WO2009128623A2 - Moteur à air comprimé - Google Patents

Moteur à air comprimé Download PDF

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Publication number
WO2009128623A2
WO2009128623A2 PCT/KR2009/001846 KR2009001846W WO2009128623A2 WO 2009128623 A2 WO2009128623 A2 WO 2009128623A2 KR 2009001846 W KR2009001846 W KR 2009001846W WO 2009128623 A2 WO2009128623 A2 WO 2009128623A2
Authority
WO
WIPO (PCT)
Prior art keywords
air
compressed air
compressed
main frame
air pressure
Prior art date
Application number
PCT/KR2009/001846
Other languages
English (en)
Korean (ko)
Other versions
WO2009128623A3 (fr
Inventor
박준태
Original Assignee
Park Joontai
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 Park Joontai filed Critical Park Joontai
Publication of WO2009128623A2 publication Critical patent/WO2009128623A2/fr
Publication of WO2009128623A3 publication Critical patent/WO2009128623A3/fr

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/14—Gas-turbine plants having means for storing energy, e.g. for meeting peak loads
    • F02C6/16—Gas-turbine plants having means for storing energy, e.g. for meeting peak loads for storing compressed air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/16—Mechanical energy storage, e.g. flywheels or pressurised fluids

Definitions

  • the gas molecules are not stationary, the gas molecules constantly move themselves in an irregular linear motion, and the compressed air pressure that expresses the force (gas molecular kinetic energy) that the gas molecules impinge on the wall of the sealed container is the power source.
  • the rotating body 20 is rotated by the pressure (compressed air molecular kinetic energy) of the compressed air supplied to and stored in an air pressure chamber formed in the rotating body 20 mounted on the main frame 10 of the apparatus of the present invention. It is related with the "compressed air engine” which generate
  • Air pressure chamber as a means for blocking the compressed air supplied to the air pressure chamber (bulkhead) formed in the rotating body 20 rotatably mounted to the main frame 10 of the apparatus of the present invention
  • the air exhaust chamber formed in the main frame 10 without discharging the compressed air rotated by the rotating body 20 to the atmosphere. It became the summary comprised by the means which can discharge to the exhaust air chamber and reuse the compressed air stored in the air tank 50.
  • Compressed air which rotates a turbine at the pressure of compressed air acting on the turbine blades of a conventional compressed air turbine engine that generates power by using compressed air, is discharged to the atmosphere and reused compressed air. There is a problem that cannot be used.
  • Air pressure chamber as a technique for supplying the compressed air stored in the air tank 50 without being discharged to the atmosphere and resupplying it to the air pressure chamber. It is a compressed air engine serving as a means for solving the problem of generating power to the drive shaft 30 by rotating the rotating body 20 at the pressure of the compressed air supplied and stored.
  • the compressed air pressure that is applied to the turbine blade wheel of the conventional compressed air turbine engine is discharged into the atmosphere because the compressed air that is rotated by the turbine is not discharged to the atmosphere.
  • the present invention relates to a technology configured as a means to be reused.
  • the main frame 10 Bulkheads which are mounted to reciprocate in multiple bulkhead rooms formed in the tank, block the compressed air supplied to the air pressure chamber.
  • the pressure of the compressed air stored in the air pressure chamber is controlled by the compressed air pressure acting on the wall surface of the bulkhead and the wall surface of the air pressure chamber. It is the technique of the summary which can generate the power to the drive shaft 30 by rotating ().
  • An air pressure chamber formed in the rotating body 20 which is mounted on the inner diameter formed in the main frame 10 of the apparatus of the present invention and rotates, is formed in the main frame 10.
  • the bulkhead which is mounted to reciprocate in the bulkhead room, can be inserted into the air pressure chamber formed in the rotor 20 by the elastic action of the coil spring 42.
  • the mounted airhead wall is formed by moving a roller mounted at the end of the airhead wall while sliding at the bottom of the air pressure chamber. It is designed to be reinserted into the bulkhead room.
  • the compressed air supplied to the air pressure chamber is shut off by an air barrier so that the compressed air stored in the air pressure chamber is not discharged to the atmosphere.
  • the compressed air exhausted in the exhaust air chamber (Exhaust air chamber) is stored in the air tank (50) through the air exhaust pipe (34) It is configured such that the compressed air stored in the air tank 50 is resupplied to the air pressure chamber to rotate the rotor 20 at the pressure of the compressed air to power the drive shaft 30. Generates.
  • the drive shaft 30 is used as a means for reusing and storing the compressed air in which the rotating body 20 is rotated by the compressed air pressure to the air tank 50 without discharging it to the atmosphere. To generate power;
