GB647089A - Improvements in elastic fluid power plants - Google Patents

Improvements in elastic fluid power plants

Info

Publication number
GB647089A
GB647089A GB8067/48A GB806748A GB647089A GB 647089 A GB647089 A GB 647089A GB 8067/48 A GB8067/48 A GB 8067/48A GB 806748 A GB806748 A GB 806748A GB 647089 A GB647089 A GB 647089A
Authority
GB
United Kingdom
Prior art keywords
engine
compressor
power
air
fluid
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
GB8067/48A
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.)
Ljungstroms Angturbin AB
Original Assignee
Ljungstroms Angturbin AB
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 Ljungstroms Angturbin AB filed Critical Ljungstroms Angturbin AB
Publication of GB647089A publication Critical patent/GB647089A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/055Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor being of the positive-displacement type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/06Heating; Cooling; Heat insulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)

Abstract

647,089. Elastic-fluid power plants. AKTIEBOLAGET LJUNGSTROMS ANGTURBIN. March 18, 1948, No. 8067. Convention date, May 22, 1947. [Classes 110(ii) and 110(iii)] In a plant comprising one or more powergiving engines of the positive-displacement type and a separate compressor-driving engine, the conduits supplying both, or all engines with working-fluid are in open communication so that the decreasing speed of the power-giving engines allows an increase in supply of fluid to the compressor-driving engine to increase the torque developed by the power engine. In Fig. 1 the power-giving engine 14 and the compressor engine 12 are of the meshing screw types such as described in Specification 645,848. Fluid, usually air, is taken through an inlet 18, compressed into a chamber 28 and forced through cooling channels in the engine rotor from ducts 32, 52. The air thus heated passes through pipes 30, 36 to a combustion chamber 16, with a liquid or gaseous fuel supply 38, the combustion gases flowing through pipes 40, 42 to the screw engines 12, 14 respectively. Exhaust gases from ports 58, 60 may pass to atmosphere or to a regenerator. As the engine 14 slows down under heavy load on its shaft 50, the gas flow through the pipe 42 is decreased and that through the pipe 40 increased to increase the speed of the engine 12 and thus increase the flow of air through the compressor 10. The compressor may be of any type and the engine 12 need not be of the displacement type but may be a gas turbine. Fig. 4 shows another arrangement having a gas turbine 66 driving a compressor 10 and two combustion chambers 68, 70 with a common supply 74 of compressed air. Air is taken in at 18, compressed and delivered through a pipe 72 leading to the cooling system of the power engine 14. Combustion gases flow through pipes 80, 82 to the turbine 66 and engine 14. Exhaust ports 84, 58 are provided, leading to atmosphere or to regenerators. Part of the compressed air may byepass the cooling systems and pass directly to the combustion chamber as by way of a pipe 86 with valve 88. The plant may be used for traction purposes, oil-well drilling, power shovels and the like where a large starting torque in wanted. Compressed air may be mixed with working fluid on its way to a turbine or engine.
GB8067/48A 1947-05-22 1948-03-18 Improvements in elastic fluid power plants Expired GB647089A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE647089X 1947-05-22

Publications (1)

Publication Number Publication Date
GB647089A true GB647089A (en) 1950-12-06

Family

ID=20313941

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8067/48A Expired GB647089A (en) 1947-05-22 1948-03-18 Improvements in elastic fluid power plants

Country Status (1)

Country Link
GB (1) GB647089A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8109074B2 (en) 2002-03-14 2012-02-07 Newton Propuslion Technologies Gas turbine engine system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8109074B2 (en) 2002-03-14 2012-02-07 Newton Propuslion Technologies Gas turbine engine system

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