EP0033728A1 - Explosionsturbine und gasverteiler - Google Patents

Explosionsturbine und gasverteiler

Info

Publication number
EP0033728A1
EP0033728A1 EP80900155A EP80900155A EP0033728A1 EP 0033728 A1 EP0033728 A1 EP 0033728A1 EP 80900155 A EP80900155 A EP 80900155A EP 80900155 A EP80900155 A EP 80900155A EP 0033728 A1 EP0033728 A1 EP 0033728A1
Authority
EP
European Patent Office
Prior art keywords
distributor
combustion
drive
distributors
turbines
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.)
Withdrawn
Application number
EP80900155A
Other languages
English (en)
French (fr)
Inventor
Henri Le Meur
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
Publication of EP0033728A1 publication Critical patent/EP0033728A1/de
Withdrawn legal-status Critical Current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
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants

Definitions

  • the invention relates to an explosion turbine provided with a gas distribution system by rotary discs or by sliding drawers.
  • the invention solves the problems by creating an explosion turbine equipped with centrifugal or axial compressors, each phase of the thermodynamic cycle of which is carried out fully with disc or drawer distributors while offering the minimum of gas flow resistance as well as a variation of the speed on demand thanks to an electric motor or electromagnets.
  • the advantages obtained essentially consist in obtaining an independent explosion turbine, the thermodynamic cycle of which is carried out with maximum efficiency with an instantaneous speed variation.
  • the drawings representing only one embodiment include: Figure 1, a longitudinal section of the turbine. Figures 2,3,5 and 6 of the cross sections of the gas distributors along AB of this same turbine. Figure 4 an electrical distributor.
  • the thermodynamic cycle of the explosion turbine is defined in 2 stages 1st teaos: Admission-Compression
  • the compressor (1) sends compressed air into the volute (6), regulated at a pressure determined by the valve (7). This air passes through the orifices of the intake distributor (8) in the combustion chambers (9) 2nd stage: Explosion-Detent-Sweep Explosion:
  • the intake distributor (8) closes, the expansion valve (10) always closed. Fuel injection by the injector (14), ignition of the gas mixture by the spark plugs (15), combustion, rise in temperature and pressure. Relaxation:
  • the expansion valve (10) opens.
  • the intake distributor (8) opens, the expansion valve (10) always open.
  • the fresh air coming from the compressor sweeps the remainder of the burnt gases through the openings of the intake distributor (8) which has just opened.
  • the expansion valve (10) closes, the intake valve (8) continues to supply fresh air to the chamber (9) and the cycle begins again.
  • the electric motor (11) with its speed variations determines the number of explosions thus performing the role of accelerator, it simultaneously controls the ignition and the injection of fuel.
  • the intake (8) and expansion (10) distributors are identical and are placed upstream and downstream of the combustion chambers (9).
  • the intake (8) and expansion (10) distributors are each formed (FIG. 2) of two fixed discs (16) and (17) between which a rotating disc (18) on a central ring moves with gentle friction ( 19).
  • the outer ring (20) assembles the discs (16) and (17).
  • the discs (lô) and (17) have one or more orifices (21) located at the assembly opposite one another.
  • the quantity of these orifices (21) corresponds to the number of combustion chambers (9) of the turbine.
  • the tightness of the intake or expansion orifices (21) on the combustion chamber side is ensured by circular segments (22) floating on circular springs (23) and friction on the rotary disc (18).
  • the segment (22) may have in its middle a groove (24) which would divide it in two.
  • the tightness of the intake and expansion side is ensured by two projections (25) in the form of a circular segment around the disc, which allows the minimum of friction to be obtained.
  • the rotary disc (18) has one or more openings (26) which, once opposite the orifices (21) of the fixed discs (16) and (17) ensure the admission or the expansion of the combustion chambers (9).
  • the rotating discs (18) have teeth (27) on their periphery which mesh with the pinions (13) driven together by the drive shaft (12) and the variable speed electric motor (11).
  • the lights (26) of the rotary discs (18) for intake and expansion are identical, in the assembly they overlap slightly (hatched part) which allows scanning at the end of the cycle.
  • the combustion chambers (9) are supplied one after the other, with two supply lights of two diametrically opposed combustion chambers, with three lights supply in triangle or star, with four in square, this which gives multiple combinations depending on the number of rooms.
  • the rotary discs (18) have sodium in their middle where they are cooled in air by ventilation (28).
  • a source of air from the compressor (1) supplies the interior of the rotating disc (18) across the central ring (19).
  • Internal ribs (29) channel the air by licking the lights (26) to exit on the periphery like a rotary jet.
  • the discs (16) and d7) are cooled with air by means of fins or with water;
  • the discs (18) are lubricated by two oil inlets (30) on the combustion chamber side and by two inlets (30) in the projections (25) on the intake and expansion side.
  • the drive pinions (13)) are oiled by the fallout and evacuation takes place through the orifice (31).
  • the intake (8) and expansion (10) distributors with sliding drawers are the same and formed (FIG. 3) of two identical fixed rectangular plates (32) and (33) each having an orifice (34) located at the assembly opposite and around one of them (the one on the combustion chamber side) is a circular sealing segment (22) floating on a circular spring (23) identical to that of the rotary disc distributors.
  • the sliding drawer (35) has in its center at the place where the explosion occurs as well as on the other face, a cavity (37) equal to the diameter of the orifice (34) on the chamber side and larger by l 'other side to obtain, the minimum friction.
  • the sliding drawer (35) in its reciprocating movement obstructs or releases the orifices (34) for admission and expansion of the chambers (9).
  • the reciprocating movement of these sliding drawers (35) is done by means of a rod (38) controlled by an electromagnet (39) itself controlled by a rotary electrical distributor (40) ( Figure 4).
  • the sliding drawers (35) are lubricated by two oil inlets (41), one on each side over the thickness of the drawer and evacuation through the orifice (42).
  • the sliding drawers (35) can also be controlled by cams (43) (FIG. 5) driven by the motor (11) by means of the axis (44)
  • cams (43) (FIG. 5) driven by the motor (11) by means of the axis (44)
  • the particularity of this cam (43) is, that it has all around its profile a groove (45) in which the pins (46) slide with a roller (47) fixed on the sliding drawers (35).
  • Two sliding drawers (35) are coupled on the same cam ( Figure 6) which allows two combustion chambers (9) to work alternately.
  • the relationship between the cams is made by means of a toothed rubber belt (48).
  • the cam (43) is lubricated by two oil inlets (49), one on each side and the discharge through the orifice (50).
  • the sliding drawers (35) have sodium in their middle and the plates (32) and (33) are cooled with air by means of fins or with water.
  • the turbine object of the invention can be used in cars, aviation, the navy and in industry for the production of electricity.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sliding Valves (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
EP80900155A 1979-05-03 1980-11-17 Explosionsturbine und gasverteiler Withdrawn EP0033728A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR7912381A FR2455677A1 (fr) 1979-05-03 1979-05-03 Turbine a explosions et systemes de distribution des gaz par disques rotatifs ou par tiroirs coulissants
FR7912381 1979-05-03

