JPS5512214A - Turbine step - Google Patents

Turbine step

Info

Publication number
JPS5512214A
JPS5512214A JP8399678A JP8399678A JPS5512214A JP S5512214 A JPS5512214 A JP S5512214A JP 8399678 A JP8399678 A JP 8399678A JP 8399678 A JP8399678 A JP 8399678A JP S5512214 A JPS5512214 A JP S5512214A
Authority
JP
Japan
Prior art keywords
flow passage
outlet port
flow
static
inlet port
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP8399678A
Other languages
Japanese (ja)
Inventor
Tetsuo Sasada
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP8399678A priority Critical patent/JPS5512214A/en
Publication of JPS5512214A publication Critical patent/JPS5512214A/en
Pending legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE:To improve efficiency of turbine as well as to decrease unsteady loss in such a way that flow passage area is gradually decreased to make contracted vein flow passage, and uniformity of the flow is improved. CONSTITUTION:Flow passage bulkheads 1c, 1d of a diaphragm 1 are made into contracted vein bulkheads which are gradually protruded to the sides of the flow passage as they go along from a nozzle outlet port 2b to the downstream side, and a contracted passage by gradually decreasing the sectional area of the flow passage to conduct from a static blade outlet port 2b to a dynamic blade inlet port 2a. The flow passage area of the static cascade decrease from the static blade inlet port 2a to the outlet port 2b, further, decreases from the static blade outlet port 2a to the rear end of the diaphragm. Therefore, uniformity is increased for flow in the dynamic blade inlet port 3a, to obtain a turbine which has high efficiency and high stability.
JP8399678A 1978-07-12 1978-07-12 Turbine step Pending JPS5512214A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8399678A JPS5512214A (en) 1978-07-12 1978-07-12 Turbine step

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8399678A JPS5512214A (en) 1978-07-12 1978-07-12 Turbine step

Publications (1)

Publication Number Publication Date
JPS5512214A true JPS5512214A (en) 1980-01-28

Family

ID=13818135

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8399678A Pending JPS5512214A (en) 1978-07-12 1978-07-12 Turbine step

Country Status (1)

Country Link
JP (1) JPS5512214A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59147466U (en) * 1983-03-25 1984-10-02 株式会社セキネ Pig feeder that controls feeding amount
JPS6291131A (en) * 1986-08-22 1987-04-25 長谷川　恭子 Feeder for pig
JPS6398058U (en) * 1986-12-15 1988-06-24
JPS6417156U (en) * 1987-07-23 1989-01-27

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59147466U (en) * 1983-03-25 1984-10-02 株式会社セキネ Pig feeder that controls feeding amount
JPS6291131A (en) * 1986-08-22 1987-04-25 長谷川　恭子 Feeder for pig
JPS6398058U (en) * 1986-12-15 1988-06-24
JPS6417156U (en) * 1987-07-23 1989-01-27

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