  • the compressed air stored in the compressed air tank 60 controls the air control valve 60A, and the compressed air supplied to the compressed air supply chamber formed in the main frame 10 is compressed. Compressed air discharged from the air outlet of the air supply chamber is blocked by the compressed air supplied to the air pressure chamber through an opening formed in the air pressure chamber. As a means of blocking the bulkhead, the pressure of the compressed air supplied and stored in the air pressure chamber is applied to the wall surface of the bulkhead and the air pressure chamber. Power is generated on the drive shaft 30 by rotating the rotor 20 in the direction of the arrow (A) with the compressed air pressure (compressed air molecular kinetic energy) acting on the wall in the direction of the arrow (AB).
  • the compressed air stored in the air pressure chamber As a means for blocking the bulkhead, it is a means for discharging the compressed air into the exhaust air chamber formed in the main frame 10, and passes through the air exhaust pipe 34 connected to the exhaust air chamber. Compressed air discharged from the exhaust air chamber is stored in the air tank 50.
  • the compressed air discharged from the air pressure chamber (air pressure chamber) is discharged to the air tank 50 and the effect that can be reused stored air (; ⁇ );
  • Air circulation pump (50A) is operated to supply compressed air to air
  • FIG. 1 is a schematic longitudinal cross-sectional view in which the drive shaft 30 fixedly mounted to the rotating body 20 is rotatably mounted to the main frame 10 and the sealing cover 10A.
  • FIG. 2 shows the air barrier wall 41A, 41B, 41C, 41D and the rotating body 20 which are mounted to reciprocate in the air barrier wall device chambers 40A, 40B, 40C, and 40D formed in the main frame 10.
  • FIG. Schematic cross section of the air pressure chambers 21A, 21B, 21C, 21D, 21E, 21F formed in the chamber.
  • FIG. 3 shows the compressed air supply chambers 11A, 11B, 11C, and 11D formed in the main frame 10, air blocking wall device chambers 40A, 40B, 40C, and 40D, and air exhaust chambers 32A, 32B, 32C, and 32D.
  • Fig. 4 is a schematic cross-sectional view showing an arrow on the movement of the air blocking wall 41A mounted to be able to reciprocate in the air blocking wall device chamber 40A formed in the main frame 10. Figs.
  • FIG. 5 is a schematic partial cross-sectional view showing an arrow for the movement of the air blocking wall 41A mounted to be capable of reciprocating in the air blocking wall device chamber 40A formed in the main frame 10.
  • FIG. 5 is a schematic partial cross-sectional view showing an arrow for the movement of the air blocking wall 41A mounted to be capable of reciprocating in the air blocking wall device chamber 40A formed in the main frame 10.
  • FIG. 6 is a schematic connection diagram of a compressed air tank 60 connected to an air tank 50.
  • 11A, 11B, 11C, 11D compressed air supply chamber.
  • 21A, 21B, 21C, 21D, 21E, 21F air pressure chamber.
  • 32A, 32B, 32C, 32D Exhaust air chamber.
  • 40A, 40B, 40C, 40D Bulkhead room.
  • 60A Air control valve.
  • Air pressure chamber 21A in which air blocking walls 41A, 41B, 41C, 41D, which are mounted to reciprocate at 40C, 40D, are formed on the outer diameter side of the rotating body 20. It is configured to be inserted into the air pressure chambers 21A, 21B, 21C, 21D, 21E and 21F through the openings formed in the 21B, 21C, 21D, 21E and 21F. Compressed air supplied to the compressed air supply chambers 11A, 11B, 11C, and 11D formed in the main frame 10, and the compressed air stored in the direction of the arrow A in the direction of the arrow (A) 21A, 21B, 21C ( Compressed air supplied to 21D) 21E and 21F is an air exhaust chamber 32A and 32B.
  • the air blocking walls 41A, 41B, 41C, and 41D block the 32C, 32D, and the air pressure chambers 21A, 21B, 21C, 21D, 21E, and 21F.
  • the compressed air pressure supplied to and stored in the arrow (AB) direction acts as a reaction of the air pressure on the walls of the air barrier walls 41A, 41B, 41C, 41D mounted on the main frame 10.
  • the configuration of the present invention is configured by the rotating body 20 rotatably mounted in (iii) to generate power as follows.
  • the compressed air discharged from the air outlets of the 11B, 11C, and 11D can be supplied to the air pressure chambers 21A, 21B, 21C, 21D, 21E, 21F formed in the rotor 20. Compressed to the main frame 10 such that an air outlet of the compressed air supply chambers 11A, 11B, 11C, and 11D is formed toward the inner diameter formed in the main frame 10. Air supply chambers 11A, 11B, 11C, and 11D are formed.
  • the air blocking walls 41A, 41B, 41C, and 41D pass through openings formed in the air pressure chambers 21A, 21B, 21C, 21D, 21E, and 21F.
  • air blocking walls 41A, 41B, 41C, 41D are sliding at the bottom of air pressure chambers 21A, 21B, 21C, 21D, 21E, 21F.
  • the rollers 41 are respectively attached to the ends of the air blocking walls 41A, 41B, 41C, and 41D so as to be movable.
  • An air barrier wall to prevent the compressed air supplied to the air pressure chambers 21A, 21B, 21C, 21D, 21E, and 21F from being discharged to the air exhaust chambers 32A, 32B, 32C, and 32D.
  • 41A, 41B, 41C and 41D block and rotate the rotor 20 at the pressure of the compressed air stored in the air pressure chambers 21A, 21B, 21C, 21D, 21E and 21F.
  • the air barrier walls 41A, 41B, 41C, 41D can be inserted into the air pressure chambers 21A, 21B, 21C, 21D, 21E, 21F by the elastic action of the coil spring 42.
