Mitsubishi Heavy Industries Limited

Mitsubishi Hitachi Power Systems, Ltd.

Hitachi, Ltd.

Mitsubishi Power, Ltd.

Tokyo University of Science Foundation

Shunsuke Mizumi

Koji Ishibashi

Takeshi Kudo

Juichi Kodera

Soichiro Tabata

Chongfei Duan

Susumu Nakano

Kenji Yashirodai

Satoshi Kumagai

Ryuichiro Iwano

Masaki Matsuda

Jie Huang

Yasuhiro Sasao

Naoto Omura

Hideki Ono

Hideaki Sugishita

Kazuyuki Matsumoto

Yoshihiro Kuwamura

Koichi Murakami

Noriyo Nishijima

Shinji Oikawa

Going Won Lee

Masaru Sekihara

Goingwon Lee

Shigeo Ookura

Masahiro Motosuke

Masato Kurita

Daiki Shiraishi

Jose Carlos Kuroki Ramirez

Satoshi Miyake

Ketsu Ko

Masayuki Kayahara

Yoshiaki Onda

Koji Ogata

Tatsuhito Hattori

Kazuya Sakakibara

The sensor of a fluid sensor system includes an outer peripheral sensor unit including three or more sensor pairs to surround and sandwich the heating element. The computing device of the system includes a first identification unit identifies a sensor pair in which an output difference between an output value corresponding to a temperature detected by one temperature sensor of the sensor pair and an output value corresponding to a temperature detected by the other temperature sensor of the sensor pair is largest, a second identification unit identifies other sensor pairs adjacent to the identified sensor pair in the circumferential direction, and a flow direction estimation unit estimates the flow direction of the fluid on the basis of the output difference in the sensor pair having the largest output difference and output differences in the other sensor pairs adjacent to the sensor pair in the circumferential direction.

Fluid sensor system, computing device, and flow direction estimation method

In a method for estimating flange displacement amount, effective three-dimensional coordinate data at a lower first position on a surface continuous with a lower flange surface of a first supported portion and at an upper first position coincident with the lower first position in the horizontal direction on a surface continuous with an upper flange surface are determined. The effective three-dimensional coordinate data at the respective positions are changed such that the effective three-dimensional coordinate data at the lower first position and the effective three-dimensional coordinate data at the upper first position are coincident with each other. In accordance with a difference between a position in a vertical direction indicated by the effective three-dimensional coordinate data at an upper target position on the upper flange surface after a coordinate change and a position in the vertical direction indicated by the effective three-dimensional coordinate data at a lower target position on the lower flange surface after a coordinate change, displacement amounts of the upper target position and the lower target position in the vertical direction when a state changes from an open state to a fastened state are obtained.

Method for estimating flange displacement amount in rotary machine, program for executing the method, and device for performing the method

This stationary turbine blade comprises: a stationary blade main body extending in the radial direction intersecting the flow direction of steam; a hydrophilic region which is formed on the surface of the stationary blade main body and which has a higher hydrophilicity than the other parts and has the radial dimension gradually increasing toward the downstream side in the flow direction; and a collecting portion which is provided on the downstream side of the hydrophilic region and which collects a liquid film flowing along the hydrophilic region.

Stationary turbine blade and steam turbine

In an assembly method for a turbine, measured shape data is acquired by measuring a shape for each of a plurality of casing components in a state in which the plurality of casing components are not fastened to each other. self-weighted state shape data, which is shape data when self-weight is applied, is created for each of the plurality of casing components. A reference shape model is corrected based on a difference between the measured shape data of a target measurement part and the self-weighted state shape data of the target measurement part. By using the corrected shape model, fastened state shape data, which is shape data in a state in which the plurality of casing components are fastened to each other, is estimated for each of the plurality of casing components.

Assembly method for turbine, assembly support program for turbine, and assembly support device for turbine

This fin tip position measurement method comprises: a jig installation step for installing a jig having a flat measurement surface expanded in a circumferential direction and an axial direction to a tip of at least one among a plurality of seal fins that protrude in a radial direction with respect to an axial line, extend in the circumferential direction, and are arranged in a direction in which the axial line extends; a first measurement step for measuring a distance from the axial line to the measurement surface by scanning the measurement surface with a laser beam; and a first calculation step for calculating a distance from the axial line to the tip of the seal fin by adding a radial dimension of the jig to the distance to the measurement surface.

Fin tip position measurement method, fin tip position measurement system, and jig for measuring fin tip position

A turbine stator vane includes: a stator vane body extending in a radial direction intersecting a flow direction of steam; a recovery portion that is defined on a surface of the stator vane body, and configured to recover a liquid film flowing along the surface of the stator vane body; and a center region, which is defined on the surface of the stator vane body and includes grooves extending from an upstream side toward the recovery portion in the flow direction. Intervals between adjacent grooves decrease from the upstream side toward the recovery portion.

