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    • 1. 发明专利
    • Wind power generator and its control method
    • 风力发电机及其控制方法
    • JP2008261245A
    • 2008-10-30
    • JP2007103059
    • 2007-04-10
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • MATSUO ATSUSHIFUKAMI KOJINOGUCHI SHUNEIHAYASHIDA KAZUKITOFUN TEPPEIYATOMI YUJI
    • F03D7/04
    • F03D7/0204F05B2270/309F05B2270/321F05B2270/329F05B2270/402F05B2270/404Y02E10/723
    • PROBLEM TO BE SOLVED: To provide a yaw control technique of a wind power generator which reduces wind direction variation while suppressing increase of the number of yaw rotation even in the case where wind direction gradually changes in a long period of time.
      SOLUTION: The wind power generator of this invention is provided with a nacelle 3 for loading a wind mill rotor 7, a nacelle rotation mechanism 4, a wind direction anemometer 10 and a control device 21 for controlling the nacelle rotating mechanism 4. The controlling device 21 calculates the wind direction variation from the wind direction measured by the wind direction anemometer 10 and a direction of the wind mill rotor 7, and yaw rotation of the nacelle 3 is conducted by the nacelle rotating mechanism 4 if either one of the following two conditions is satisfied; 1: the absolute value of the wind direction variation is kept to be equal to or larger than a first threshold value just for a predetermined first duration time, 2: the absolute value of the wind direction variation is kept to be equal to or larger than a second threshold value which is larger than the first threshold value for a predetermined second duration time which is shorter than the first duration time.
      COPYRIGHT: (C)2009,JPO&INPIT
    • 要解决的问题:即使在风向在长时间段内逐渐变化的情况下,也可以提供减小风向变化同时抑制偏航旋转数增加的风力发电机的偏航控制技术。 解决方案:本发明的风力发电机设置有用于装载风车转子7,机舱旋转机构4,风向风速计10和用于控制机舱旋转机构4的控制装置21的机舱3。 控制装置21计算由风向风速计10测定的风向和风车转子7的风向的风向变化,并且,通过机舱旋转机构4进行机舱旋转机构4的偏转旋转, 满足以下两个条件; 1:风向变化的绝对值在预定的第一持续时间内保持为等于或大于第一阈值,2:风向变化的绝对值保持等于或大于 在比第一持续时间短的预定的第二持续时间内大于第一阈值的第二阈值。 版权所有(C)2009,JPO&INPIT
    • 3. 发明专利
    • AXIAL FLOW TURBINE BLADE CASCADE
    • JPH09242503A
    • 1997-09-16
    • JP4462096
    • 1996-03-01
    • MITSUBISHI HEAVY IND LTD
    • TSUTSUMI MASANORINOGUCHI SHUNEIOSAKA HIROMI
    • F01D5/02F01D5/14
    • PROBLEM TO BE SOLVED: To provide a novel blend round in which a cost and performance can be compatible with each other by setting specific dimensionless values R/O of a curvature radius R of the blend round with respect to a blade throat width O in sections between a rear edge of a blade and a throat, the throat and a branch point, and the branch point and a front edge of the blade. SOLUTION: A first section A from a rear edge 1a of a blade profile to a throat 4 is formed such that a dimensionless value R/O of a curvature radius R of a blend round with respect to a throat width O is maintained at about 0.4. A second section B from the throat 4 upstream to a branch point 7 at a distance substantially equal to a throat length is formed such that the value R/O is consecutively and linearly varied from about 0.4 to about 0.7. In a third section C from the branch point 7 to a front edge 3a of the blade profile, the entire blend round is formed such that the value R/O is maintained at about 0.7. Consequently, it is possible to enhance performance and enlarge the blend round so as to reduce a machining cost.
    • 4. 发明专利
    • AXIAL FLOW TURBINE EXHAUST CHAMBER
    • JPH10227202A
    • 1998-08-25
    • JP2771797
    • 1997-02-12
    • MITSUBISHI HEAVY IND LTD
    • HIRANO YUICHIRONOGUCHI SHUNEITAKENAGA HISAKUNI
    • F01D25/30
    • PROBLEM TO BE SOLVED: To reduce loss that turbine exhaust is produced and improve the performance of an exhaust chamber in an annular exhaust chamber arranged in an axial flow turbine outlet, by forming a fin extended from the peripheral side of an exhaust chamber inlet to the approximately center part of the exhaust chamber and a channel smoothly curved between the fin and an exhaust chamber inner wall. SOLUTION: In this exhaust chamber arranged in the outlet part of an axial flow turbine, a fin 4a extended from the peripheral side of an exhaust chamber inlet 1 is formed into a shape which is smoothly curved having an interval approximately in parallel with an exhaust chamber inner wall 3, and also an exhaust channel 7 formed by the fin 4a and the exhaust chamber inner wall 3 is formed as a smooth enlarged passage. This fin 4a is folded back according as it is directed to a downstream side and has a part in parallel with a turbine rotary shaft 5, and the end of the fin 4a is positioned in the approximately center of the inner cross section of the meridian plane of the exhaust chamber. Hereby, loss in an exhaust chamber inflow part can be suppressed to the minimum extent, and the end part of the fin 4a is positioned in the approximately center of the cross section of the meridian plane of the exhaust chamber, therefore a large scale slewing flow can be suppressed and the loss can be reduced.
    • 9. 发明专利
    • LOW PRESSURE WHEEL CHAMBER OF STEAM TURBINE
    • JPH0932505A
    • 1997-02-04
    • JP18407395
    • 1995-07-20
    • MITSUBISHI HEAVY IND LTD
    • TAKITA KATSUHIKOHAMAGAMI YOSHIYUKIWANI MASABUMINOGUCHI SHUNEI
    • F01D9/02F01D9/04F01D25/24F01D25/26
    • PROBLEM TO BE SOLVED: To restrain excessive deformation by thermal expansion in a low pressure wheel chamber of a steam turbine by integrally forming a high temperature side member composed of a pressure partition wall arranged between a blade ring to support steam inlet side stationary blades and a steam inlet pipe by welding or the like, and arranging a thermal expansion absorbing part between its high temperature side member and a single wheel chamber. SOLUTION: An outer wheel chamber part 11 and an inner wheel chamber part 3 are integrally formed, and a low temperature side single wheel chamber 110 having high rigidity is constituted, and a high temperature steam inlet pipe 1 and a blade ring 4 to support steam inlet side stationary blades 5 are provided, and a high temperature side member composed of a pressure partition wall 9 arranged between its blade ring 4 and the steam inlet pipe 1 is integrally formed by welding or the like. A thermal expansion absorbing part by interposing a flexible seal 15 between these integrally formed high temperature side member and single wheel chamber 110 is provided, and thermal expansion of the high temperature side member is absorbed, and its influence is prevented from being transmitted to the low temperature wheel chamber side. Therefore, deformation of the wheel chamber is reduced, and leakage of steam in a fitting part is reduced, and performance is improved, and thermal stress is reduced, and durability of the wheel chamber is improved.