  • the spring frame 43 is fixedly mounted to the main frame 10 so as to seal the opening of the 40C and 40D.
  • the compressed air stored in the compressed air supply chambers 11A, 11B, 11C, and 11D is discharged through the air outlets of the compressed air supply chambers 11A, 11B, 11C, and 11D, and the air pressure chambers 21A and 21B.
  • Air pressure chambers 21A, 21B, 21C through openings of 21C, 21D, 21E, 21F.
  • the air pressure chambers 21A, 21B, 21C and 21D so that compressed air can be supplied to the 21D, 21E and 21F.
  • the air pressure chambers 21A, 21B, 21C, 21D, 21E and 21F are rotated so that the openings of the 21E and 21F are formed on the outer diameter side of the rotating body 20. It is formed in the whole 20.
  • the drive shaft 30, which is driven by the rotational force of the rotating body 20 rotating at the compressed air pressure stored in the air pressure chambers 21A, 21B, 21C, 21D, 21E, 21F, is rotated. It is inserted into the center hole formed in 20 and fixedly mounted.
  • the drive shaft 30 is rotatably mounted to the bearing 30A mounted in the hole formed in the main frame 10.
  • the drive shaft 30 is rotatably mounted to the bearing 30B mounted in the hole formed in the sealing cover 10A.
  • the drive shaft 30 is mounted on the bearing 30B mounted on the sealing cover 10A so that the compressed air stored in the air 21 is vented to 21F and the sealing cover 10A is mounted on the main frame. 10 is fixedly mounted.
  • An air exhaust pipe 34 is connected to an air exhaust port 32 formed in the air exhaust chambers 32A, 32B, 32C, and 32D formed in the main frame 10, and the air exhaust pipe 34 is an air tank 50. Is mounted on the connection.
  • the air circulation pump 50A connected to the air tank 50 is compressed so that the compressed air stored in the air tank 50 can be supplied to the compressed air tank 60 by operating the air circulation pump 50A. Connected to the air tank 60 is mounted.
  • the air supply pipe 44 is connected to the air control valve 60A attached to the compressed air tank 60, and the air supply port 11 is formed in the compressed air supply chambers 11A, 11B, 11C, and 11D, respectively. ) Is connected to the air supply pipe (44).
  • Compressed air tank 60 for compressing atmospheric air using air compressor 50B so that the compressed air stored in the compressed air tank 60 can be maintained at a constant pressure.
  • Air compressor 50B is connected to the air compressor, and when the compressed air stored in the compressed air tank 60 is overpressured, the emergency discharge valve 60B is a means for discharging the compressed air to the atmosphere. 60 is mounted.
  • air blocking walls 41A and 41C and air blocking walls 41B and 41D are provided with air pressure chambers 21A and 21B. ) (21C) (21D)
  • the compressed air stored in the compressed air tank 60 is supplied to the compressed air supply chambers 11A, 11B, 11C, 11D by adjusting the air control valve 60A. (See Fig. 6)
  • the air blocking wall 41A mounted so that the rotating body 20 rotates by the compressed air pressure and reciprocates in the air blocking wall device room 40A by the elastic action of the coil spring 42 is indicated by an arrow (B). Direction is inserted into the air pressure chamber 21A. (See Fig. 4)
  • the compressed air supplied to the compressed air supply chamber 11A is discharged from the air outlet of the compressed air supply chamber 11A, and the compressed air is arrowed through the opening of the air pressure chamber 21A formed in the rotor 20.
  • the compressed air blocked by the air blocking wall 41A inserted into the air pressure chamber 21A and the wall surface of the air pressure chamber 21A
  • the rotating body 20 rotates in the direction of arrow A by the compressed air pressure acting on the wall surface of the air blocking wall 41A in the direction of arrow AB. (See Fig. 4)
  • the compressed air discharged to the air exhaust chamber 32A is discharged and stored in the air tank 50 connected to the air exhaust pipe 34 through the air exhaust port 32.
  • the compressed air discharged and stored in the air tank 50 is supplied to the compressed air tank 60 by means of an air circulation pump 50A.
  • the air blocking wall 41A is moved in the direction of the arrow (B) by the elastic action of the coil spring 42 mounted in the air blocking wall device chamber 40A so that the air blocking wall 41A is rotated.
  • the roller 41 which is inserted into the air pressure chambers 21A, 21B, 21C, 21D, 21E, and 21F formed in the sequential order, is mounted at the end of the air blocking wall 41A.
  • the air pressure chambers 21A and 21B are also applied to the walls 41B, 41C, and 41D in the same manner as the air blocking wall 41A.
  • 21E, 21B, 21C, 21D, 21E are supplied and discharged sequentially to 21E and 21F.
  • the compressed air supplied to the 21F is blocked by the air blocking walls 41A, 41B, 41C, 41D, and the air pressure chambers 21A, 21B, 21C, 21D, 21E.
  • Power is generated in the drive shaft 30 by rotating the rotor 20 in the direction of the arrow (A) with the compressed air pressure stored in the 21F).
  • compressed air engine As a “compressed air engine” that provides power to machinery that requires industrial power (generators, automobiles, locomotives, ships, etc.), compressed air that does not generate greenhouse gas (Co2) is used as a power source. It is a power generator that produces power by pressure (compressed air molecule kinetic energy).

