会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明公开
    • TURBINE ROTOR BLADE
    • TURBINENROTORSCHAUFEL
    • EP2230385A1
    • 2010-09-22
    • EP09701788.3
    • 2009-01-08
    • Mitsubishi Heavy Industries, Ltd.
    • TOCHITANI, NaotoDANNO, ShoheiYAMASHITA, Shoki
    • F01D5/30
    • F01D5/3007F01D5/225Y10T29/49321
    • It is possible to easily and rapidly slot a blade root of a final (last) turbine rotor blade into a blade groove on a turbine disc even when the plan-view shape of a shroud of the turbine rotor blade is complex. A turbine rotor blade (1) that is provided with a blade root (3) that is slotted into a blade groove formed on a circumferential portion of the turbine disc to hold the whole blade, a blade portion (4) that is exposed to high-temperature gas, a platform (5) that supports this blade portion (4), a shank (6) that connects the blade root (3) and the platform (5), and a shroud (7) that extends along the circumferential direction from the end of the blade portion (4) has a cut-out portion (8) cut out to a predetermined depth, either at the leading-edge or the trailing-edge of the blade root (3), along the lengthwise direction thereof from the end of the blade root (3) to an intermediate part of the shank (6).
    • 即使当涡轮转子叶片的护罩的平面视图形状复杂时,也可以容易且快速地将最终(最后)涡轮转子叶片的叶片根部切换到涡轮盘上的叶片凹槽中。 一种涡轮转子叶片(1),其具有叶片根部(3),所述叶片根部(3)被开槽成形成在所述涡轮盘的圆周部分上以保持整个叶片的叶片槽;暴露于高的叶片部分(4) - 温度气体,支撑该叶片部分(4)的平台(5),连接叶片根部(3)和平台(5)的柄部(6)以及沿圆周方向延伸的护罩(7) 从叶片部分(4)的端部沿切割部分(8)的长度方向切割到刀片根部(3)的前缘或后缘处的预定深度的切口部分(8) 从叶片根部(3)的端部到柄部(6)的中间部分。
    • 3. 发明公开
    • METHOD OF CONTROLLING TURBINE EQUIPMENT AND TURBINE EQUIPMENT
    • 控制涡轮机设备和涡轮机设备的方法
    • EP2334911A2
    • 2011-06-22
    • EP09723967.7
    • 2009-03-27
    • Mitsubishi Heavy Industries, Ltd.Pebble Bed Modular Reactor (Pty) Limited
    • ONO, HitoiSONODA, TakashiTOCHITANI, NaotoKATO, MakotoUMAYA, MasahideFUJII, Fuminori
    • F01K13/02
    • F02C1/05F01K13/02F01K25/00F02C1/10F02C9/18F05D2260/85F05D2270/30G21D1/02G21D3/08Y02E30/40
    • To provide a method of controlling a turbine equipment and a turbine equipment capable of carrying out a starting operation of controlling a load applied to a speed reducing portion while complying with a restriction imposed on an apparatus provided at a turbine equipment. The invention is characterized in including a speed accelerating step (S1) of increasing a revolution number by driving to rotate a compressing portion and a turbine portion by a motor by way of a speed reducing portion, a load detecting step (S2) of detecting a load applied to the speed reducing portion by a load detecting portion, and a bypass flow rate controlling step (S3) of increasing a flow rate of a working fluid bypassed from a delivery side to a suction side of the compressing portion when an absolute value of the detected load is equal to or smaller than an absolute value of a predetermined value and reducing the flow rate of the bypassed working fluid when equal to or larger than the absolute value of the predetermined value.
    • 提供一种控制涡轮机设备和涡轮机设备的方法,该涡轮机设备和涡轮机设备能够执行控制施加到减速部分的负载的启动操作,同时符合对设置在涡轮机设备处的设备施加的限制。 本发明的特征在于包括:速度加速步骤(S1),其通过由电动机经由减速部分驱动旋转压缩部分和涡轮部分来增加转数;负载检测步骤(S2),其检测 通过载荷检测部施加于减速部的载荷;以及旁路流量控制步骤(S3),当从压缩部的输送侧向吸入侧绕过的工作流体的流量增大时 检测到的负载等于或小于预定值的绝对值,并且当等于或大于预定值的绝对值时,减小旁路工作流体的流量。
    • 5. 发明公开
    • TURBINE
    • 涡轮
    • EP2385222A1
    • 2011-11-09
    • EP09839233.5
    • 2009-08-10
    • Mitsubishi Heavy Industries, Ltd.
    • OTANI, YukihiroTOCHITANI, Naoto
    • F01D25/28F01D9/00F01D25/00F01D25/26
    • F01D25/246F01D25/243F01D25/265F05D2230/642F05D2250/232
    • To provide a turbine that is capable of deforming (tilting) of a support portion (more specifically, a circular-truncated cone portion). A turbine (1) that is provided with a vertically divided casing (3) that is divided into two portions in a longitudinal direction and a support portion (9) that supports a stator-blade ring (8) disposed in the casing (3), wherein the support portion (9) is provided with a flange portion (9a) that is secured between a joining surface of one portion of the casing (3) and a joining surface of the other portion of the casing (3), being sandwiched therebetween, and a circular-truncated cone portion (9b) that connects the flange portion (9a) and a stator-blade holding ring (8), and wherein a thick plate portion (9c) having a greater plate thickness than the plate thickness of the flange portion (9a) and the stator-blade holding ring (8) is provided between the flange portion (9a) located at a lower-half portion and the stator-blade holding ring (8).
    • 提供能够使支撑部(更具体地,圆截锥体部)变形(倾斜)的涡轮机。 一种涡轮机(1),其具有沿长度方向分成两部分的垂直分割的壳体(3)和支撑设置在壳体(3)中的定子叶片环(8)的支撑部分(9) ,其中所述支撑部分(9)设置有凸缘部分(9a),所述凸缘部分(9a)固定在所述壳体(3)的一部分的接合表面和所述壳体(3)的另一部分的接合表面之间, 以及连接凸缘部分(9a)和定子 - 叶片保持环(8)的圆形截头圆锥部分(9b),并且其中厚板部分(9c)的板厚度大于 凸缘部分(9a)和定子 - 叶片保持环(8)设置在位于下半部分的凸缘部分(9a)和定子 - 叶片保持环(8)之间。