EP0187148B1 - Rotationsmaschine - Google Patents

Rotationsmaschine Download PDF

Info

Publication number
EP0187148B1
EP0187148B1 EP85902631A EP85902631A EP0187148B1 EP 0187148 B1 EP0187148 B1 EP 0187148B1 EP 85902631 A EP85902631 A EP 85902631A EP 85902631 A EP85902631 A EP 85902631A EP 0187148 B1 EP0187148 B1 EP 0187148B1
Authority
EP
European Patent Office
Prior art keywords
rotor
curve
axis
points
machine according
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 - Lifetime
Application number
EP85902631A
Other languages
English (en)
French (fr)
Other versions
EP0187148A1 (de
Inventor
Italo Contiero
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 EP0187148A1 publication Critical patent/EP0187148A1/de
Application granted granted Critical
Publication of EP0187148B1 publication Critical patent/EP0187148B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/40Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
    • F01C1/44Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the inner member

Definitions

  • This invention relates to a rotary machine which exploits inner cyclic variable volumes.
  • Such an engine as described in the preamble of claim 1 is shown in FR-A-2 235 268.
  • the rotary machine according to the invention is composed of:
  • the rotor is composed of N r sides (N r ⁇ 1) which have N e equal ends with equal surfaces E.
  • N e surfaces E with plane r are N e equal circles or radius r with centres P i which are points of respective axes Y I .
  • Points P run on a curve R N which characterises the rotary machine, as in the Wankel engine, the geometry of which is based on a curve R N , which is a trochoid curve.
  • Perimetral surfaces M or stator cavity U is the external envelope of the rotor surfaces E, which slide round touching surface M along N e equal lines.
  • the present invention has rotor points P, running on trajectories R N different from the above trajectories and described in claim 1.
  • the present invention can work as a pump, compressor, motor, engine, valve, distributor or hydraulic joint; it may burn fuel for heat and/or electricity as in magneto-hydrodynamic generators; it can also be used as a compressor and/or booster for thermic motors with inner reactive combustion.
  • Stator body 1 has an inner cavity with perimetral surface M.
  • Transmission shaft 14 has rotary axis Y c which intersects plane r orthogonally at point C.
  • the rotor touches contour M by interposed rings 10 of radius r.
  • Cylinders 4 and rings 10 have common axis Y I .
  • An non-extensible connection (bar 7) joins pivot/s 6 centered in points D with transmission shaft 14 ( Figures 2 and 3).
  • Rotor sides or pistons 5 have equal height, their flat bases are parallel to plane r and slip over the stator bases.
  • External surface 9 of each piston 5 corresponds to one rotating chamber V.
  • Integer N is modulus of curve R N .
  • Each chamber V is defined by piston wall 9, two surfaces E of rings 10, cylinder M, and two stator bases.
  • N r pistons 5 form one chamber Z of variable volume Z ( ⁇ ) .
  • Chamber Z is defined by N e surfaces 13 of pistons 5, N e surfaces E or rings 10 and the two stator bases; it pumps a fluid which enters and exits through holding valves (not shown in figures). Volumes V ( ⁇ ) and Z ( ⁇ ) are defined in any position of the rotor. The fluid in chamber Z cools and lubricates the machine and may feed a hydraulic accumulator (not shown in figures).
  • the rotor can be made by packing thin metal sheets together. It may also be an open prismatic structure, and composed of only one side without hinges, or composed of solid cylinders only. Chambers V and Z may be interconnected.
