GB707480A - Improvements in and relating to gas turbine plants - Google Patents

Improvements in and relating to gas turbine plants

Info

Publication number
GB707480A
GB707480A GB29222/51A GB2922251A GB707480A GB 707480 A GB707480 A GB 707480A GB 29222/51 A GB29222/51 A GB 29222/51A GB 2922251 A GB2922251 A GB 2922251A GB 707480 A GB707480 A GB 707480A
Authority
GB
United Kingdom
Prior art keywords
compressor
turbine
air
valves
opened
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
GB29222/51A
Inventor
Otto Zadnik
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.)
CA Parsons and Co Ltd
Original Assignee
CA Parsons and 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 CA Parsons and Co Ltd filed Critical CA Parsons and Co Ltd
Publication of GB707480A publication Critical patent/GB707480A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01KSTEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K23/00Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
    • F01K23/02Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
    • F01K23/06Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
    • F01K23/10Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

707,480. Gas turbine plant. PARSONS & CO., Ltd., C. A. Dec. 13, 1951, No. 29222/51. Class 110(3) In a gas turbine plant comprising a compressor driven by a turbine which exhausts to an independent power turbine the exhaust gases of which pass through a combustion chamber and a h.eat exchanger. heating the air between the compressor. and the compressor turbine, to a steam generator, controllable quantities of hot air are tapped from the exhaust of the power turbine or any point in the circuit between the compressor and the power turbine exhaust and mixed with the air entering the compressor, and further controllable quantities of air are tapped from a stage of the compressor or between the compressor turbine and power turbine or both and led direct to the combustion chamber. The plant shown comprises a two stage compressor 3, 4 which discharges through a heat exchanger 11 to a compressor turbine 6 which exhausts through a chamber 7 to a power turbine 8a. The exhaust gases from the power turbine pass through a duct 8b to a combustion chamber 9 which heats the air between the compressor 3, 4 and the compressor-turbine 6. The gases leaving the heat exchanger 11 pass through a steam generator 13 to the exhaust duct 15. A duct 14 is provided to enable the exhaust gases to by-pass the steam generator. Valves 16, 17 in the ducts 14. 15 are controlled by a pressure regulator 18 so that the valve 16 is opened and valve 17 closed, when a predetermined steam pressure is reached. If it is desired to increase the steam supply from the steam generator 13. the valves 37, 38 are opened and hot air passed to the intake of the compressor 3, 4. This results in an increase in the temperatures of the exhaust gases of the turbine 8a and so increases the output of the steam generator. If a further increase is desired, the valves 43 and 45 may be opened. The air passing through these valves passes through injectors which increase the flow through the duct 36. The inlet throttle 2 may also be used to increase the flow through the duct 36. A still further increase in output of the steam generator 13 may be obtained by opening valves 33, 35 so passing air direct to the combustion chamber 9 in which more fuel may then be burnt. Hot air may also be led to filters 40 through which air enters the compartment 41 containing the plant. The steam from the generator 13 may be used to operate auxiliaries of the plant through pipes 21 or added to the air leaving the compressor through a pipe 48. Steam is also used to operate a turbine 22 which drives an electric generator 23 which may be used as a motor. The electric generator 23 is connected to the turbine 22 and a blower 24 by clutches 25. In starting, the generator 23 is energized from the battery 27 to drive the blower 24. Air then passes through the compressor 34, heat exchanger 11, turbines 6, 8a to the combustion chamber 9 and steam generator 13. The valves 33 and 35 may be opened to increase the air flow to the combustion chamber 9. When the compressor is up to speed, the throttle 2 may be opened and the blower shut down. In a modification, the compressor is run up to speed by an electric motor fed with current by an auxiliary Diesel set. After starting, the valves 37. 43 and 45 may be opened to control the speed of the compressor.
GB29222/51A 1951-12-13 1951-12-13 Improvements in and relating to gas turbine plants Expired GB707480A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB310606X 1951-12-13

Publications (1)

Publication Number Publication Date
GB707480A true GB707480A (en) 1954-04-21

Family

ID=10317363

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29222/51A Expired GB707480A (en) 1951-12-13 1951-12-13 Improvements in and relating to gas turbine plants

Country Status (3)

Country Link
CH (1) CH310606A (en)
FR (1) FR1078355A (en)
GB (1) GB707480A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1038344B (en) * 1956-09-11 1958-09-04 Licentia Gmbh Process for operating a gas turbine system with regenerative heat exchanger and waste heat recovery

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1042300B (en) * 1956-07-27 1958-10-30 Sulzer Ag Gas turbine plant with waste heat boiler

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1038344B (en) * 1956-09-11 1958-09-04 Licentia Gmbh Process for operating a gas turbine system with regenerative heat exchanger and waste heat recovery

Also Published As

Publication number Publication date
CH310606A (en) 1955-10-31
FR1078355A (en) 1954-11-17

Similar Documents

Publication Publication Date Title
US3703807A (en) Combined gas-steam turbine power plant
GB636364A (en) Improvements in gas turbine plant for the associated production of heat and mechanical energy including adjusting means therefor
US2469679A (en) Gas turbine
GB592243A (en) Improvements in or relating to steam-air heat-power plants
GB1151200A (en) Reserve Power Gas Turbine-Generators and Methods of Operating same in "Spinning Reserve"
GB537483A (en) Improvements in or relating to internal combustion engines operating with supercharging
GB1225759A (en)
US2898731A (en) Power producing equipment incorporating gas turbine plant
GB707480A (en) Improvements in and relating to gas turbine plants
US3444686A (en) Gas turbine smog control for internal combustion engine
GB604114A (en) Improvements in regenerative gas turbine plants
US2748566A (en) Compound gas-turbine engine with lowpressure compressor and turbine bypass
GB1486741A (en) Power plant
GB492831A (en) Improvements in gas turbine plants of the continuous combustion type
GB1441039A (en) Internal combustion engines installations
GB723419A (en) Improvements relating to gas turbine plant providing a continuous supply of hot compressed air
GB695339A (en) Improvements relating to plants for producing a supply of compressed air
GB709147A (en) Method of operating gas-turbine plants
GB587449A (en) Improvements in motive power installations having a generator for hot gas under pressure
GB592389A (en) Improvements in or relating to thermal power plants
GB1103948A (en) Improvements in and relating to gas turbine plant
SU794234A1 (en) Power plant
GB578628A (en) Gas-or air-turbine plant
GB488538A (en) Means for regulating and starting thermal power plants
GB608776A (en) Improvements in or relating to gas turbine plants