GB867762A - Installation comprising a plurality of gas-generators, more particularly free-pistongenerators, producing hot gas under pressure - Google Patents

Installation comprising a plurality of gas-generators, more particularly free-pistongenerators, producing hot gas under pressure

Info

Publication number
GB867762A
GB867762A GB7061/60A GB706160A GB867762A GB 867762 A GB867762 A GB 867762A GB 7061/60 A GB7061/60 A GB 7061/60A GB 706160 A GB706160 A GB 706160A GB 867762 A GB867762 A GB 867762A
Authority
GB
United Kingdom
Prior art keywords
generators
gas
conduits
communication
installation
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
GB7061/60A
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.)
Societe dEtudes et de Participations Eau Gaz Electricite Energie SA
Original Assignee
Societe dEtudes et de Participations Eau Gaz Electricite Energie SA
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 Societe dEtudes et de Participations Eau Gaz Electricite Energie SA filed Critical Societe dEtudes et de Participations Eau Gaz Electricite Energie SA
Publication of GB867762A publication Critical patent/GB867762A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B71/00Free-piston engines; Engines without rotary main shaft
    • 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
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/06Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output
    • F02C5/08Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output the gas generator being of the free-piston type

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Abstract

867,762. Combustion product plant. SOC. D'ETUDES ET DE PARTICIPATIONS EAU GAZ, ELECTRICITE, ENERGIE S.A. Feb. 29, 1960 [March 18, 1958], No. 7061/60. Class 7(1)' An installation comprising a plurality of gas generators producing hot gas under pressure more particularly freepiston generators is characterized by a passage connecting two compressor cylinders of at least two gas generators and by means permitting the transfer of air through the passage from one of the two compressor cylinders to the other at least at low loads. In Fig. 1 the two engine cases 8 may communicate with one another as shown or may if preferred be separated from each other by a closure plate 10 shown dotted. In place of the mean pressure acting below the face 16b of the piston 16 a pressure taken from the cushion for a predetermined position of the piston elements 3b may be employed. There is established at least for low loads of the installation a communication between at least two of the compressor compartments 2a of the two gas-generators A and B for at least a part of their working cycle during which different pressures prevail in these cylinders such that there is a transfer of air from one of the cylinders to the other. It is assumed that the two gas-generators A and B are maintained at a constant phase difference of 180 degrees. In such case it is merely necessary to provide in the communication conduits 33 means which by construction or more or less complete closure produce in the conduits 33 a variable resistance to the flow of transferred air. These means effect a greater reduction in the cross-section of the conduits 33 as the load of the installation increases and close these conduits completely at a load at which the turbine 28 can absorb the quantity of gas supplied by the gas generators without the communication. The means for controlling the free cross-section of the conduits 33 may have for example the form of slide valves 34. A rod 35 connects together the two slide valves 34 and these two valves are controlled by a factor whose magnitude depends upon the load under which the installation is operating. To effect this control of the slide valves they may be connected by means of a rod 35a to a piston 36 under the action of liquid put under pressure by a governor 27 driven by the turbine 28 the liquid also controlling the fuel supply. Preferably, the transfer conduits 33 are inside the casing 6 to reduce noise produced by the transfer. To maintain the two generators at a phase difference of 180 degrees there may be used a device such as that shown in the left hand part of Fig. 1 and comprising a contactor arm 38 driven at a fixed speed for example by an electric motor. The displacement of the brushes 39 and 40 determines the displacement in the functioning of the pistons of the gas generators as described in Specification 853,183. To ensure a discharge as long as the gas generators are running in phase, each of the conduits 33 is put in communication with the surrounding air or with the suction casing and this communication is closed only at the moment at which the desired phase difference between the gas generators is obtained. A particularly simple device for effecting this is shown in Fig. 2. Fig. 5 shows a simplified system applied to an installation having two generators operating with a phase difference of 180 degrees. The slide valve 34 can occupy only two positions, one for which it completely closes the conduit 33 and the other for which it completely opens the conduit 33. The valve 34 is controlled by means of a cock 48. The slide valve 34 is opened fully only for starting and running idle. It is sufficient to provide the slide valve 34 on one side only of the two generators. The arrangement of Fig. 7 is applicable to the case where the gas generators operate almost always at their maximum power or to the case where fuel consumption is of secondary importance and where simplification of the installation is of first importance. In this arrangement the output of power gas is regulated throughout the entire range of different powers by greater or lesser opening of the conduit 33 connecting together the two compressor spaces 2a. The slide valve 34 completely closes the conduit 33 only at the moment when maximum power is reached. The slide valve may be controlled by a governor 27 as shown in Fig. 1. Regulation of the quantity of fuel injected may be effected by the pressure prevailing in the engine case 8 of each gas generator. The cross-section of the communication conduit 33 may be constant and the phase difference between the two gas generators may be varied. The phase difference may be varied by movement of at least one of the brushes 39, 40 (Fig. 1). The phase difference between the gas generators and the cross-section of the conduit or conduits 33 may be varied simultaneously. The single control member 34 may be replaced by tvo control members controlled simultaneously, each of these members being close to one of the two compressor spaces. The communication between the compressor cylinders may be controlled by alternating means which during each working cycle of the free pistons produce an opening and closing of the communication between the compressor spaces. The number of gas generators having their compressor spaces connected together by a transfer conduit may be greater than two.
GB7061/60A 1959-03-18 1960-02-29 Installation comprising a plurality of gas-generators, more particularly free-pistongenerators, producing hot gas under pressure Expired GB867762A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR867762X 1959-03-18

Publications (1)

Publication Number Publication Date
GB867762A true GB867762A (en) 1961-05-10

Family

ID=9345808

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7061/60A Expired GB867762A (en) 1959-03-18 1960-02-29 Installation comprising a plurality of gas-generators, more particularly free-pistongenerators, producing hot gas under pressure

Country Status (1)

Country Link
GB (1) GB867762A (en)

Similar Documents

Publication Publication Date Title
US3096615A (en) Turbocharger system for internal combustion engines
US2365616A (en) Regulating apparatus for gas turbine plants
GB1002051A (en) Improvements relating to internal combustion engines
US4433547A (en) Torque leveller
GB772287A (en) Power system incorporating a gas turbine
GB867762A (en) Installation comprising a plurality of gas-generators, more particularly free-pistongenerators, producing hot gas under pressure
US5163292A (en) Simplified fluid pressure operated engine
US2435232A (en) Regulating the scavenging of free piston engines
US2849995A (en) Free piston machine operation
US2387560A (en) Aircraft power plant for high altitude flight
US2567486A (en) Power plant having means for automatically charging the engine with scavenging air
US3011484A (en) Installations comprising a plurality of auto-generators producing hot gas under pressure
US3092958A (en) Free piston engine
US3827241A (en) Governing power output of hot gas engines
US2565324A (en) Gas turbine with throttling air turbine in compressor intake
GB893029A (en) Improvements in installations comprising at least one freepiston gas-generator and at least one turbine driven thereby
US2960818A (en) Gas-generators of the internal-combustion-operated free-piston type
US3782119A (en) Stirling cycle engine with power control by charge of working gas pressure
US2541419A (en) Gas metering apparatus for gas engines
JPH06173699A (en) Internal combustion engine for generating device
US2608052A (en) Fluid pressure control apparatus for free piston machines
US3410307A (en) Installations comprising several free piston autogenerators supplying a receiver with driving gases
GB703284A (en) Improvements in the regulation of power plants including a free-piston auto-generator and receiver machine such as a turbine
US2702453A (en) Equipressure power generating plant and method of operating same
US3020706A (en) Control means for free-piston or semi-free piston engines