GB133400A - - Google Patents

Info

Publication number
GB133400A
GB133400A GB133400DA GB133400A GB 133400 A GB133400 A GB 133400A GB 133400D A GB133400D A GB 133400DA GB 133400 A GB133400 A GB 133400A
Authority
GB
United Kingdom
Prior art keywords
lever
valve
pulsation
link
float
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
Publication date
Publication of GB133400A publication Critical patent/GB133400A/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
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0207Surge control by bleeding, bypassing or recycling fluids

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanically-Actuated Valves (AREA)

Abstract

133,400. British Thomson - Houston Co., (General Electric Co.). Sept. 9, 1918. Regulating and controlling.- A pulsation-preventing valve mechanism is combined with a constant-volume regulator of known type. The pivoted beam 13 and sliding weight 17 of the constant-volume regulator are connected to the usual float 18 in the inlet 7 of the compressor 6, which is driven by the turbine 5. Regulation of the turbine speed by the constantvolume regulator is obtained through a lever 12 actuating the pilot valve 11 of a fluid-actuated motor 10, which controls a valve in the pressure-fluid inlet 9 of the turbine. The pulsation-preventing gear comprises a lever pivoted on a fixed arm 16 and connected at one end by a link 47 to a pressureresponsive device connected by a pipe 46 to the compressor delivery 8. A shaft 14, around which the lever 15 can turn, is rigidly connected to the beam 13. The lever 15 is connected to the bypass valve 32 by a link 43, a lever 42, a shaft 41, a sliding plate 36 containing a cam-groove, a rod 34, and an arm 33. The pivot point B of the beam 13 in the lever 15 is lowered either by an increase in pressure in the delivery 8 raising the link 47, or by a decrease in the volume lowering the float 18. When this happens, the link 43 is lowered and consequently the cam-plate 36 is moved. The cam-slot in the plate 36 has two straight portions and a curved portion. When the pin of the rod 34 is in a straight portion, the by-pass valve is not affected; but when the pin is in the curved portion, a movement of the plate 36 operates the by-pass valve in the correct direction to prevent pulsations. Stops 49, 50 limit the movements of the bell-crank lever 23 and correspond to maximum and minimum speeds at which it is desired to run the machine. If, for instance, the float rises to an extent corresponding with the maximum desired speed, the bellcrank lever is moved against the stop 49 and prevents further operation of the steam-regulating mechanism 9 by the volume governor. The speed governor 30 then takes control. Even in this state of affairs, the pulsation-preventing mechanism remains under the control of the force on the float 18 and the discharge pressure, because the pivot point B can move about the pivot of the lever 15 independently of the fixing or otherwise of the bell-crank lever 23. The pulsation-preventing mechanism may thus be brought into operation under all conditions.
GB133400D Expired GB133400A (en)

Publications (1)

Publication Number Publication Date
GB133400A true GB133400A (en) 1900-01-01

Family

ID=1726818

Family Applications (1)

Application Number Title Priority Date Filing Date
GB133400D Expired GB133400A (en)

Country Status (1)

Country Link
GB (1) GB133400A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2730789A1 (en) * 1977-07-07 1979-01-18 Linde Ag Controlling pumping limit of variable turbocompressor - by varying return flow to inlet as function of intake flow and output setting

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2730789A1 (en) * 1977-07-07 1979-01-18 Linde Ag Controlling pumping limit of variable turbocompressor - by varying return flow to inlet as function of intake flow and output setting

Similar Documents

Publication Publication Date Title
US1655683A (en) Regulating mechanism fob turbine-driven centrifugal compressors
JPH0659877B2 (en) Pitch controller for variable pitch propeller
US2125949A (en) Regulator
US2979891A (en) Thrust control apparatus for liquid propellant rocket engines
US2205625A (en) Aircraft propulsion
GB133400A (en)
US3187505A (en) Gas turbine fuel regulator
US3516250A (en) Fuel control system for turbo-shaft engines
US1093116A (en) Governing mechanism for turbines.
US1280811A (en) Pulsation-preventing apparatus for centrifugal compressors.
US3744925A (en) Apparatus for regulating a turbo-compressor
US2533231A (en) Speed-responsive governor
US3348375A (en) Gas turbine engine fuel control
US2949735A (en) Control apparatus for a propulsion engine
US2926681A (en) Speed governing systems for turbines
US3019602A (en) Speed regulator for prime movers
US3073329A (en) Isochronous governor
US2159863A (en) Engine governor
US2763986A (en) Emergency control system, regulator and computer mechanism
US1591937A (en) Prime-mover-control system
US6955113B2 (en) Electro-hydraulic actuator with mechanical servo position feedback
US902001A (en) Automatic regulating device for fluid-pressure apparatus.
US1280812A (en) Pulsation-preventing mechanism.
RU2230922C2 (en) System to control fuel delivery into gas-turbine engine
US1281217A (en) Pulsation-preventing mechanism for centrifugal compressors.