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    • 1. 发明专利
    • Thermocouple reference junction compensating device
    • 热电偶参考连接补偿装置
    • JP2009192372A
    • 2009-08-27
    • JP2008033314
    • 2008-02-14
    • Mitsubishi Heavy Ind LtdOkazaki Mfg Co Ltd三菱重工業株式会社株式会社岡崎製作所
    • YOSHITANI HIROSHISHIDA TOMONORITERADA MASABUMIMIHARA TAKASHISEGAWA EIICHI
    • G01K7/12
    • PROBLEM TO BE SOLVED: To provide a thermocouple reference junction compensating device, capable of securing convenience, reducing the cost and improving the temperature compensation accuracy for the reference junction of a thermocouple.
      SOLUTION: This device is provided with the reference junction 10 of the thermocouple, a temperature-measuring resistor 20 for measuring the, temperature based on the change of a resistance value, and a metal block 30 made of a solid metal having an approximately cylindrical shape. The metal block 30 is provided with three or more storage holes 32, extending from the upper surface of the metal block 30 to the inside of the metal block 30, capable of holding the reference junction 10 and the temperature-measuring resistor 20 inside the metal block 30, by inserting the reference junction 10 and the temperature-measuring resistor 20 into each bottom part 32a, respectively, and the temperature measured by the temperature-measuring resistor 20, inserted into the storage hole 32, is used as the temperature of the reference junction 10 of the thermocouple.
      COPYRIGHT: (C)2009,JPO&INPIT
    • 要解决的问题:为了提供热电偶参考点补偿装置,能够确保方便性,降低成本并提高热电偶的参考接合点的温度补偿精度。 解决方案:该装置具有热电偶的参考连接点10,用于根据电阻值的变化来测量温度的温度测量电阻器20以及由固态金属制成的金属块30 大致圆柱形。 金属块30设置有从金属块30的上表面延伸到金属块30的内部的三个以上的存储孔32,能够将基准接合点10和温度测量电阻20保持在金属内 块30,通过将参考接头10和温度测量电阻器20分别插入到每个底部32a中,并且将由插入到存储孔32中的温度测量电阻器20测量的温度用作温度 热电偶的参考接头10。 版权所有(C)2009,JPO&INPIT
    • 2. 发明专利
    • THERMAL UNBALANCE REGULATING SYSTEM FOR TURBINE
    • JP2000356106A
    • 2000-12-26
    • JP16848399
    • 1999-06-15
    • MITSUBISHI HEAVY IND LTD
    • MIHARA TAKASHIYAMAMOTO YOSHITO
    • F01D25/12F01D19/00
    • PROBLEM TO BE SOLVED: To prevent the occurrence of unevenness of temperature distribution and to reduce the generation of vibration of a rotor due to the unbalance by a method wherein water or steam is injected against a spot of the rotor where a thermal unbalance is apt to occur. SOLUTION: In this system, a support member 80 is passed through a cavity 78 at the outlet part of the final state moving blade 74 of a steam turbine and a water injection nozzle 1 is inserted into the support member. Water is injected in a pulse-form manner to prevent the occurrence of unevenness of the temperature of a rotor 73. A number of revolutions sensor 9 detects the discrimination bar 90a of a wheel 90, a vibration sensor 10 detects vibration displacement of a wheel 91, and the detecting results are sent to vibration measuring device 8. At the measuring device 8, a vibration pulse signal is outputted in a range where vibration displacement exceeds a threshold. A quantity of water regulating device 5 is driven through a thermal unbalance vibration change confirming device 7, and water from a water feed source 5 is injected in a pulse-form manner.
    • 4. 发明专利
    • TEMPERATURE SENSOR
    • JPH03239930A
    • 1991-10-25
    • JP3703290
    • 1990-02-17
    • NAT SPACE DEV AGENCYMITSUBISHI HEAVY IND LTDOKAZAKI MFG CO LTD
    • YAMAWAKI KOICHIOMURO SHOJIROOZAKI AKIOKAWASAKI TETSUOKOUSETSU YUUJIONO YOSHIOITO KOICHIKYOHARA SHIROTANAKA SHIYOUJIMIHARA TAKASHI
    • G01K1/08G01K7/02G01K7/18
    • PURPOSE:To allow the decrease of the oscillation of a winding frame and to prevent the failure of a cable connected to the temp. measuring platinum strand at the base end of the winding frame by supporting the front end of the winding frame with the front end of a holding cylinder via a supporting member or directly supporting the front end of the winding frame. CONSTITUTION:The temp. measuring platinum strand 2 is wound on the outer peripheral surface of the winding frame 1 and a positioning hole 4 is hollowed in the central axial direction of bottom at the base end of the winding frame 1. Connecting holes 5, 5 to connect the hole 4 and the winding end are bored. The end face of the MI cable 9 which houses platinum alloy core wires 8, 8 interposed with an inorg. insulating material 7, such as MgO, in an armor pipe 6 consisting of a platinum alloy is subjected to end face sealing 10 and the core wires 8, 8 are exposed from the seal 10. The core wires 8, 8 are inserted into the communicating holes 5, 5 and the cable 9 is fitted into the positioning hole 4. Both ends of the strand 2 and the front ends of the core wires 8, 8 are connected. The strand 2 is then coated with a coating material and enmal is packed into the cavity between the core wires 8 and 8 to closely seal the cavity. The increase in the spacing is obviated by a thermal elongation difference even if the sensor heats up to a high temp. at the time of use. The oscillation of the winding frame 1 is thus limited.
    • 8. 发明专利
    • HIGH DAMPING THRUST BEARING
    • JP2002070853A
    • 2002-03-08
    • JP2000258401
    • 2000-08-29
    • MITSUBISHI HEAVY IND LTD
    • MIHARA TAKASHIYAMASHITA KATSUYASHINOHARA TANEHIRO
    • F16C17/03F16C27/00
    • PROBLEM TO BE SOLVED: To provide a thrust bearing which can support a rotating shaft stably and can decay axial vibration of the rotating shaft, even under the condition that a thrust load is not acting on the rotating shaft or the thrust load became small. SOLUTION: This high damping thrust bearings comprises: a thrust pad having a pad face faced each other across the predetermined clearance with a flange face of a thrust collar extending radially outwardly against the rotating shaft; a thrust pad supporting means for supporting the thrust pad having a thrust load transfer face at the position away axially from the thrust collar; a thrust bearing case which has an interior bore accommodating the thrust pad and the thrust pad supporting means and in which the interior bore has a thrust load carrier plane arranged to face each other with the thrust load transfer face. In the thrust bearing wherein a primary oil film is formed by the oil supplied to a predetermined clearance, a supporting plate further arranged between the thrust load transfer face and the thrust load carrier plane wherein a secondary oil film is formed between the thrust load transfer face and/or the thrust load carrier plane and the supporting plate.