EP1085182A1 - Moteur rotatif à combustion interne - Google Patents

Moteur rotatif à combustion interne Download PDF

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Publication number
EP1085182A1
EP1085182A1 EP99307291A EP99307291A EP1085182A1 EP 1085182 A1 EP1085182 A1 EP 1085182A1 EP 99307291 A EP99307291 A EP 99307291A EP 99307291 A EP99307291 A EP 99307291A EP 1085182 A1 EP1085182 A1 EP 1085182A1
Authority
EP
European Patent Office
Prior art keywords
piston
output shaft
chamber
internal combustion
engine
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.)
Granted
Application number
EP99307291A
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German (de)
English (en)
Other versions
EP1085182B1 (fr
Inventor
Chanchai Santiyanont
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Individual
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Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to DE69917632T priority Critical patent/DE69917632T2/de
Priority to EP19990307291 priority patent/EP1085182B1/fr
Publication of EP1085182A1 publication Critical patent/EP1085182A1/fr
Application granted granted Critical
Publication of EP1085182B1 publication Critical patent/EP1085182B1/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
    • F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B13/00—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion
    • F01B13/04—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder
    • F01B13/045—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder with cylinder axes arranged substantially tangentially to a circle centred on main shaft axis
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
    • F02B57/08—Engines with star-shaped cylinder arrangements

