GB1135766A - Improvements in or relating to steam turbines - Google Patents

Improvements in or relating to steam turbines

Info

Publication number
GB1135766A
GB1135766A GB1419065A GB1419065A GB1135766A GB 1135766 A GB1135766 A GB 1135766A GB 1419065 A GB1419065 A GB 1419065A GB 1419065 A GB1419065 A GB 1419065A GB 1135766 A GB1135766 A GB 1135766A
Authority
GB
United Kingdom
Prior art keywords
steam
wall
sleeve
casing
pressure
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.)
Expired
Application number
GB1419065A
Inventor
Adolf Frankel
Austin Anthony Skerrett
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.)
Associated Electrical Industries Ltd
Original Assignee
Associated Electrical Industries 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 Associated Electrical Industries Ltd filed Critical Associated Electrical Industries Ltd
Priority to GB1419065A priority Critical patent/GB1135766A/en
Publication of GB1135766A publication Critical patent/GB1135766A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26Double casings; Measures against temperature strain in casings
    • F01D25/265Vertically split casings; Clamping arrangements therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/06Fluid supply conduits to nozzles or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1,135,766. Steam turbines. ASSOCIATED ELECTRICAL INDUSTRIES Ltd. March 28, 1966 [April 2, 1965 (3)], Nos. 14190/65, 14194/65 and 14195/65. Heading F1T. A steam turbine cylinder comprises a number of successive expansion stages through which the driving steam flows, an outer casing protected internally from contact with hot steam from the driving steam flow up to an intermediate stage, and means situated after that stage for collecting steam from the driving steam flow and circulating the collected steam to the inside of the outer casing for cooling the casing, this means being arranged to collect the steam in such manner as to convert at least part of the velocity head of the collected driving steam into a pressure head as a result of impact, which pressure head prevents undesired leakage of hot steam to the casing via a leakage path from the driving steam flow at or close to the intermediate stage. The casing 5, Fig.2A, of an H.P. steam turbine cylinder is formed as a one-piece casting or forging having an integral inlet branch 47 with a wall 47A sufficiently thick to withstand the reduced working pressure obtaining immediately downstream of the second stage. Steam at the full inlet pressure and temperature passes through a much thinner inner wall 47B of the branch 47 to an annular nozzle box 34. The inner wall 47B is clamped at its outer end to the outer wall 47A and a sleeve 93 is secured to its inner end. To allow for thermal expansion, the outer end of the sleeve 93 slidably engages the inner wall 47B, and the inner ends of the inner wall and sleeve slidably engage packing rings 95, 97 carried by the nozzle box 34. Steam at the reduced pressure and temperature obtaining immediately downstream of the second-stage rotor blading 57 is collected in a slot 125 in each of a series of spokes 123, the impact converting some of the velocity head into pressure head to increase the pressure of the collected steam. The collected steam passes via radial passages 127 to anannular chamber 129 and thence around the nozzle box 34 to the annular space 99 between the outer wall 47A and the sleeve 93, whence it flows through holes 101 at about the mid-length of the sleeve into the annular space 103 between the sleeve and the inner wall 47B. From the inner end of the space 103, the steam flows via an annular chamber 105 and ducts (107, 109), Fig. 2B (not shown), to a point of lower pressure. The flow of steam through the annular spaces 99, 103 cools the outer wall 47A so that its inner end is held at about the temperature of the casing 5. The transition between this temperature and the inlet temperature to which the outer end of the outer wall 47A is subjected occurs over a cylindrical part of the outer wall of uniform cross-section so that no undue thermal stress occurs.
GB1419065A 1965-04-02 1965-04-02 Improvements in or relating to steam turbines Expired GB1135766A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1419065A GB1135766A (en) 1965-04-02 1965-04-02 Improvements in or relating to steam turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1419065A GB1135766A (en) 1965-04-02 1965-04-02 Improvements in or relating to steam turbines

Publications (1)

Publication Number Publication Date
GB1135766A true GB1135766A (en) 1968-12-04

Family

ID=10036660

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1419065A Expired GB1135766A (en) 1965-04-02 1965-04-02 Improvements in or relating to steam turbines

Country Status (1)

Country Link
GB (1) GB1135766A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013110765A1 (en) * 2012-01-26 2013-08-01 Energy Intelligence Lab Gmbh Multi-part, cooled turbine and generator housing
EP3014086A4 (en) * 2013-06-28 2017-03-01 Exxonmobil Upstream Research Company Systems and methods of utilizing axial flow expanders
US10036265B2 (en) 2013-06-28 2018-07-31 Mitsubishi Heavy Industries Compressor Corporation Axial flow expander
CN109339873A (en) * 2018-09-30 2019-02-15 东方电气集团东方汽轮机有限公司 Last stage vane of steam turbine protective device for high back pressure heat supply

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013110765A1 (en) * 2012-01-26 2013-08-01 Energy Intelligence Lab Gmbh Multi-part, cooled turbine and generator housing
EP3014086A4 (en) * 2013-06-28 2017-03-01 Exxonmobil Upstream Research Company Systems and methods of utilizing axial flow expanders
US10036265B2 (en) 2013-06-28 2018-07-31 Mitsubishi Heavy Industries Compressor Corporation Axial flow expander
US10385832B2 (en) 2013-06-28 2019-08-20 Exxonmobil Upstream Research Company Systems and methods of utilizing axial flow expanders
CN109339873A (en) * 2018-09-30 2019-02-15 东方电气集团东方汽轮机有限公司 Last stage vane of steam turbine protective device for high back pressure heat supply

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