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    • 32. 发明专利
    • Power generation system
    • 发电系统
    • JP2010133284A
    • 2010-06-17
    • JP2008307830
    • 2008-12-02
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • TSUTSUMI MASANORIKANAHOSHI TAKAYUKIFURUKAWA TOYOAKI
    • F01K23/14F01D15/12F01K23/10F01K23/16F01N5/00F01N5/02
    • Y02E20/16Y02T10/16
    • PROBLEM TO BE SOLVED: To provide a power generation system suppressing occurrence of misalignment in an SSS (Synchro Self Shifting) clutch switching whether or not rotation is to be transmitted.
      SOLUTION: This power generation system includes: a power turbine taking out output from exhaust gas supplied from a motor; a first output shaft transmitting rotation output from the power turbine; a first speed reduction gear connected to the first output shaft; a steam turbine taking out output from exhaust heat supplied from the motor; a second output shaft transmitting rotation output from the steam turbine; a second speed reduction gear connected to the second output shaft; a generator connected to the steam turbine through the second speed reduction gear; and the SSS clutch connected to the power turbine through the first speed reduction gear and connected to the steam turbine through the second speed reduction gear.
      COPYRIGHT: (C)2010,JPO&INPIT
    • 要解决的问题:为了提供抑制SSS(同步自动换档)离合器切换中的不对准的发电系统,是否传送旋转。 解决方案:该发电系统包括:动力涡轮机,从电动机提供的排气中输出; 从动力涡轮机传递旋转输出的第一输出轴; 连接到第一输出轴的第一减速齿轮; 蒸汽涡轮机从电动机提供的排气热量输出; 第二输出轴,其传递来自所述蒸汽轮机的旋转输出; 连接到第二输出轴的第二减速齿轮; 通过第二减速装置连接到蒸汽轮机的发电机; 并且SSS离合器通过第一减速齿轮连接到动力涡轮机,并通过第二减速齿轮连接到蒸汽轮机。 版权所有(C)2010,JPO&INPIT
    • 36. 发明专利
    • FUEL TANK FOR ARTIFICIAL SATELLITE
    • JPH1035595A
    • 1998-02-10
    • JP19320996
    • 1996-07-23
    • MITSUBISHI HEAVY IND LTD
    • FURUKAWA TOYOAKIHARA TADAHIKO
    • B64G1/40
    • PROBLEM TO BE SOLVED: To prevent the collision of a bladder and a wall of a fuel tank securely and reduce collision force by arranging a stuffing having expansion and shrinkage property between the wall of the fuel tank and the bladder in a the fuel tank for artificial satellite having the bladder made of an elastic body in which fuel is stored in the inside thereof. SOLUTION: In a fuel tank for artificial satellite constituted by a wall 1 of the fuel tank and a bladder 2 made of an elastic body in which fuel is stored, a stuffing 3 which is wrapped by a stuffing net 4 and has expansion and shrinkage property is arranged between the wall 1 of the fuel tank and the bladder 2. Since this stuffing 3 must have strong expansion and shrinkage property and be light in weight, down of bird is used. Consequently, it is possible to prevent the collision of the bladder 2 against the wall 1 of the fuel tank, reduce collision force by the stuffing 3 having expansion and shrinkage property, and prevent the damage of the bladder 2. Moreover, an elastic film having many small through holes may be provided in such a manner that it wraps the stuffing 3 and the stuffing net 4 on the outside of the stuffing net 4.
    • 40. 发明专利
    • GAS BEARING STRUCTURE
    • JPH08334124A
    • 1996-12-17
    • JP16309395
    • 1995-06-07
    • MITSUBISHI HEAVY IND LTD
    • MATSUMOTO IWAOFURUKAWA TOYOAKI
    • F16C32/06
    • PURPOSE: To achieve an electrical purpose without using an electrical control part so as to improve explosion proof properties much better, by interposing compressed air in a bearing void, and actuating upon a part for receiving the load of a counter, magnetic action formed by a permanent magnet, preferably magnetic repulsive force. CONSTITUTION: A thin layered ring bearing void 4 is formed between a counter member 1 (rotary shaft) and a bearing main body 3 (bearing metal). Multiple air supply holes 5 are opened and arranged at equal intervals in the peripheral direction from the outer circumferential surface side of the bearing main body 3 toward the inner circumferential side of a magnet body 20. These air supply holes 5 are provided adjacently to a compressed air supply source 7 through a check valve 6 on the outer circumferential side of the bearing main body 3. The counter member 1 is formed in such a manner that a cylindrical permanent magnet 1B having the same magnetism as the ring magnet body 20 is included in a rotary shaft 1A so that magnetic repulsive force consisting of the repulsive magnetic fields of two magnets 1B, 20 by using the rotary shaft 1A formed of a magnetic material is generated in the bearing void 4 opposed to the ring magnetic body 20.