JPS6419002U - - Google Patents

Info

Publication number
JPS6419002U
JPS6419002U JP11141187U JP11141187U JPS6419002U JP S6419002 U JPS6419002 U JP S6419002U JP 11141187 U JP11141187 U JP 11141187U JP 11141187 U JP11141187 U JP 11141187U JP S6419002 U JPS6419002 U JP S6419002U
Authority
JP
Japan
Prior art keywords
flow path
intermediate shell
heat exchanger
condenser
above heat
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
JP11141187U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP11141187U priority Critical patent/JPS6419002U/ja
Publication of JPS6419002U publication Critical patent/JPS6419002U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案の一実施例のタービン車室、中
間胴及び復水器の縦断面図、第2図は抽気ヒータ
の挿入位置x/bと圧力損失係数sの相関図である
。 1……タービン車室、2……中間胴、3……復
水器、4……熱交換器、5……冷却管巣、6a,
6b……排気(タービンの)。
FIG. 1 is a longitudinal sectional view of a turbine casing, an intermediate shell, and a condenser according to an embodiment of the present invention, and FIG. 2 is a correlation diagram between the insertion position x/b of the bleed heater and the pressure loss coefficient s. 1... Turbine casing, 2... Intermediate shell, 3... Condenser, 4... Heat exchanger, 5... Cooling pipe nest, 6a,
6b...exhaust (of the turbine).

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 軸直角排気形式の蒸気タービンの車室下部に設
けられその中間胴内に熱交換器等を備える復水器
において、中間胴の排気の流路の巾をb、同流路
の外側より上記熱交換器等の中心までの距離をx
とするとき、上記熱交換器等が0.33<x/b<
0.69の範囲に取付けられてなることを特徴と
する復水器。
In a condenser installed in the lower part of the casing of an axis-perpendicular exhaust type steam turbine and equipped with a heat exchanger, etc. in the intermediate shell, the width of the exhaust flow path in the intermediate shell is b, and the above heat is absorbed from the outside of the flow path. The distance to the center of the exchanger, etc. is x
When the above heat exchanger etc. is 0.33<x/b<
A condenser characterized in that it is installed in a range of 0.69.
JP11141187U 1987-07-22 1987-07-22 Pending JPS6419002U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11141187U JPS6419002U (en) 1987-07-22 1987-07-22

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11141187U JPS6419002U (en) 1987-07-22 1987-07-22

Publications (1)

Publication Number Publication Date
JPS6419002U true JPS6419002U (en) 1989-01-31

Family

ID=31349432

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11141187U Pending JPS6419002U (en) 1987-07-22 1987-07-22

Country Status (1)

Country Link
JP (1) JPS6419002U (en)

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