GB672326A - Flow-equalizing means for two or more liquid streams - Google Patents

Flow-equalizing means for two or more liquid streams

Info

Publication number
GB672326A
GB672326A GB129350A GB129350A GB672326A GB 672326 A GB672326 A GB 672326A GB 129350 A GB129350 A GB 129350A GB 129350 A GB129350 A GB 129350A GB 672326 A GB672326 A GB 672326A
Authority
GB
United Kingdom
Prior art keywords
rotor
ducts
flow
accuracy
liquid
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
GB129350A
Other languages
English (en)
Inventor
John Neville Morris
Raymond Leslie Kent
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.)
SU Carburetter Co Ltd
Original Assignee
SU Carburetter Co Ltd
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
Priority to BE500665D priority Critical patent/BE500665A/xx
Application filed by SU Carburetter Co Ltd filed Critical SU Carburetter Co Ltd
Priority to GB129350A priority patent/GB672326A/en
Priority to FR1030190D priority patent/FR1030190A/fr
Publication of GB672326A publication Critical patent/GB672326A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Taps Or Cocks (AREA)
GB129350A 1950-01-18 1950-01-18 Flow-equalizing means for two or more liquid streams Expired GB672326A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
BE500665D BE500665A (enrdf_load_stackoverflow) 1950-01-18
GB129350A GB672326A (en) 1950-01-18 1950-01-18 Flow-equalizing means for two or more liquid streams
FR1030190D FR1030190A (fr) 1950-01-18 1950-12-27 Dispositif régulateur de l'écoulement des liquides

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB129350A GB672326A (en) 1950-01-18 1950-01-18 Flow-equalizing means for two or more liquid streams

Publications (1)

Publication Number Publication Date
GB672326A true GB672326A (en) 1952-05-21

Family

ID=9719455

Family Applications (1)

Application Number Title Priority Date Filing Date
GB129350A Expired GB672326A (en) 1950-01-18 1950-01-18 Flow-equalizing means for two or more liquid streams

Country Status (3)

Country Link
BE (1) BE500665A (enrdf_load_stackoverflow)
FR (1) FR1030190A (enrdf_load_stackoverflow)
GB (1) GB672326A (enrdf_load_stackoverflow)

Also Published As

Publication number Publication date
BE500665A (enrdf_load_stackoverflow)
FR1030190A (fr) 1953-06-10

Similar Documents

Publication Publication Date Title
GB745630A (en) Fluid flow control device for jet propulsion nozzles
GB672326A (en) Flow-equalizing means for two or more liquid streams
GB928027A (en) Improvements in and relating to turbine flow meters
FR2406079A1 (fr) Dispositif de regulation de turbine a gaz
US2752132A (en) Non-icing carburetor
GB767357A (en) Improvements in fuel distribution apparatus particularly for use with aviation powerplants of the continuous combustion type
GB1097350A (en) A flow rate divider for distributing aerated liquid fuel in an internal combustion engine
US2562936A (en) Impinging-jet fuel-spray bar
GB676512A (en) Improvements relating to exhaust gas turbine installations
GB853108A (en) Combustion system
GB751451A (en) Improvements in or relating to devices for mixing fluid streams
US2654384A (en) Flow divider device
GB1236545A (en) Rotary oil burner
GB777956A (en) Improvements in or relating to fluid valves
US2455308A (en) Control apparatus for internalcombustion engines
GB665603A (en) Improvements in or relating to distributors for fluids
GB810432A (en) Improvements in or relating to oscillating column combustion apparatus
GB759695A (en) Improvements in or relating to speed-sensitive control devices
GB620073A (en) Improvements in or relating to combustion systems for gas turbines with heat exchangers
GB742485A (en) Improvements in or relating to gas-turbine power plant installations
GB833418A (en) Improvements in or relating to liquid distributing systems
GB759583A (en) Improvements in or relating to speed-sensitive devices of the magnetic drag type
GB191009400A (en) Improvements in or relating to Elastic Fluid Turbines.
GB191315454A (en) An Improved Method of and Apparatus for Controlling the Flow of Fluids.
GB746084A (en) Improvements in or relating to aviation gas turbine power plants