GB499357A - Improvements relating to centrifugal blowers - Google Patents

Improvements relating to centrifugal blowers

Info

Publication number
GB499357A
GB499357A GB19774/38A GB1977438A GB499357A GB 499357 A GB499357 A GB 499357A GB 19774/38 A GB19774/38 A GB 19774/38A GB 1977438 A GB1977438 A GB 1977438A GB 499357 A GB499357 A GB 499357A
Authority
GB
United Kingdom
Prior art keywords
elements
low
pressure
vanes
section
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
GB19774/38A
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
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 Daimler Benz AG filed Critical Daimler Benz AG
Priority to GB19774/38A priority Critical patent/GB499357A/en
Publication of GB499357A publication Critical patent/GB499357A/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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4213Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/16Combinations of two or more pumps ; Producing two or more separate gas flows
    • F04D25/166Combinations of two or more pumps ; Producing two or more separate gas flows using fans
    • 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
    • F04D29/286Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors multi-stage rotors

Abstract

499,357. Centrifugal blowers. TUGWOOD, R. J. (Daimler-Benz Akt.-Ges.) July 4, 1938, No. 19774. [Class 110 (i)] In order to supply low-pressure air for cooling a Diesel engine and high-pressure air for scavenging or charging, the centrifugal blower has in a common rotor both vane elements 8, Fig. 1, for the former supply and tubular elements 9 for the latter. The elements 8 have thickened edges at their inlet ends, and the elements 9 have a flat cross-section and are curved and splayed conically towards their outlet ends where they project beyond the vanes 8. The vanes 8 lead to a low-pressure passage 5 and the tubes 9 to a high-pressure passage 13<1>. Grooves 11 are provided in the surface of the flared inlet 10. The high- and low-pressure spaces 13, 5<1> may be sealed by extending the elements between the walls 14, 15, Fig. 3, and providing a labyrinth seal 12 consisting of coacting grooves of triangular cross-section.
GB19774/38A 1938-07-04 1938-07-04 Improvements relating to centrifugal blowers Expired GB499357A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB19774/38A GB499357A (en) 1938-07-04 1938-07-04 Improvements relating to centrifugal blowers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB19774/38A GB499357A (en) 1938-07-04 1938-07-04 Improvements relating to centrifugal blowers

Publications (1)

Publication Number Publication Date
GB499357A true GB499357A (en) 1939-01-23

Family

ID=10134996

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19774/38A Expired GB499357A (en) 1938-07-04 1938-07-04 Improvements relating to centrifugal blowers

Country Status (1)

Country Link
GB (1) GB499357A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2827261A (en) * 1953-08-21 1958-03-18 Garrett Corp Fluid propulsion apparatus
US2997959A (en) * 1958-01-24 1961-08-29 Westinghouse Electric Corp Pump
US3005311A (en) * 1957-08-08 1961-10-24 Frederick W Ross Gas turbine engine with combustion inside compressor
US3143103A (en) * 1963-08-23 1964-08-04 Caterpillar Tractor Co Multi-stage supercharger with separate outlet for cooling air
DE1270887B (en) * 1964-03-26 1968-06-20 Caterpillar Tractor Co Exhaust gas turbocharger system for internal combustion engines
US3946565A (en) * 1974-08-29 1976-03-30 Wallace Murray Corporation Intercooler fan and compressor construction
US5228829A (en) * 1986-08-20 1993-07-20 A. Ahlstrom Corporation Method and apparatus for dividing flow of high-consistency fiber suspension
WO2006117073A1 (en) * 2005-04-29 2006-11-09 Daimlerchrysler Ag Exhaust-gas turbocharger for an internal combustion engine
CN101852218A (en) * 2010-04-16 2010-10-06 江门市汉宇电器有限公司 Drainage pump cover
CN105351205A (en) * 2015-12-11 2016-02-24 中国北方发动机研究所(天津) Novel centrifugal type water pump

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2827261A (en) * 1953-08-21 1958-03-18 Garrett Corp Fluid propulsion apparatus
US3005311A (en) * 1957-08-08 1961-10-24 Frederick W Ross Gas turbine engine with combustion inside compressor
US2997959A (en) * 1958-01-24 1961-08-29 Westinghouse Electric Corp Pump
US3143103A (en) * 1963-08-23 1964-08-04 Caterpillar Tractor Co Multi-stage supercharger with separate outlet for cooling air
DE1270887B (en) * 1964-03-26 1968-06-20 Caterpillar Tractor Co Exhaust gas turbocharger system for internal combustion engines
US3946565A (en) * 1974-08-29 1976-03-30 Wallace Murray Corporation Intercooler fan and compressor construction
US5228829A (en) * 1986-08-20 1993-07-20 A. Ahlstrom Corporation Method and apparatus for dividing flow of high-consistency fiber suspension
WO2006117073A1 (en) * 2005-04-29 2006-11-09 Daimlerchrysler Ag Exhaust-gas turbocharger for an internal combustion engine
US7870731B2 (en) 2005-04-29 2011-01-18 Daimler Ag Exhaust gas turbocharger for an internal combustion engine
CN101852218A (en) * 2010-04-16 2010-10-06 江门市汉宇电器有限公司 Drainage pump cover
CN105351205A (en) * 2015-12-11 2016-02-24 中国北方发动机研究所(天津) Novel centrifugal type water pump

Similar Documents

Publication Publication Date Title
GB497188A (en) An internal combustion engine for use at high altitudes charged by turbo-blowers
GB1401486A (en) Centrifugal compressors especially for supercharging engines
GB499357A (en) Improvements relating to centrifugal blowers
GB742477A (en) Improvements in or relating to bladed stator or rotor constructions for fluid machines such as axial-flow turbines or compressors
GB1147991A (en) Improvements in or relating to intermeshing-screw type rotary engines
GB291007A (en) Improvements in rotary fans
GB613892A (en) Method of producing centrifugal blowers for supercharging internal combustion engines
GB478498A (en) Improvements in or relating to multistage axial compressors
GB564336A (en) Multistage axial flow compressor
GB504385A (en) Improvements in or relating to rotary blowers or compressors
GB461887A (en) Improvements relating to internal combustion turbines
GB152689A (en) Improvements in and relating to turbo-compressors and turbo-blowers
GB526730A (en) Improvements in or relating to rotary engines
GB463390A (en) Improvements in and relating to elastic fluid turbines
GB679467A (en) Improvements in gas turbines
GB791917A (en) Improvements in and relating to gas turbine plants
GB429959A (en) Improvements relating to screw fans
GB529799A (en) Improvements in power plants comprising an electric generator driven by a gas turbine
GB625625A (en) Improvements in or relating to rotary power conversion machines of the rotary abutment type
GB827798A (en) Improvements in or relating to pressure exchangers
GB811434A (en) Improvements in or relating to regenerative heat exchangers
GB485488A (en) Improvements in rotary supercharging blowers
GB139717A (en) Improvements in and connected with air blowers
GB178109A (en) Rotor for centrifugal pumps and blowers
GB1053509A (en)