GB812273A - Improvements in and relating to turbines, compressors, blowers and fans - Google Patents

Improvements in and relating to turbines, compressors, blowers and fans

Info

Publication number
GB812273A
GB812273A GB13555/55A GB1355555A GB812273A GB 812273 A GB812273 A GB 812273A GB 13555/55 A GB13555/55 A GB 13555/55A GB 1355555 A GB1355555 A GB 1355555A GB 812273 A GB812273 A GB 812273A
Authority
GB
United Kingdom
Prior art keywords
blowers
compressors
turbines
fans
relating
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
GB13555/55A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB812273A publication Critical patent/GB812273A/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
    • F04D21/00Pump involving supersonic speed of pumped fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/145Means for influencing boundary layers or secondary circulations
    • 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
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • 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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • F04D29/682Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid extraction

Abstract

812,273. Boundary layer control. HAUSAMMANN, W. May 10, 1955 [May 10, 1954], No. 13555/55. Class 4. [Also in Group XXVI] A turbine or compressor comprising at least one duct formed between the hub surface and partition walls 152 of the rotor and an outer surface, and a sill 155 on the hub or outer surface which faces upstream in the case of a compressor and downstream in the case of a turbine and is arranged at an angle to the plane of the rotor, has the boundary layer removed from the sill by a suction pump 171 through the slot 156 and ducts 159, 161.
GB13555/55A 1954-05-10 1955-05-10 Improvements in and relating to turbines, compressors, blowers and fans Expired GB812273A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH812273X 1954-05-10

Publications (1)

Publication Number Publication Date
GB812273A true GB812273A (en) 1959-04-22

Family

ID=4538608

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13555/55A Expired GB812273A (en) 1954-05-10 1955-05-10 Improvements in and relating to turbines, compressors, blowers and fans

Country Status (1)

Country Link
GB (1) GB812273A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3418494A1 (en) * 2017-06-23 2018-12-26 Rolls-Royce plc Secondary flow control

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3418494A1 (en) * 2017-06-23 2018-12-26 Rolls-Royce plc Secondary flow control
US10760427B2 (en) 2017-06-23 2020-09-01 Rolls-Royce Plc Secondary flow control

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