  • Figure 4 shows a schematic view of a coaxial cyclic volume machine composed of one rotating cyclic volume machine as a compressor, and one rotating cyclic volume machine as an engine, with one common transmission shaft 14 and one common stator base between them.
  • Operating fluid enters 3 and flows through the two transfer channels 23 bored in the common base, and is controlled by engine rotor P 1 P 2 P 3 p 4 .
  • the fluid enters the two opposite combustion chambers, where it is further compressed for combustion. Waste gases are discharged through channels 24 bored in the stator base of the engine side. Maximum fluid compression occurs in engine area 11, where ignition takes place and expansion of gases rotates the polygonal structure of the engine and the compressor.
  • cooling fluid enters the Z area of the compressor, passing through the Z area of the engine, and powers a hydraulic accumulator which is also a heat radiator (not shown).
  • Axes X 1 and X 2 form angle ⁇ on projection plane. Angle ⁇ is important for precompression of the engine when the axis of channel 23 is parallel to axis Y c .
  • Modulus N conditions the choice of the maximum number N r of rotor sides 1 ⁇ Nr ⁇ N which have number N e of equal cylindrical ends E; 2 ⁇ Ne ⁇ 2(Nr ⁇ 1).
  • Rotor points-P, of the present invention run along curve R N belonging to a new class of curves called ROTOID CURVES with the peculiar geometrical property called invariant length W.
  • Points Fi 1 to N, lie on curve L and distributed in infinite groups of points, each group consisting of N points F 1 , ... F N , N ⁇ 2, (modulus N is constant integer).
  • Axis Y c is orthogonal to a plane r in a point C inside the region defined by curve L. Point C is distinct from baricentre 0 of N-polygon F i .
  • L being a closed curve, function f ( ⁇ ) will be defined for any value of a; then f ( ⁇ ) is a continuous function.
  • a system of N equalities expressed by f, a, ⁇ 1 , ⁇ 2 , ... ⁇ N is valid according to Carnot's theorem, to determine side length W ( ⁇ )
  • W is the side measure of one family of equilateral N-polygons P i .
  • Figure 1 shows a machine in the general case: rotor axis Y o is orthogonal to reference plane r in baricentre O. Baricentre 0 is different from pole C, Y o //Y c . Angles P i P ⁇ i+1 P i+2 vary with anomaly a.
  • Machines with rotor vertices on points Q i are characterized by the non-deformability of the rotor and rotoid curve R N is defined by radius CQ, Figure 5, angles Q i Q ⁇ i+1 Q i+2 are constant.
  • Machines characterized by these trajectories of rotor vertices have axis Y o coinciding with axis Y c and with the symmetry axis of stator cavity U.
  • equations g ( ⁇ ) of formula (2) have the property of invariant length W:
  • equation g ( ⁇ ) defines rotoid curves R N of the machines shown in Figure 3, in which the four points P, are vertices of a family of rhombuses P, with baricentre in pole C. Vertices P, are on rotoid curve R 4 defined by:
  • An inextensible connection (bar 7) joins the middle points of rotor sides P i P i +1 and P i+2 P i+3 to transmission shaft 14.
  • bar 7 has a centre of rotation coinciding with baricentre 0 of rhombus P i .
  • point D need not be on a circumference.
  • the rotor of the cyclic volume machine may be used as a tool to rectify perimetral surface M of inner stator cavity U.
  • Perimetral surface M of stator cavity U may be radiused with stator bases according to a complementary profile to the profile of rotor surface E.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
  • Rotary Pumps (AREA)
  • Permanent Magnet Type Synchronous Machine (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)
  • Lasers (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Lubricants (AREA)
  • Soil Working Implements (AREA)
  • Centrifugal Separators (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Motor Or Generator Cooling System (AREA)