Definitions

  • the present invention related generally to automotive engineering and, more specifically, to an internal combustion rotary engine of the type including reciprocating pistons which rotate around its axis of rotation.
  • each piston chamber is perpendicular to the radius of output shaft.
  • Piston is reciprocated by rotation of its crankshaft.
  • Piston chamber is wrapped with cylindrical shape valve that has curved end to match inner cylindrical surface of casing in order to close and open gas inlet port and exhaust outlet port.
  • Gas inlet port, exhaust outlet port and spark plug holding port are formed on outer cylinder.
  • the engine has a rotary piston, not reciprocating piston, and operated by piston rod, crankshaft, and drive train to rotate two sets of synchronous piston.
  • An internal combustion rotary engine comprising: a casing defining a cylindrical chamber; a rotor with output shaft as an axis in the said cylindrical chamber; crankshaft with pinion gear at the rear end in the rotor; piston chamber and piston in the rotor exists; drive train provided to synchronize the rotation of the output shaft and the crankshaft.
  • the illustrated internal combustion rotary engine comprises a casing formed with a pair of end plates 22, 24 and outer cylinder 26 securely assembled as shown to enclose a cylindrical rotor.
  • the cylindrical rotor has output-shaft 13 as axis.
  • Exhaust-port 7 and suction-port 8 extend through the outer cylinder 26 to provide communication with the cylindrical rotor chamber.
  • Spark plug 9 extends through the outer cylinder 26.
  • the rotor includes two annular bodies 19 having a cylindrical outer surface matching the cylindrical inner surface formed by outer cylinder 26.
  • the rotor includes front mounting plate of crankshaft 20, and rear-mounting plate of crankshaft 21 secured against the annular bodies 19.
  • the output shaft 13 is rotatably mounted and it extends through the casing by which the sleeve bearing in the end plates 22, 24 of the casing support.
  • the axis of output shaft and the axis of rotor are the same (concentric) and rotate together.
  • crankshaft-mounting arm 66 is fixedly secured on the output shaft 13 for bodily rotation with it.
  • a crankshaft-mounting arm 66 includes bearing housing 63, 65 and bearing 64.
  • Piston chambers are fixedly secured with piston chamber bases 37 inside annular body of rotor 19. Each piston chamber axially extends to the outer surface of annular body of rotor 19, and wrapped by its cylindrical shape valve 18. Seal 52 is inserted in annular body of rotor to prevent lube oil leakage from cylindrical shape valve 18.
  • Axis of each piston chamber is perpendicular to the radius of output shaft 13 and preferably uniformly spaced from output shaft axis in the direction of rotor rotation.
  • the cylindrical shape valve 18 is slightly movable along the axis of its piston chamber. The curved end of the valve is pressed with inner cylindrical surface of outer cylinder of casing 26 by coil springs 41 to keep gas tight.
  • the coil springs is seated in spring stem 42 that mounted on piston chamber bases 37 and lower end of cylindrical shape valve 18 to prevent cylindrical valve from moving.
  • At the outer surface of piston chamber base 37 has ring 38 covered to prevent gas leak from cylindrical shape valve 18.
  • Key 39 with spring is mounted in keyway 40, 44 outside of each piston chamber and inside of its cylindrical shape valve 18 respectively.
  • Opening valve 45 is formed at the curve end of cylindrical shape valve 18 to locate the start opening position of exhaust-port and suction-port, and closing valve 46 is located at the start closing position of exhaust-port and suction-port.
  • a piston 17, normally of cylindrical shape similar to conventional construction, is reciprocating in each piston chamber.
  • a piston rod is pivotally connected to each piston 17 and rotatively connected to its corresponding crank of crankshaft 16 by bearing 64.
  • the engine has two engine blocks, the first and the second block, and each block has two pistons.
  • piston chamber bases 37 are fixedly secured on crankshaft front mounting plate 20 and cover of output shaft arm mounting plate 54.
  • piston chamber bases 37 are fixedly secured on crankshaft rear mounting plate 21 and output shaft arm mounting plate 53.
  • Fig. 1 and 2 show the position of gas inlet, exhaust outlet and spark plug for the first engine block and the second engine block respectively.
  • screw gear chamber 25 Between front end plate of casing 24 and crankshaft front mounting plate 20 is screw gear chamber 25, which enclose screw gear 15.
  • the screw gear is formed on the front end of output shaft 13 for driving lube oil pump and ignition distributor.
  • a drive train is provided to synchronize the rotation of the output shaft 13 and both crankshafts 16.
  • the drive train includes an annular gear-carrying cap 32 in drive train chamber 23.
  • the drive train chamber 23 is between rear end plate of casing 22 and rear mounting plate of crankshaft 21.
  • a sleeve to carry the output shaft is formed at the center of annular gear-carrying cap 32 with one end of this sleeve fixedly secured to rear end plate of casing 22.
  • An annular gear 33 is fixed to the annular gear-carrying cap 32.
  • the annular gear 33 mesh with pinion gears formed on the rear end of both crankshafts 16.
  • the drive train shall specify the gear teeth ratio of annular gear to pinion gear to be appropriate to engine efficiency preferably twice the number of pistons in each engine block.
  • the gear teeth ration of annular gear to pinion gear shall be 4:1 so that when the output shaft rotates one round clockwise, the crankshafts will rotate four rounds clockwise.
  • the gear teeth ration of 3,4,6,8 piston engine shall be 6:1,8:1,12:1 and 16:1 respectively.
  • crankshaft 16 As the output shaft 13 and both of crankshafts 16 concurrently rotate, the pistons 17 reciprocate in their piston chamber due to the rotation of crankshaft 16.
  • the reciprocation of the pistons is synchronized with spark plug ignition and the piston chamber then rotate clockwise to the exhaust outlet.
  • fuel mixture is drawn into piston chamber, compressed, ignited by spark plug, and exhausted while the piston chamber rotate clockwise.
  • operation sequence of the engine as shown in the figure 15, 16 and 17 illustrates two sets of engine block. Each block comprises two-pistons.
  • piston chamber No. 1&2 passes through the inlet port while the piston moves down accordingly to suck the fuel air mixture into its piston chamber.
  • the suction stroke is also complete.
  • the second engine block is operating in exhaust stroke (Fig.15, No.71, 72, 73).
  • Compression stroke of the first engine block occurs when piston chamber No.1#2 continues to move around the output shaft while the crankshaft drives piston No.1&2 move up compressing fuel air mixture.
  • the second engine block is operating in suction stroke (Fig.16 No.77, 78).
  • Ignition stroke of the first engine block occurs when piston chamber No.1&2 moves further until the spark plug is positioned at the center of the piston chamber, the spark plug is then ready for ignition. Piston No.1&2 moves down after the combustion of gas in the piston chamber. At the same time the second engine block is operating in compression stroke (Fig.16 No.79)
  • Exhaust stroke of the first engine block occurs when piston chamber No.1&2 complete its downward movement. While moving around to the exhaust port, the piston No.1&2 moves up again to expel the exhaust. When the piston No.1&2 moves up to the top position, piston chamber No.1&2 will pass through and promptly close the exhaust port. At the same time the second engine block is operating in ignition stroke (Fig.17 No.83, 84, 85).
  • Piston chamber No.1 and No.2 comprise first engine block while piston chamber No.3 and No.4 form second engine block.
  • the movement of each pair of piston as well as each pair of engine block must be balanced in order to maximize the generation of power.
  • the engine might comprise a plurality of engine block preferably with at least two engine blocks for balancing.
  • one engine block may comprise a plurality of pistons and piston chambers preferably at least two for the same requirement for balancing.
  • the ignition stage of each piston will substantially equal to no of piston in each engine block that are three, four, six and eight for 3,4,6,8 piston engines respectively.
  • a compressor is basically constructed with the same structure as that of internal combustion rotary engine, having cylindrical chamber; rotor with output shaft as its axis in cylindrical chamber; crankshaft, piston, piston chamber within rotor. Expanding piston chamber created by downward movement of piston draws fluid such as air through filter connected with suction port on outer cylinder. After compression, the fluid is driven out of the exhaust port through pipe to a storage tank for future use.
  • the compressor may be used to compress liquid or gas. While working as a compressor, the reciprocating piston will operate on two-stroke cycle, completing a cycle at each self-revolution of the piston chamber.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Supercharger (AREA)
EP19990307291 1999-09-14 1999-09-14 Moteur rotatif à combustion interne Expired - Lifetime EP1085182B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DE69917632T DE69917632T2 (de) 1999-09-14 1999-09-14 Rotierende Brennkraftmaschine
EP19990307291 EP1085182B1 (fr) 1999-09-14 1999-09-14 Moteur rotatif à combustion interne

