GB757577A - Axial flow turbines and compressors - Google Patents

Axial flow turbines and compressors

Info

Publication number
GB757577A
GB757577A GB28477/54A GB2847754A GB757577A GB 757577 A GB757577 A GB 757577A GB 28477/54 A GB28477/54 A GB 28477/54A GB 2847754 A GB2847754 A GB 2847754A GB 757577 A GB757577 A GB 757577A
Authority
GB
United Kingdom
Prior art keywords
housing
carrier
blades
oct
compressors
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
GB28477/54A
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.)
Sulzer AG
Original Assignee
Sulzer AG
Sulzer Freres SA
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 Sulzer AG, Sulzer Freres SA filed Critical Sulzer AG
Publication of GB757577A publication Critical patent/GB757577A/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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line

Landscapes

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

Abstract

757,577. Elastic-Quid turbines and compressors. SULZER FRERES SOC. ANON. Oct. 4, 1954 [Oct. 9, 1953], No. 28477/54. Classes 110(1) and 110(3) In a multi-stage axial flow turbine or as shown, a compressor having adjustable stator blades 8 the latter are all carried by a cylindrical member 9 disposed between the rotor 1 and the housing 6 of the machine. The adjusting mechanism for the stator blades is disposed in the chamber 7 formed between the housing and the rotor. A flange 10 on the carrier 9 enters a groove 11 in the housing and abutting lugs 12, 13 on the housing and carrier are secured together by screws at 14, 15 with heads engaging longitudinal slots in the lugs 13. Longitudinal shafts 20 carry pinions 23 and bevel wheels 21 meshing with a ring gear 25 and bevel wheels 22 on the guide blades. The ring gear is driven by a bevel wheel 28 on a motor 27. Alternatively it may be hand operated. In place of shafts 20 thrust rods operating the blades through levers or gearing may be used. Other designs employ separate mechanisms for adjusting the earlier and later stages. The carrier may be fixed at the centre and make labyrinth seals at its ends with the housing.
GB28477/54A 1953-10-09 1954-10-04 Axial flow turbines and compressors Expired GB757577A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH757577X 1953-10-09

Publications (1)

Publication Number Publication Date
GB757577A true GB757577A (en) 1956-09-19

Family

ID=4534399

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28477/54A Expired GB757577A (en) 1953-10-09 1954-10-04 Axial flow turbines and compressors

Country Status (6)

Country Link
US (1) US2862687A (en)
BE (1) BE531926A (en)
CH (1) CH315187A (en)
GB (1) GB757577A (en)
LU (1) LU33042A1 (en)
NL (2) NL86773C (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10288087B2 (en) 2016-03-24 2019-05-14 United Technologies Corporation Off-axis electric actuation for variable vanes
US10294813B2 (en) 2016-03-24 2019-05-21 United Technologies Corporation Geared unison ring for variable vane actuation
US10301962B2 (en) * 2016-03-24 2019-05-28 United Technologies Corporation Harmonic drive for shaft driving multiple stages of vanes via gears
US10329946B2 (en) 2016-03-24 2019-06-25 United Technologies Corporation Sliding gear actuation for variable vanes
US10329947B2 (en) 2016-03-24 2019-06-25 United Technologies Corporation 35Geared unison ring for multi-stage variable vane actuation
US10415596B2 (en) 2016-03-24 2019-09-17 United Technologies Corporation Electric actuation for variable vanes
US10443430B2 (en) 2016-03-24 2019-10-15 United Technologies Corporation Variable vane actuation with rotating ring and sliding links
US10443431B2 (en) 2016-03-24 2019-10-15 United Technologies Corporation Idler gear connection for multi-stage variable vane actuation
US10458271B2 (en) 2016-03-24 2019-10-29 United Technologies Corporation Cable drive system for variable vane operation

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2976015A (en) * 1957-04-04 1961-03-21 Napier & Son Ltd Turbine stator blade rings
DE1113787B (en) * 1958-09-12 1961-09-14 Bbc Brown Boveri & Cie Axial compressor with rotatable guide vanes for dusty gas
DE1267131B (en) * 1964-08-22 1968-04-25 Ishikawajima Harima Kabushiki Reversible drive for ships
US3231239A (en) * 1964-11-30 1966-01-25 Ronald A Tyler Gas turbine
GB1098218A (en) * 1965-10-14 1968-01-10 Fiat Spa Arrangement for varying the inclination of the guide vanes of the inlet distributor of a gas turbine
CH556475A (en) * 1972-09-08 1974-11-29 Bbc Sulzer Turbomaschinen MULTI-STAGE AXIAL COMPRESSOR.
GB2078865B (en) * 1980-06-28 1983-06-08 Rolls Royce A variable stator vane operating mechanism for a gas turbine engine
JPS597708A (en) * 1982-07-07 1984-01-14 Hitachi Ltd Mounting angle variable device of stationary blade in axial flow machine
FR2708311B1 (en) * 1993-07-28 1995-09-01 Snecma Turbomachine stator with pivoting vanes and control ring.
DE102004004976A1 (en) * 2004-01-31 2005-08-18 Mtu Aero Engines Gmbh Device for adjusting vanes

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE237490C (en) *
US2300766A (en) * 1940-05-10 1942-11-03 Bbc Brown Boveri & Cie Multistage centrifugal compressor
US2371706A (en) * 1941-02-10 1945-03-20 Eugene Andre Paul Axial flow compressor
US2424839A (en) * 1943-09-21 1947-07-29 B F Sturtevant Co Spin vanes control device for cooling fans in aircraft engines
US2500070A (en) * 1945-06-15 1950-03-07 Westinghouse Electric Corp Multistage, axial flow, gas compressor
BE471940A (en) * 1946-03-20
GB621175A (en) * 1946-11-16 1949-04-05 Power Jets Res & Dev Ltd Improvements in or relating to stator blading of compressors and like machines
BE496713A (en) * 1949-07-01
GB701576A (en) * 1950-06-28 1953-12-30 Rolls Royce Improvements in or relating to compressors

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10288087B2 (en) 2016-03-24 2019-05-14 United Technologies Corporation Off-axis electric actuation for variable vanes
US10294813B2 (en) 2016-03-24 2019-05-21 United Technologies Corporation Geared unison ring for variable vane actuation
US10301962B2 (en) * 2016-03-24 2019-05-28 United Technologies Corporation Harmonic drive for shaft driving multiple stages of vanes via gears
US10329946B2 (en) 2016-03-24 2019-06-25 United Technologies Corporation Sliding gear actuation for variable vanes
US10329947B2 (en) 2016-03-24 2019-06-25 United Technologies Corporation 35Geared unison ring for multi-stage variable vane actuation
US10415596B2 (en) 2016-03-24 2019-09-17 United Technologies Corporation Electric actuation for variable vanes
US10443430B2 (en) 2016-03-24 2019-10-15 United Technologies Corporation Variable vane actuation with rotating ring and sliding links
US10443431B2 (en) 2016-03-24 2019-10-15 United Technologies Corporation Idler gear connection for multi-stage variable vane actuation
US10458271B2 (en) 2016-03-24 2019-10-29 United Technologies Corporation Cable drive system for variable vane operation
US11131323B2 (en) 2016-03-24 2021-09-28 Raytheon Technologies Corporation Harmonic drive for shaft driving multiple stages of vanes via gears

Also Published As

Publication number Publication date
NL182289B (en)
LU33042A1 (en)
CH315187A (en) 1956-07-31
US2862687A (en) 1958-12-02
NL86773C (en)
BE531926A (en)

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