Publications (1)

Publication Number Publication Date
EP0033728A1 true EP0033728A1 (de) 1981-08-19

Family

ID=9225506

Family Applications (1)

Application Number Title Priority Date Filing Date
EP80900155A Withdrawn EP0033728A1 (de) 1979-05-03 1980-11-17 Explosionsturbine und gasverteiler

Country Status (7)

Country Link
EP (1) EP0033728A1 (de)
JP (1) JPS6033979B2 (de)
DE (1) DE3043412C2 (de)
FR (1) FR2455677A1 (de)
GB (1) GB2071768B (de)
IT (1) IT1146114B (de)
WO (1) WO1980002444A1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3507856A1 (de) * 1985-03-06 1986-09-11 Kurt 5630 Remscheid Uhlitz Turbinen-verbrennungsmotor
DE4113680A1 (de) * 1991-03-12 1992-09-17 Asea Brown Boveri Gasturbogruppe
DE4314646A1 (de) * 1993-05-04 1994-11-10 Josef Lipinski Kolbenloser Verbrennungsmotor, der nach dem Einspritz- oder Dieselverfahren arbeitet
WO1995004214A1 (en) * 1993-07-27 1995-02-09 Sergei Felixovich Tandilov Rotating slide valve
HUP9602589A3 (en) * 1996-09-23 1999-03-29 Diviak Janos Electrically controlled intermittent gas turbine
FR2829528B1 (fr) * 2001-09-07 2004-02-27 Bernard Gilbert Macarez Pulsomoteur-turbomoteur a impulsion-turbine a gaz a chambre de combustion impulsionnelle et a detente de bouffees
JP6132979B2 (ja) * 2014-04-18 2017-05-24 アムネクスト・テクノロジ株式会社 燃焼ガスを駆動力として噴出するエンジン
RU2610362C1 (ru) * 2015-10-06 2017-02-09 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Способ работы и устройство блока пульсирующих камер сгорания
RU2674091C1 (ru) * 2017-10-30 2018-12-04 федеральное государственное автономное образовательное учреждение высшего образования "Самарский национальный исследовательский университет имени академика С.П. Королёва" Пульсирующий турбореактивный двигатель
JP6755052B1 (ja) * 2019-07-10 2020-09-16 バイオチューブ株式会社 結合組織体及びその製造方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR957489A (de) * 1950-02-20
FR999239A (de) * 1952-01-29
US1552272A (en) * 1921-04-18 1925-09-01 Carner James Frederick Explosive engine or turbine
DE897771C (de) * 1942-08-28 1953-11-23 Karl Dr-Ing Leist Brennkammer mit periodischer Verbrennung z. B. fuer Gasturbinen und Strahltriebwerke
US2579321A (en) * 1948-04-09 1951-12-18 Nina K Guercken Apparatus for producing gas under pressure
US2861422A (en) * 1951-06-18 1958-11-25 Herbert L Magill Power gas generator
DE1218218B (de) * 1963-04-06 1966-06-02 Eugen Groeger Dr Ing Verpuffungs-Gasturbine
DE1273263B (de) * 1965-10-30 1968-07-18 Eugen Groeger Dr Ing Verpuffungs-Gasturbine
GB1217070A (en) * 1968-07-17 1970-12-23 Rolls Royce Improvements in or relating to gas turbine engines
FR2210718B2 (de) * 1974-02-25 1978-04-14 Meur Henri Le
DE2517947C3 (de) * 1975-04-23 1981-04-16 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Zylindrische Brennkammer für pulsierende Verbrennung, zur Verwendung in einem Strahltriebwerk
DE2646248A1 (de) * 1976-10-13 1978-04-27 Hermann Dipl Ing Dr Tech Hagen Verpuffungs-gasturbinentriebwerk

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8002444A1 *

Also Published As

Publication number Publication date
WO1980002444A1 (fr) 1980-11-13
FR2455677B1 (de) 1985-03-22
IT1146114B (it) 1986-11-12
DE3043412A1 (en) 1982-02-18
FR2455677A1 (fr) 1980-11-28
GB2071768B (en) 1983-04-20
JPS6033979B2 (ja) 1985-08-06
DE3043412C2 (de) 1986-06-26
IT8048535A0 (it) 1980-04-28
JPS56500463A (de) 1981-04-09
GB2071768A (en) 1981-09-23

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Effective date: 19810513