GB119379A - Improvements in and relating to Centrifugal Compressors. - Google Patents

Improvements in and relating to Centrifugal Compressors.

Info

Publication number
GB119379A
GB119379A GB133418A GB133418A GB119379A GB 119379 A GB119379 A GB 119379A GB 133418 A GB133418 A GB 133418A GB 133418 A GB133418 A GB 133418A GB 119379 A GB119379 A GB 119379A
Authority
GB
United Kingdom
Prior art keywords
compressors
weights
float
driven
means responsive
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
GB133418A
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.)
British Thomson Houston Co Ltd
Original Assignee
British Thomson Houston 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
Application filed by British Thomson Houston Co Ltd filed Critical British Thomson Houston Co Ltd
Priority to GB133418A priority Critical patent/GB119379A/en
Publication of GB119379A publication Critical patent/GB119379A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0269—Surge control by changing flow path between different stages or between a plurality of compressors; load distribution between compressors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)

Abstract

119,379. British Thomson - Houston Co., (General Electric Co.). Jan. 23, 1918. Regulating or controlling. - A number of compressors operating in parallel and each driven by its own motor, which is regulated by means responsive to the load on the corresponding compressor, are provided with means responsive to an operating condition common to all the compressors for simultaneously modifying the regulating means for each comopressor. The Figure shows two compressors 5, 6, driven by turbines 7, 8, the inlet valves 30 of which are each controlled by a counterbalanced lever 17 connected to a float 20 in the inlet conduit 11 to the compressor. A speed governor control is combined with this constant volume governor, which may be adjusted for different volumes by variations of the position of the weights 18. In the apparatus shown, the position of the weights 18 is determined by the pressure in the header 9 from which both compressors draw gas, acting through the counterbalanced float 34 and the shaft 14.
GB133418A 1918-01-23 1918-01-23 Improvements in and relating to Centrifugal Compressors. Expired GB119379A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB133418A GB119379A (en) 1918-01-23 1918-01-23 Improvements in and relating to Centrifugal Compressors.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB133418A GB119379A (en) 1918-01-23 1918-01-23 Improvements in and relating to Centrifugal Compressors.

Publications (1)

Publication Number Publication Date
GB119379A true GB119379A (en) 1918-10-03

Family

ID=32340538

Family Applications (1)

Application Number Title Priority Date Filing Date
GB133418A Expired GB119379A (en) 1918-01-23 1918-01-23 Improvements in and relating to Centrifugal Compressors.

Country Status (1)

Country Link
GB (1) GB119379A (en)

Similar Documents

Publication Publication Date Title
US2306277A (en) Internal combustion engine and supercharging apparatus
US2613029A (en) Axial flow compressor regulation
US2318905A (en) Gas turbine plant
GB1320530A (en) Gas turbine engine
US2339150A (en) Blower control system
US2693081A (en) Apparatus for controlling gas turbine engines during transient operation
US2460778A (en) Torque regulating device for compressors
GB531997A (en) Improvements relating to constant pressure gas turbines
US2409837A (en) Centrifugal type compressor
GB1082705A (en) Gas turbine engine control system
US2485431A (en) Engine control apparatus
US2689606A (en) Fuel feeding system for gas turbine engines
US2496407A (en) Internal-combustion turbine plant
US2454038A (en) Control system for aircraft turbosuperchargers
US2651911A (en) Power plant having a common manual control for the fuel valves of the compressor and power turbines
US3050941A (en) Fuel control apparatus for a combustion engine
US2566550A (en) Control for centrifugal compressor systems
GB119379A (en) Improvements in and relating to Centrifugal Compressors.
US3557552A (en) Gas turbine engine installation fuel systems
US2409533A (en) Apparatus for controlling superchargers
US3777478A (en) Method of and apparatus for control of helicopter gas turbine engine during auto-rotation
US2544235A (en) Combustion gas turbine plant
US2544852A (en) Exhaust gas turbine with variable nozzle area for maintaining constant pressure dropthrough the turbine
US2378441A (en) Aircraft supercharger control
US1017509A (en) Governing mechanism for centrifugal apparatus.