Turbine stator vane and steam turbine

A turbine includes a rotor including a rotation shaft that rotates around an axis and a blade row formed on an outer surface of the rotation shaft; a casing, which covers the rotor, has a casing inner surface being expanded radially outward approaching a downstream side of the casing in a direction of the axis; and an inner member body formed to line the casing inner surface of the casing such that an extraction port is formed between an upstream side end of the inner member body and the casing inner surface. A discharge port is formed between a downstream side end of the inner peripheral member body and the casing inner peripheral surface. The extraction port and the discharge port are formed in an annular shape centered on the axis. A flow path cross-sectional area of the discharge port is smaller than that of the extraction port.

Turbine

A steam turbine includes a rotary shaft, a blade provided on an outer peripheral surface of the rotary shaft, a casing covering the rotary shaft and the blade from an outer peripheral side, a vane provided on an inner peripheral surface of the casing, and a seal device including a seal ring provided between the outer peripheral surface and the vane and a position adjusting portion configured to adjust a position of the seal ring in a radial direction. A seal clearance adjusting method includes a measurement step of measuring a length of the seal ring in the radial direction from a predetermined reference position as a reference length, a preparation step of preparing an unused seal ring, and an adjustment step of adjusting a length of the unused seal ring from the reference position to be the reference length by the position adjusting portion.

Steam turbine seal clearance adjusting method

This turbine stator vane extends in the radial direction which intersects the flow direction of steam, and includes a pressure surface facing the upstream side in the flow direction, and a suction surface facing the downstream side in the flow direction. A plurality of grooves are formed in at least the pressure surface, the grooves extending outward in the radial direction toward the downstream side. At the periphery of the grooves in the pressure surface, formed is a hydrophilic uneven region having greater hydrophilic properties than the pressure surface. The downstream-side ends of the plurality of grooves are connected to slits for capturing a liquified component of the steam.

Turbine stator vane, turbine stator vane assembly, and steam turbine

A method and system for measuring a turbine shape is provided in which an appropriate measurement accuracy can be achieved that is sufficient to prevent a failure to recognize features of shape of a measurement object, with extension of a measurement time suppressed. In a turbine including casings, recesses and protrusions on flange surfaces of the casings are measured at measurement intervals M set on the basis of the entire length L of flange portions in an axial direction, the number of bolts N joining the flange portions, and intervals between the bolts in the axial direction of the flange portions.

Method and system for measuring turbine shape

A turbine stator blade () includes a pressure side (P) extending in a radial direction intersecting a flow direction of steam, and facing upstream in the flow direction. A slit () extending in the radial direction and capturing a liquefied component of the steam is formed on a downstream side of the pressure side (P). A hydrophilic uneven region () having a liquid film capacity greater than that of the pressure side (P) by being recessed in a depth direction intersecting the pressure side (P) is formed in a further upstream position than the slit (). The hydrophilic uneven region () has a depth in the depth direction increasing and a flow resistance decreasing toward downstream and toward the slit ().

Turbine stator blade and steam turbine

A turbine stator blade () includes a pressure side (P) extending in a radial direction intersecting a flowing direction of steam and facing upstream in the flowing direction. A slit () capturing droplets generated by liquefaction of the steam is formed on a downstream side of the pressure side (P). A fine uneven region (), which guides the droplets attached to the pressure side (P) in the radial direction such that the droplets are moved toward the slit () and from upstream toward downstream, is formed in a further upstream position than the slit (). The fine uneven region () has a flow resistance to the droplets gradually increasing from inward to outward in the radial direction.

A stationary blade includes a main unit having a hollow blade structure formed from a metal plate by plastic forming. The stationary blade includes a blade tail section. In a blade tail upper portion, the metal plate has a concave-shaped recess and a rib formed on an inner surface side thereof, and the metal plate further has slits formed by slitting on a blade pressure side thereof, so that droplets affixed on a blade surface can be guided into an inside of the hollow blade when the blade tail section is joined to the hollow blade main unit. The recess in the metal plate is covered so as to be lidded by a suction-side protrusion of a suction-side metal plate from a blade suction side to thereby form a hollow blade tail section. The metal plates are welded together to the main unit.

Steam turbine

In assembling a turbine including: a casing consisting of an upper half part and a lower half part fastened together by bolts; a stationary body accommodated in the casing and supported by the lower half part; and a rotary body supported by a plurality of bearings so as to be situated on the inner side of the stationary body, there are executed: a procedure of reading a finite element model of the three-dimensional configuration of the turbine; a reading procedure of reading actual measurement information on the three-dimensional configuration of the upper half part and the lower half part of the casing in the open state; a model correction procedure of reflecting actual measurement information of an evaluated portion that is a specific part of the casing in the finite element model and generating a correction model obtained through correction of the finite element model; a deformation amount estimation procedure of estimating the movement amount of the evaluated portion generated when the upper half part and the lower half part of the casing are fastened together by the bolts through simulation using the correction model; and an output procedure of outputting an estimated value of the movement amount to an output device.

Growing community of inventors

Yokohama, Japan

Shunsuke Mizumi