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

L'invention porte sur un moteur à air comprimé qui fournit de l'énergie à partir d'un air comprimé à haute pression (énergie cinétique des molécules de l'air comprimé). Le moteur selon l'invention comprend un châssis principal comportant un espace de cloison et une cloison, qui est montée sur l'espace de cloison de façon qu'elle peut faire des mouvements de va-et-vient dans l'espace de cloison. La cloison enferme l'air comprimé qui alimente une chambre de pression d'air ménagée dans une turbine à air. Un rotor de la turbine à air est monté dans les limites de la circonférence interne du châssis principal, de manière qu'il peut tourner. L'air comprimé stocké dans la chambre à air comprimé fait tourner la turbine à air et est ensuite stocké dans un réservoir d'air sans être évacué dans l'atmosphère, ce qui permet de le réutiliser. L'invention permet de cette manière de produire de l'énergie à partir de la rotation de la turbine à air sous l'effet de l'air comprimé, et d'approvisionner en énergie des équipements mécaniques (générateur de puissance, automobile, navire, compresseur, etc.).
PCT/KR2009/001846 2008-04-18 2009-04-10 Moteur à air comprimé WO2009128623A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR1020080036149A KR100957452B1 (ko) 2008-04-18 2008-04-18 압축공기엔진
KR10-2008-0036149 2008-04-18

Publications (2)

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WO2009128623A2 true WO2009128623A2 (fr) 2009-10-22
WO2009128623A3 WO2009128623A3 (fr) 2010-01-21

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PCT/KR2009/001846 WO2009128623A2 (fr) 2008-04-18 2009-04-10 Moteur à air comprimé

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WO (1) WO2009128623A2 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015149575A1 (fr) * 2014-04-04 2015-10-08 丛洋 Turbine de moteur à gaz comprimé et moteur correspondant
SE2130344A1 (en) * 2021-12-06 2023-06-07 Wadeea Khalaf Hydro-Compressed Air Pure Energy. (HCAPE)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101360668B1 (ko) * 2011-01-18 2014-02-07 박준태 공기압력엔진

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4604029A (en) * 1983-04-20 1986-08-05 Findeva Ag Compressed-air vibrator with turbine drive
KR20070108967A (ko) * 2006-05-09 2007-11-15 박준태 압축공기터빈기관

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01106901A (ja) * 1987-10-20 1989-04-24 Suke Ishii ノヅルの回転を遅くしたエンジン
JPH1193601A (ja) 1997-09-18 1999-04-06 Osaka Gas Co Ltd エアモータおよびその運転装置
JPH11173101A (ja) 1997-12-05 1999-06-29 Max Co Ltd ロータリーベーン型エアモータ

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4604029A (en) * 1983-04-20 1986-08-05 Findeva Ag Compressed-air vibrator with turbine drive
KR20070108967A (ko) * 2006-05-09 2007-11-15 박준태 압축공기터빈기관

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015149575A1 (fr) * 2014-04-04 2015-10-08 丛洋 Turbine de moteur à gaz comprimé et moteur correspondant
SE2130344A1 (en) * 2021-12-06 2023-06-07 Wadeea Khalaf Hydro-Compressed Air Pure Energy. (HCAPE)

Also Published As

Publication number Publication date
WO2009128623A3 (fr) 2010-01-21
KR20080048997A (ko) 2008-06-03
KR100957452B1 (ko) 2010-05-11

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