GB830362A - Improvements in transverse flow blowers - Google Patents

Improvements in transverse flow blowers

Info

Publication number
GB830362A
GB830362A GB14518/57A GB1451857A GB830362A GB 830362 A GB830362 A GB 830362A GB 14518/57 A GB14518/57 A GB 14518/57A GB 1451857 A GB1451857 A GB 1451857A GB 830362 A GB830362 A GB 830362A
Authority
GB
United Kingdom
Prior art keywords
rotor
chamber
entry
transverse
duct
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
GB14518/57A
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.)
Machinenfabrik Benninger A G
Original Assignee
Machinenfabrik Benninger A G
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 Machinenfabrik Benninger A G filed Critical Machinenfabrik Benninger A G
Publication of GB830362A publication Critical patent/GB830362A/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
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/04Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

830,362. Transverse-flow blowers. MASCHINENFABRIK BENNINGER A.G. May 7, 1957 [May 8, 1956; Nov. 27, 1956], No. 14518/57. Class 110 (1). In a transverse-flow blower in which a space is separated by a rotor into a suction chamber and a discharge chamber, means are provided for producing an abrupt increase in pressure on the rotor periphery near the point of entry of the rotor blades into the suction chamber. In the transverse-flow blower shown in Fig. 1, air is bled from the discharge chamber 13 through a duct 18 and impinges upon the rotor periphery at about the point of entry of the rotor blades 15 into the inlet chamber 12. This assists the entry of air into the rotor from the inlet chamber 12. A nozzle may be provided at the end of duct 18. The auxiliary jet of air may be supplied from a separate source, such as a compressor, instead of from the discharge chamber 13, and in this case the duct 18 may be replaced by a duct disposed parallel to the rotor axis at the point of entry of the rotor periphery into the inlet chamber 12 and discharging through nozzles or slots. A further arrangement is shown in Fig. 3, wherein the chambers 12 and 13 are separated by a transverse wall 25 inclined at not more than 30 degrees to the radial direction. The wall 25 produces an auxiliary flow from the chamber 13 in the direction of the arrows.
GB14518/57A 1956-05-08 1957-05-07 Improvements in transverse flow blowers Expired GB830362A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH830362X 1956-05-08

Publications (1)

Publication Number Publication Date
GB830362A true GB830362A (en) 1960-03-16

Family

ID=4540259

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14518/57A Expired GB830362A (en) 1956-05-08 1957-05-07 Improvements in transverse flow blowers

Country Status (1)

Country Link
GB (1) GB830362A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3181777A (en) * 1961-11-29 1965-05-04 Coester Robert Transverse-flow blower
US4836743A (en) * 1987-08-13 1989-06-06 Etat Francais Cross flow fan
US11396879B2 (en) * 2016-09-30 2022-07-26 Daikin Industries, Ltd. Cross-flow blower and indoor unit of air-conditioning device equipped with same

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3181777A (en) * 1961-11-29 1965-05-04 Coester Robert Transverse-flow blower
US4836743A (en) * 1987-08-13 1989-06-06 Etat Francais Cross flow fan
US11396879B2 (en) * 2016-09-30 2022-07-26 Daikin Industries, Ltd. Cross-flow blower and indoor unit of air-conditioning device equipped with same

Similar Documents

Publication Publication Date Title
US4711084A (en) Ejector assisted compressor bleed
GB1317992A (en) Gas turbine power plant
GB1037006A (en) Single stage centrifugal compressor refrigeration system
GB609926A (en) Improvements in or relating to internal-combustion turbines
GB923557A (en) Improvements in thrust diverting means for vtol and stol aircraft
GB1360428A (en) Vacuum cleaner including a fan assembly
GB803994A (en) Improvements in power units of the gas turbine type
GB830362A (en) Improvements in transverse flow blowers
GB897575A (en) Methods of and apparatus for preventing surging in single-stage or multi-stage radial flow compressors
GB736835A (en) Improvements in or relating to blading for axial flow turbo-engines
GB891278A (en) A gas turbine power unit
GB927207A (en) Improvements in gas turbine units
GB586573A (en) Improvements in or relating to internal combustion turbine plant
GB724652A (en) Aircraft fuel systems and booster pumps therefor
GB701557A (en) Improvements relating to gas turbine power plant
GB791917A (en) Improvements in and relating to gas turbine plants
GB754579A (en) Improvements in or relating to a turbine-driven impeller or fan
GB801758A (en) Improvements in or relating to centrifugal fans
GB941344A (en) Improvements in or relating to a centripetal turbine
GB877976A (en) Multistage axial flow compressors
GB850638A (en) Improvements in or relating to centrifugal fans
GB585330A (en) Improvements in or relating to turbines
GB814745A (en) An axial flow compressor
GB1223999A (en) Gas turbine engine
GB881816A (en) Improved gas turbine engine