Claims (7)

1. Rotationsmachine bestehend aus:
einem Stator mit einer zylindrischen Bohrung U,
einer Antriebswelle mit Rotationsachse Yc,
einem Rotor mit Rotationsachsen Yo parallel zur Achse Yc und mit Nr Seiten, die Ne gleiche zylindrische Flächen E an den Enden aufweisen; die Bohrung des Stators U hat eine Umfangsfläche M, die aus einer externen Hülle aus Ne zylindrischen Flächen E mit Nr Seiten des Rotors besteht: die Flächen E einer jeden Seite des Rotors haben Längsachsen Yl (i = 1, 2, ... Ne) parallel zur Achse Yc. die die Ebene in den Punkten Pi, Pi+1 in den gleichen Abständen W in jeder beliebigen Winkelposition des Rotors rechtwinklig schneiden, dadurch gekennzeichnet, dass:
jede Seite des Rotors ein rotierender und/oder übersetzender Kolben mit den Punkten Pi und Pi+1 auf einer Rotoidkurve RN ist, die die Eigenschaft der invarianten Länge W = P i P i+1 besitzt; wobei diese kurve durch die Transformation einer flachen, einfachen und geschlossenen Kurve L mit Hilfe des Gesetzes
Figure imgb0029
enthalten ist, in dem:
g(α) ist eine nicht konstante Funktion, die eine Kurve RN in polaren Koordinaten definiert,
f(a) ist eine gegebene, stetige und positive Funktion, die die Kurve L definiert, mit 0≤α≤2π,
W ist die Länge des Segments P i P i+1 eines jeden Kolbens mit i = 1 bis N,
N ist eine ganze Zahl, der das Modul N der Kurve RN entspricht,
W(a) ist die Länge der Seiten eines gleichseitigen N-Polygons F1F2 ... FN mit den auf der Kurve L liegenden Punkten F1, F2 ...FN·
2. Maschine nach Anspruch 1, dadurch gekennzeichnet, dass:
die gegebene Kurve L = L" mit h Symmetrieachsen;
N = 2h;
die Winkel P1ĈF2 = P2ĈF3 = ... PNĈF1=λ sind konstant, wobei r im Punkt C die Achse Yc schneidet;
die Achse Yo des Rotors und die Achse Yc der Antriebswelle sind mit der Symmetrieachse der Statorbohrung U deckungsgleich.
3. Maschine nach Anspruch 2, dadurch gekennzeichnet, dass:
N = 4;
Figure imgb0030
in der N die Anzahl der Symmetrieachsen der Kurve RN darstellt und A, p, q Konstante sind.
4. Maschine nach Anspruch 2, dadurch gekennzeichnet, dass:
der Rotor umfasst 2h Scheitel des Rotors Pi mit i = 1 bis 2h
die gegebene Kurve Lh ist definiert durch die Gleichung
Figure imgb0031
der Anspruch 3 und die Rotoidkurve RN ist definiert durch die Gleichung:
Figure imgb0032
5. Maschine nach Anspruch 1, dadurch gekennzeichnet, dass:
die Scheitel des Rotors QI' i = 1 bis N, N = 4, liegen auf einer Rotoidkurve RN und halten einen konstanten Abstand zum Schwerpunkt O des Rotors ein;
die Winkel QiÔQi+1 = 2/N und die Winkel Qii+1Qi+2 sind konstant;
die Kurve RN ist durch den Radius CQ 1 , der exzentrisch verläuft definiert,
die Achse Yo des Rotors ist parallel und nicht deckungsgleich zur Achse Yc.
6. Maschine nach einem oder mehreren Ansprüchen 1 bis 5, dadurch gekennzeichnet, dass:
der Rotor besteht aus N gleichen Zylindern E;
die Zylinder E haben eine kreisförmige Grundfläche mit dem Radius r= P i P i+1/2 = W/2.
7. Maschine nach einem oder mehreren Ansprüchen 1 bis 6, dadurch gekennzeichnet, dass:
die Segmente der N zylindrischen Enden des Scheitels des Rotors werden als Werkzeug genutzt, um die Umfangsfläche M der U-Bohrung des Stators zu schleifen.
EP85902631A 1984-06-22 1985-06-03 Rotationsmaschine Expired - Lifetime EP0187148B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT41597/84A IT1180993B (it) 1984-06-22 1984-06-22 Macchina volumetrica rotativa

Publications (2)

Publication Number Publication Date
EP0187148A1 EP0187148A1 (de) 1986-07-16
EP0187148B1 true EP0187148B1 (de) 1990-05-23

Family

ID=11251765

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85902631A Expired - Lifetime EP0187148B1 (de) 1984-06-22 1985-06-03 Rotationsmaschine

Country Status (6)

Country Link
EP (1) EP0187148B1 (de)
AT (1) ATE53098T1 (de)
AU (1) AU4436185A (de)
DE (1) DE3577900D1 (de)
IT (1) IT1180993B (de)
WO (1) WO1986000370A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1991760A1 (de) * 2005-12-01 2008-11-19 CONTIERO, Italo Drehflügel-verdrängermaschine

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7178502B2 (en) 2001-06-05 2007-02-20 Paul D. Okulov Balanced rotary internal combustion engine or cycling volume machine
US6899075B2 (en) * 2002-03-22 2005-05-31 Roxan Saint-Hilaire Quasiturbine (Qurbine) rotor with central annular support and ventilation
FR2936272B1 (fr) 2008-09-22 2012-07-13 Vincent Genissieux Machine rotative a losange deformable multifonctions
CA2851716C (en) 2011-10-14 2016-04-12 Gullivert Technologies Inc. Belt and support for a rotor mechanism in a rotary apparatus and rotary apparatus comprising same
FR3005106B1 (fr) 2013-04-25 2017-11-24 Jean Pierre Ambert Machine volumique rotative a trois pistons

