GB1057234A - Turbine engine - Google Patents

Turbine engine

Info

Publication number
GB1057234A
GB1057234A GB15354/64A GB1535464A GB1057234A GB 1057234 A GB1057234 A GB 1057234A GB 15354/64 A GB15354/64 A GB 15354/64A GB 1535464 A GB1535464 A GB 1535464A GB 1057234 A GB1057234 A GB 1057234A
Authority
GB
United Kingdom
Prior art keywords
turbine
compressor
assembly
nozzle assembly
ratio
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
GB15354/64A
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.)
Old Carco LLC
Original Assignee
Chrysler Corp
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 Chrysler Corp filed Critical Chrysler Corp
Publication of GB1057234A publication Critical patent/GB1057234A/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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49764—Method of mechanical manufacture with testing or indicating
    • Y10T29/49771—Quantitative measuring or gauging
    • Y10T29/49776—Pressure, force, or weight determining

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

1,057,234. Gas turbine plant; turbine blades. CHRYSLER CORPORATION. April 14, 1964 [July 25, 1963], No. 15354/64. Headings F1G and F1T. Prior to the assembly of a gas turbine engine, Fig. 1 (not shown), having a centrifugal compressor 24 driven by an axial flow turbine 26 and a separate power turbine 48, the actual flow areas of a series of turbines 26 and corresponding nozzle blade assemblies 42 are determined experimentally on test rigs, Figs. 10, 11 (not shown), under conditions corresponding to maximum engine speed. A turbine 26 and nozzle assembly 42 are then selectively matched so that the ratio of their actual flow areas is within 1% of the ideal flow area ratio as determined empirically, thus ensuring that the engine will be capable of developing its full rated power. In the embodiment the ideal ratio of the nozzle assembly 42 to the turbine 26 is 1 to 1À5. The turbine and nozzle assembly are also matched as a sub-assembly to the compressor 24 so as to ensure compressor operation within limits defined by the compressor's characteristic surge and choke lines.
GB15354/64A 1963-07-25 1964-04-14 Turbine engine Expired GB1057234A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US297538A US3252212A (en) 1963-07-25 1963-07-25 Method of selectively matching a turbine wheel and turbine nozzle assembly

Publications (1)

Publication Number Publication Date
GB1057234A true GB1057234A (en) 1967-02-01

Family

ID=23146742

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15354/64A Expired GB1057234A (en) 1963-07-25 1964-04-14 Turbine engine

Country Status (2)

Country Link
US (2) US3252212A (en)
GB (1) GB1057234A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010017434B4 (en) * 2009-06-29 2021-06-17 General Electric Company Device and method for testing a compressor

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1040864A (en) * 1964-07-27 1966-09-01 Warner Electric Brake & Clutch Improvements in or relating to drive transmission arrangements for electric motors
US3486460A (en) * 1968-09-25 1969-12-30 Black & Decker Mfg Co Gaging vane construction
US3704075A (en) * 1970-12-14 1972-11-28 Caterpillar Tractor Co Combined turbine nozzle and bearing frame
WO2011109514A1 (en) 2010-03-02 2011-09-09 Icr Turbine Engine Corporatin Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US20120324903A1 (en) * 2011-06-27 2012-12-27 Icr Turbine Engine Corporation High efficiency compact gas turbine engine
GB201200845D0 (en) * 2012-01-19 2012-02-29 Rolls Royce Plc Method of sealing cooling holes
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
TWI717955B (en) * 2019-12-27 2021-02-01 台睿精工股份有限公司 A method and structure for compensating tolerances in assembling modules

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2796658A (en) * 1953-11-02 1957-06-25 Sheffield Corp Mjethod of gauging and selecting cooperating parts
GB785419A (en) * 1955-03-22 1957-10-30 Sulzer Ag Radial flow compressors
US3034343A (en) * 1955-06-23 1962-05-15 Jr John E Lindberg Engine analyzer with self-synchronizing sweep
US3037348A (en) * 1956-09-28 1962-06-05 Daimler Benz Ag Gas turbine arrangement, particularly for motor vehicles
US3120053A (en) * 1958-06-02 1964-02-04 J C Thompson Tool & Die Inc Micrometer method
US3038331A (en) * 1958-06-10 1962-06-12 Curtiss Wright Corp Apparatus for measuring reaction engine thrust
US3077074A (en) * 1958-09-10 1963-02-12 Gen Motors Corp Regenerative gas turbine
US3077030A (en) * 1959-05-21 1963-02-12 Gen Motors Corp Method of forming locators
US3044262A (en) * 1960-05-09 1962-07-17 Chrysler Corp Control mechanism for adjustable gas turbine nozzle
US3142475A (en) * 1962-12-28 1964-07-28 Gen Electric Stator assembly

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010017434B4 (en) * 2009-06-29 2021-06-17 General Electric Company Device and method for testing a compressor

Also Published As

Publication number Publication date
US3319931A (en) 1967-05-16
US3252212A (en) 1966-05-24

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