatus for a landing gear and accordingly fairly economically maintain it. CONSTITUTION: In a structure of a rotary apparatus of a landing gear of an aircraft, there is provided a modular assembly of one unit which is disposed in a wheel axle 1 of a wheel of the landing gear of the aircraft. This apparatus comprises a rotor 9 mounted in a stator 7 by a stator 7 and two rolling bearings. The stator 7 and rotor 9 are divided into two parts of the stator 7 and two parts of the rotor 9, respectively, and the two parts of the rotor 9 form an electric signal generator, and an electromagnetic coupling of a rotating transformer type for a sensor supported by a wheel, respectively.

    EXCESSIVELY MOLDED SHIELD CONNECTOR

    公开(公告)号:JPH0594851A

    公开(公告)日:1993-04-16

    申请号:JP29670891

    申请日:1991-08-28

    Abstract: PURPOSE: To retain correct eartking by forming pivot detents in a shielding cover of an electric connector by punching and surely contacting a cover tub of a shielding member which a connector shell in the case of complete closing. CONSTITUTION: A lip 62 of a shield 22 is extended between an inner rim of a flange 44 and a tail part of a dielectric housing through a slot space in an aperture 44 and hooked in a recessed part 45 in a rear part shell 18. Then, a shielding member is set closer to the cable side until pivot detents 58, 60 contact with a dielectric housing 27. The height of the insertion space, effective thickness of the shielding metal, and the height of supporting point detect are so set as to bring a tine 62 of the shield 22 into contact with the shell 18 for pivot detents and prevent further downward rotation of the shield 22.

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