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191026118A (en) * 1910-11-09 1911-01-12 Henry John Hudson Improvements in Rotary Internal Combustion Engines.
GB789375A (en) * 1953-04-29 1958-01-22 Henri Delmer A pump or engine of the oscillating-vane type
US3295505A (en) * 1963-05-31 1967-01-03 Jordan Alfred Rotary piston apparatus
FR1376285A (fr) * 1963-12-04 1964-10-23 Moteur volumétrique à combustion interne
DE1526408A1 (de) * 1965-06-09 1970-07-30 Politechnika Warszawska Verbrennungsmotor mit umlaufenden,eine geschlossene Kette bildenden,Kolben
ES416371A1 (es) * 1973-06-27 1976-05-16 Martin Artajo Maquina de embolos giratorios articulados.
FR2493397A1 (fr) * 1980-11-03 1982-05-07 Ambert Jean Pierre Moteur rotatif

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
I. Contiero, L. Beghi, "Class of algebraic curves passing through cyclic points" 16.03.85, p. 15 (published privately by I. Contiero and L. Beghi) *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1991760A1 (de) * 2005-12-01 2008-11-19 CONTIERO, Italo Drehflügel-verdrängermaschine

Also Published As

Publication number Publication date
IT1180993B (it) 1987-09-23
DE3577900D1 (de) 1990-06-28
IT8441597A1 (it) 1985-12-22
IT8441597A0 (it) 1984-06-22
WO1986000370A1 (en) 1986-01-16
AU4436185A (en) 1986-01-24
ATE53098T1 (de) 1990-06-15
EP0187148A1 (de) 1986-07-16

Similar Documents

Publication Publication Date Title
US5431551A (en) Rotary positive displacement device
US3560119A (en) Fluid pump or motor
US4300874A (en) Rotary machine with lenticular rotor and a circular guide member therefor
US3289654A (en) Rotary piston type internal combustion engine
US5171142A (en) Rotary displacement machine with cylindrical pretension on disc-shaped partition
US5391067A (en) Rotary fluid displacement device
HU210369B (en) Machine with rotating blades
US8047824B2 (en) Vane machine with stationary and rotating cylinder parts
US3799706A (en) Rotor assembly for a rotary machine
EP0187148B1 (de) Rotationsmaschine
US7488166B2 (en) Rotary volumetric machine
US4605361A (en) Oscillating vane rotary pump or motor
US5288217A (en) Cyclic volume machine
US4239466A (en) Rotary machine with adjustable means for its eccentric rotor
CA2162678A1 (en) Rotary vane mechanical power system
US3748068A (en) Rotary vane device
US3794450A (en) Rotary machine apex seal
US5071330A (en) Roller-vane hydraulic machine
US4370111A (en) Rotary pump or motor with drive rollers and free-floating rollers
US3349757A (en) Rotary positive displacement machine
US5429083A (en) Rotary internal combustion twin engine
US3989427A (en) Rotary fluid handling device
RU2082020C1 (ru) Роторная объемная гидропневмомашина
US4173439A (en) Apparatus having expanding and contracting chamber
CN1015483B (zh) 球形转子泵和球形转子机

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

17P Request for examination filed

Effective date: 19860326

17Q First examination report despatched

Effective date: 19870218

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Effective date: 19900523

Ref country code: BE

Effective date: 19900523

Ref country code: AT

Effective date: 19900523

REF Corresponds to:

Ref document number: 53098

Country of ref document: AT

Date of ref document: 19900615

Kind code of ref document: T

ITF It: translation for a ep patent filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 19900620

Year of fee payment: 6

REF Corresponds to:

Ref document number: 3577900

Country of ref document: DE

Date of ref document: 19900628

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19900630

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 19900630

Year of fee payment: 6

ET Fr: translation filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 19900803

Year of fee payment: 6

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Effective date: 19910604

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Effective date: 19910630

Ref country code: CH

Effective date: 19910630

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 19930625

Year of fee payment: 9

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Effective date: 19940603

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 19940603

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 19940620

Year of fee payment: 10

EUG Se: european patent has lapsed

Ref document number: 85902631.2

Effective date: 19920109

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 19940603

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Effective date: 19960229

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Effective date: 19960301

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST