GB737082A - Improvements in free-piston compressors or gas generators - Google Patents

Improvements in free-piston compressors or gas generators

Info

Publication number
GB737082A
GB737082A GB379651A GB379651A GB737082A GB 737082 A GB737082 A GB 737082A GB 379651 A GB379651 A GB 379651A GB 379651 A GB379651 A GB 379651A GB 737082 A GB737082 A GB 737082A
Authority
GB
United Kingdom
Prior art keywords
air
pressure
duct
discharged
supplied
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
GB379651A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB379651A priority Critical patent/GB737082A/en
Publication of GB737082A publication Critical patent/GB737082A/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
    • F02B71/04Adaptations of such engines for special use; Combinations of such engines with apparatus driven thereby
    • F02B71/06Free-piston combustion gas generators per se

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

737,082. Elastic fluid turbines. PERROTT, F. C. May 16, 1952 [Feb. 16, 1951], No. 3796/51. Class 110 (3). [Also in Group XXVII] - Gas turbines are supplied by a free piston compressor or gas generator (see also Group XXVII). Air and/or combustion products is or are discharged from the cylinder or cylinders at the end of the compression and/or the start of the working stroke. In Fig. 2 inlet ports 42 are supplied with scavenging air and the exhaust is discharged at 44. During or immediately prior to the injection of fuel, valves 46 are opened and air is discharged. The apparatus is mainly to deliver compressed air although combustion products may also be mixed with the air. Fig. 1 shows a plant in which a gas generator 12 is supplied with air under pressure by an axial flow rotary compressor 10. The exhaust of the generator drives low pressure turbines 14, 16 and the generator also supplies air and/or combustion products through a conduit 15a to an highpressure turbine 19. The turbine 19 may exhaust into the conduit 13 or as shown by the chain dotted line may deliver into the conduct 11. Intercoolers 25, 26 may be provided. A combustion chamber 27 may be inserted between the gas generator and the turbine 19. The inlet ports 41 may be arranged to impart a tangential movement to the air. The compressor 10 may be replaced by a reciprocating compressor driven by the reciprocating movement of the pistons of the gas generator. There may be several generators as in Fig. 2 coupled through a swash plate. There is a tendency for a port 45 to be closed by the pistons as they come together and this prevents the pistons coming into contact. Compressed air may be supplied for a combined steam and gas turbine plant. The time of opening of the valve 46 may be adjusted so that it takes place either shortly before or shortly after the instant when the pressure in the cylinder becomes equal to that beyond the valve. Adjustment may be accomplished preferably automatically in accordance with the delivery pressure in the duct 15a. Adjustment may be effected, for example, either by a pressure controlled throttle valve in the duct 15a or by regulating the amount of fuel injected into the cylinder in accordance with the pressure in the duct 15a. The valve 46 may be formed or arranged to provide a throttling effect. The throttling may be provided by the duct through which the air or combustion products are discharged. Means may be provided for adjusting the point in the stroke at which fuel injection commences.
GB379651A 1951-02-16 1951-02-16 Improvements in free-piston compressors or gas generators Expired GB737082A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB379651A GB737082A (en) 1951-02-16 1951-02-16 Improvements in free-piston compressors or gas generators

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB379651A GB737082A (en) 1951-02-16 1951-02-16 Improvements in free-piston compressors or gas generators

Publications (1)

Publication Number Publication Date
GB737082A true GB737082A (en) 1955-09-21

Family

ID=9765065

Family Applications (1)

Application Number Title Priority Date Filing Date
GB379651A Expired GB737082A (en) 1951-02-16 1951-02-16 Improvements in free-piston compressors or gas generators

Country Status (1)

Country Link
GB (1) GB737082A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3103100A (en) * 1954-11-08 1963-09-10 Parsons C A & Co Ltd Gas turbine plants
US4060987A (en) * 1975-05-29 1977-12-06 Shlomo Chaim Fisch Turbine drive system
FR2482659A1 (en) * 1980-05-19 1981-11-20 Grow Harlow Compression ignition controlled free piston turbine engine - includes piston which moves reciprocally within cylinder to deliver gases to pulse turbine with two-cycle loop scavenging
CN113047949A (en) * 2021-03-12 2021-06-29 哈尔滨工程大学 Split-cylinder free piston generator based on PID closed-loop control

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3103100A (en) * 1954-11-08 1963-09-10 Parsons C A & Co Ltd Gas turbine plants
US4060987A (en) * 1975-05-29 1977-12-06 Shlomo Chaim Fisch Turbine drive system
FR2482659A1 (en) * 1980-05-19 1981-11-20 Grow Harlow Compression ignition controlled free piston turbine engine - includes piston which moves reciprocally within cylinder to deliver gases to pulse turbine with two-cycle loop scavenging
CN113047949A (en) * 2021-03-12 2021-06-29 哈尔滨工程大学 Split-cylinder free piston generator based on PID closed-loop control

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