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP19990307291 EP1085182B1 (fr) 1999-09-14 1999-09-14 Moteur rotatif à combustion interne

Publications (2)

Publication Number Publication Date
EP1085182A1 true EP1085182A1 (fr) 2001-03-21
EP1085182B1 EP1085182B1 (fr) 2004-05-26

Family

ID=8241620

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19990307291 Expired - Lifetime EP1085182B1 (fr) 1999-09-14 1999-09-14 Moteur rotatif à combustion interne

Country Status (2)

Country Link
EP (1) EP1085182B1 (fr)
DE (1) DE69917632T2 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1777367A1 (fr) * 2005-10-20 2007-04-25 Chanchai Santiyanont Moteur fluide rotatif
CN1769720B (zh) * 2004-11-01 2011-11-23 参猜·山蒂亚农 回转液压马达

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE430810A (fr) *
US1370305A (en) * 1919-07-03 1921-03-01 Edwin A Golle Air-compressor
DE660674C (de) * 1933-09-05 1938-05-31 Julius Pintsch Kom Ges Ventilloser Kompressor fuer Kaeltemaschinen
US3292603A (en) * 1964-12-16 1966-12-20 Wayto Stephen Rotary engine
US3731661A (en) * 1971-12-27 1973-05-08 T Hatfield Rotary engine apparatus
WO1999039090A2 (fr) * 1998-01-30 1999-08-05 Pasha Al Bahdaini Shirwan Al Systeme 'shirwo' (un nouveau systeme d'alimentation a combustion interne)

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE430810A (fr) *
US1370305A (en) * 1919-07-03 1921-03-01 Edwin A Golle Air-compressor
DE660674C (de) * 1933-09-05 1938-05-31 Julius Pintsch Kom Ges Ventilloser Kompressor fuer Kaeltemaschinen
US3292603A (en) * 1964-12-16 1966-12-20 Wayto Stephen Rotary engine
US3731661A (en) * 1971-12-27 1973-05-08 T Hatfield Rotary engine apparatus
WO1999039090A2 (fr) * 1998-01-30 1999-08-05 Pasha Al Bahdaini Shirwan Al Systeme 'shirwo' (un nouveau systeme d'alimentation a combustion interne)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1769720B (zh) * 2004-11-01 2011-11-23 参猜·山蒂亚农 回转液压马达
EP1777367A1 (fr) * 2005-10-20 2007-04-25 Chanchai Santiyanont Moteur fluide rotatif

Also Published As

Publication number Publication date
DE69917632T2 (de) 2005-06-30
DE69917632D1 (de) 2004-07-01
EP1085182B1 (fr) 2004-05-26

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