GB844019A - Stator vane assemblies for axial-flow compressors or turbines - Google Patents

Stator vane assemblies for axial-flow compressors or turbines

Info

Publication number
GB844019A
GB844019A GB30651/58A GB3065158A GB844019A GB 844019 A GB844019 A GB 844019A GB 30651/58 A GB30651/58 A GB 30651/58A GB 3065158 A GB3065158 A GB 3065158A GB 844019 A GB844019 A GB 844019A
Authority
GB
United Kingdom
Prior art keywords
stator vane
turbines
shroud ring
axial
vane assemblies
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
GB30651/58A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB844019A publication Critical patent/GB844019A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T24/00—Buckles, buttons, clasps, etc.
    • Y10T24/14—Bale and package ties, hose clamps
    • Y10T24/1412—Bale and package ties, hose clamps with tighteners
    • Y10T24/1424—Lever
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T24/00—Buckles, buttons, clasps, etc.
    • Y10T24/14—Bale and package ties, hose clamps
    • Y10T24/1412—Bale and package ties, hose clamps with tighteners
    • Y10T24/1439—Radial screw

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

844,019. Elastic fluid turbines. GENERAL MOTORS CORPORATION. Sept. 25, 1958 [Oct. 3, 1957], No. 30651/58. Class 110 (3). A stator vane assembly for a turbine or compressor comprises an outer shroud ring, an inner shroud ring 19, and stator vanes 18 connecting the rings, the assembly being made up of segments which are secured and drawn together by coupling devices carried at the ends of the inner shroud ring portions 20, 21. Each coupling device comprises a U-shaped clasp 30 having arms 31 pivoted to a bracket 27 carried on the portion 21, a screw 36 mounted on the other portion 20 being rotatable to force the crossbar 32 of the clasp over the inclined ramp face 34 of a bracket 33 secured to the same portion 20.
GB30651/58A 1957-10-03 1958-09-25 Stator vane assemblies for axial-flow compressors or turbines Expired GB844019A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US688084A US3069135A (en) 1957-10-03 1957-10-03 Vane ring assembly

Publications (1)

Publication Number Publication Date
GB844019A true GB844019A (en) 1960-08-10

Family

ID=24763045

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30651/58A Expired GB844019A (en) 1957-10-03 1958-09-25 Stator vane assemblies for axial-flow compressors or turbines

Country Status (2)

Country Link
US (1) US3069135A (en)
GB (1) GB844019A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3142475A (en) * 1962-12-28 1964-07-28 Gen Electric Stator assembly
US3644057A (en) * 1970-09-21 1972-02-22 Gen Motors Corp Locking device
JP3631271B2 (en) * 1993-11-19 2005-03-23 ユナイテッド テクノロジーズ コーポレイション Inner shroud integrated stator vane structure
US5860788A (en) * 1996-06-14 1999-01-19 Shell Electric Mfg. (Holdings) Co. Ltd. Low drag fan assembly

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US286755A (en) * 1883-10-16 Cover for vessels
GB191026713A (en) * 1910-11-17 1911-05-25 Alexander Dewar Horne Improvements in Steam Traps.
FR730955A (en) * 1931-02-17 1932-08-26 Allmanna Sevenska Elek Ska Akt Method and device for the manufacture of impellers for radial turbines
US2390801A (en) * 1944-07-25 1945-12-11 Pollak Mfg Company Joint for exhaust manifold systems
GB727608A (en) * 1951-10-31 1955-04-06 Gen Motors Corp Improvements in blade assemblies for gas turbines and the like
US2772069A (en) * 1951-10-31 1956-11-27 Gen Motors Corp Segmented stator ring assembly
US2803866A (en) * 1953-06-29 1957-08-27 Tinnerman Products Inc Band clamp with axial manipulating means

Also Published As

Publication number Publication date
US3069135A (en) 1962-12-18

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