GB1073490A - Centrifugal compressor impellers - Google Patents

Centrifugal compressor impellers

Info

Publication number
GB1073490A
GB1073490A GB4760/66A GB476066A GB1073490A GB 1073490 A GB1073490 A GB 1073490A GB 4760/66 A GB4760/66 A GB 4760/66A GB 476066 A GB476066 A GB 476066A GB 1073490 A GB1073490 A GB 1073490A
Authority
GB
United Kingdom
Prior art keywords
hub
blades
shaft
tie bolt
webs
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
GB4760/66A
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 GB1073490A publication Critical patent/GB1073490A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • F04D29/285Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors the compressor wheel comprising a pair of rotatable bladed hub portions axially aligned and clamped together

Landscapes

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

Abstract

1,073,490. Centrifugal compressors; gas turbine engines. GENERAL MOTORS CORPORATION. Feb. 3, 1966 [Feb. 18, 1965], No. 4760/66. Headings F1C and F1G. [Also in Division F2] Each impeller blade 28 of a centrifugal compressor for a gas turbine engine has a pair of webs 32, each of which abuts a corresponding web on an adjacent blade to form a rear wall constituting one side of the flow passage between the two blades. The blades 28 are fixed to a hub 24 by dovetail roots and are welded at their trailing edges to an annular back plate 34 which is welded to the hub. To allow radial growth of the blades 28 without load transfer through the webs 32, no connection is made between the abutting edges of the webs. Inducer vanes 40 which, as shown, may be staggered in relation to the blades 28, are formed integrally with a hub 38. The hub 38 and a collar 42 are connected to the hub 24 by a pair of pins 44. The impeller is connected to a turbine shaft 46 by a hollow tie bolt 48. Two spring-pressed lock pins 54 on the hub 38 engage the serrated edge 52 of an annular flange 50 on the tie bolt 48. External threads on the lower end of the tie bolt 48 engage internal threads on the upper end of the shaft 46. The upper circumferential edge of the shaft 46 has serrations mating with serrations 47 on the lower circumferential edge of the collar 42. Accessories (61), Fig. 1 (not shown), are supported by a housing (58) suspended within the inlet (12) by struts (60) and are driven by a shaft (62) which is splined to an internal tubular portion 64 of the tie bolt 48.
GB4760/66A 1965-02-18 1966-02-03 Centrifugal compressor impellers Expired GB1073490A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US433670A US3305166A (en) 1965-02-18 1965-02-18 Centrifugal compressor

Publications (1)

Publication Number Publication Date
GB1073490A true GB1073490A (en) 1967-06-28

Family

ID=23721088

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4760/66A Expired GB1073490A (en) 1965-02-18 1966-02-03 Centrifugal compressor impellers

Country Status (2)

Country Link
US (1) US3305166A (en)
GB (1) GB1073490A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0133845A2 (en) * 1983-08-01 1985-03-06 CORAL S.p.A. Rotor for centrifugal compressors and fans
GB2344384A (en) * 1998-12-02 2000-06-07 Sunonwealth Electr Mach Ind Co Impeller for miniature fan

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO120916B (en) * 1968-11-25 1970-12-21 Kongsberg Vapenfab As
DE2735508C2 (en) * 1977-08-06 1985-03-28 Robert Bosch Gmbh, 7000 Stuttgart Washer device for cover panes of motor vehicle lights
US4502837A (en) * 1982-09-30 1985-03-05 General Electric Company Multi stage centrifugal impeller
DE3335616A1 (en) * 1983-09-30 1985-04-18 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Radial compressor impeller for turbomachines, especially gas turbine engines
US8814524B2 (en) * 2008-12-11 2014-08-26 Rolls-Royce Corporation Wheel formed from a bladed ring and disk
CN107250553A (en) * 2015-02-09 2017-10-13 阿特拉斯·科普柯空气动力股份有限公司 The method of impeller and this impeller of manufacture
DE102016108762A1 (en) * 2016-05-12 2017-11-16 Man Diesel & Turbo Se centrifugal compressors
DE102018204503A1 (en) * 2018-03-23 2019-09-26 Robert Bosch Gmbh liquid pump
CN111456966A (en) * 2020-05-22 2020-07-28 大连天孚环境科技有限公司 Detachable split type energy-saving compressor impeller

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA614865A (en) * 1961-02-21 E. Becker John Fluid couplings
US2317543A (en) * 1943-04-27 Suction cleaner
US958129A (en) * 1907-11-05 1910-05-17 Albert Huguenin Construction of rotating wheels for rotary fluid-compressors.
US2216747A (en) * 1935-09-06 1940-10-08 Gustav A Klimek Blade construction for fluid power transmitter
US2745597A (en) * 1953-01-13 1956-05-15 Harvey Whipple Inc Fan
US2889107A (en) * 1955-01-03 1959-06-02 Stalker Corp Fluid rotor construction
DE1275720B (en) * 1960-04-12 1968-08-22 Daimler Benz Ag Attachment of the impeller of a flow machine
FR1337094A (en) * 1962-10-24 1963-09-06 Cem Comp Electro Mec Fan training

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0133845A2 (en) * 1983-08-01 1985-03-06 CORAL S.p.A. Rotor for centrifugal compressors and fans
EP0133845A3 (en) * 1983-08-01 1985-07-10 Coral S.P.A. Rotor for centrifugal compressors and fans
GB2344384A (en) * 1998-12-02 2000-06-07 Sunonwealth Electr Mach Ind Co Impeller for miniature fan
GB2344384B (en) * 1998-12-02 2003-02-26 Sunonwealth Electr Mach Ind Co Fan wheel structures

Also Published As

Publication number Publication date
US3305166A (en) 1967-02-21

Similar Documents

Publication Publication Date Title
US3295825A (en) Multi-stage turbine rotor
GB1266585A (en)
GB1073490A (en) Centrifugal compressor impellers
ES364334A1 (en) Fluid compressors and turbofan engines employing same
GB1487324A (en) Gas turbine engines
GB1195012A (en) Rotor for Bladed Fluid Flow Machines.
GB1259963A (en) Improvements in fluid handling machines such as compressors, fans and turbines
GB1331209A (en) Bladed rotors for fluid flow machines
GB1314853A (en) Stator blading for turbomachinery
GB742477A (en) Improvements in or relating to bladed stator or rotor constructions for fluid machines such as axial-flow turbines or compressors
US3085400A (en) Cooling fluid impeller for elastic fluid turbines
US3028140A (en) Rotary fluid flow machine having rotor vanes constructed according to three dimensional calculations
GB1276100A (en) Bladed member for a fluid flow machine
GB1127269A (en) By-pass gas turbine engine having a compressor and fan exit guide vane assembly
GB1141280A (en) Bladed rotor for a fluid flow machine
GB1057234A (en) Turbine engine
GB693686A (en) Improvements relating to bladed rotary fluid-flow machines
US2700935A (en) Rocket fuel pump and the like
GB1509185A (en) Fluid driven turbo machines
GB1121194A (en) Bladed rotor for a fluid flow machine
GB1065278A (en) Improvements in or relating to compressors for gas turbine jet propulsion engines
GB1277416A (en) Improvements in or relating to vaned and bladed rotors
US2452185A (en) Fluid pump
GB477449A (en) Improvements in or relating to ventilating fans and the like
GB1173566A (en) Gas Turbine Improvements.