GB936283A - A device with rotating pistons, suitable for functioning as a motor, pump, movement or torque repeater - Google Patents

A device with rotating pistons, suitable for functioning as a motor, pump, movement or torque repeater

Info

Publication number
GB936283A
GB936283A GB15861/61A GB1586161A GB936283A GB 936283 A GB936283 A GB 936283A GB 15861/61 A GB15861/61 A GB 15861/61A GB 1586161 A GB1586161 A GB 1586161A GB 936283 A GB936283 A GB 936283A
Authority
GB
United Kingdom
Prior art keywords
cavities
semi
iii
annular
pistons
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
GB15861/61A
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.)
ANZUG VERSUCH ANSTALT
Original Assignee
ANZUG VERSUCH ANSTALT
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 ANZUG VERSUCH ANSTALT filed Critical ANZUG VERSUCH ANSTALT
Publication of GB936283A publication Critical patent/GB936283A/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
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2730/00Internal-combustion engines with pistons rotating or oscillating with relation to the housing
    • F02B2730/01Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Reciprocating Pumps (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Abstract

936,283. Rotary piston machines. ANZUG VERSUCH-ANSTALT. May 2, 1961 [May 4, 1960], No. 15861/61. Class 110 (2). A rotary I.C. engine, pump, motor, compressor, movement or torque repeater, comprises annular cavities at right-angles or otherwise inclined to each other and intersecting at two places, each cavity having openings for the passage of fluid and housing at least one piston carried by a rotating annular member and mechanism linking the annular members such that the pistons in passing through the cavities do not foul each other at the crossing points. As shown in Fig. 1, annular cavities 1, 2 house pistons 5, 6 respectively extending approximately through 180-degree arcs. The piston 5 is secured on its outer periphery to a ring 3 carrying an annular bevel gear 7 in mesh with a bevel wheel 11 keyed on a shaft 13. The shaft 13 has keyed thereto a second bevel wheel 12 in mesh with an annular bevel gear 8 carried by a ring 4 secured to the inner periphery of the piston 6 so that synchronous movement of the pistons takes place. Fixed walls 9, 10, broken at the intersection points I, I<SP>1</SP>, Fig. 2, on the outer periphery of the cavity 2 and the inner periphery of the cavity 1 respectively together with the continuous rings 3, 4, seal the cavities. In one embodiment, operating as a four-stroke I.C. engine, gaseous mixture is supplied to semi-cavities II, III, Fig. 6, through an inlet duct 19 having a valved branch 20, and to semi-cavities I, IV, through an inlet duct 21 having a valved branch 22 and spent gases exhausted from the semi-cavities II, III, through an outlet duct 23 having valved branches 24 and from the semi-cavities I, IV, through an outlet duct 25 having valved branches 26. Transfer chambers 27, 28 fitted with non-return valves interconnect semicavities III, IV and transfer chambers 29, 30 also fitted with non-return valves interconnect semi-chambers I, II. At the commencement of the cycle, Fig. 6, gaseous mixture is sucked into the semi-cavities I, II and compressed in the semi-cavities III, IV. As the pistons rotate and cross the intersection points, the compressed gaseous mixture is transferred through the chambers 27, 28 from the semicavities III, IV, suitably ignited and expanded into the semi-cavities IV, III to do useful work. At this stage the gaseous mixture in semicavities I, II is being compressed to later be ignited and transferred through chambers 29, 30 to semi-cavities II, I. The semi-cavities III, IV then being open to exhaust. On further rotation of the pistons, spent gases are exhausted from semi-cavities I, II and gaseous mixture sucked into semi-cavities III, IV to complete the cycle. Another four-stroke I.C. engine cycle is illustrated in which inlet ducts 35, 36, Fig. 14, are connected to the semicavities II, IV and outlet ducts 33, 34 to the semi-cavities III, I. There then being only two transfer chambers 28, 29. The invention can also be applied to a two-stroke I.C. engine and to a constant pressure engine in which fuelmixture or explosive-mixture is injected into the expanding semi-cavities. Alternatively, liquid or steam may be injected under pressure into these semi-cavities. In operating as a rotary pump or compressor fluid is sucked into the expanding semi-cavities and discharged from the contracting semi-cavities. It can also be used as a movement or torque repeater with phases similar to those of a two-stroke I.C. engine. Modifications are described with different arrangements of gearing synchronously interconnecting the pistons. In one arrangement, annular cavities disposed at an angle other than a right-angle are described. In another arrangement, is shown and described, three non-concentric annular cavities having their centres on a common axis. Two devices according to the invention may be coupled together concentrically or two or more devices coupled together in side-by-side relationship.
GB15861/61A 1960-05-04 1961-05-02 A device with rotating pistons, suitable for functioning as a motor, pump, movement or torque repeater Expired GB936283A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT793360 1960-05-04

Publications (1)

Publication Number Publication Date
GB936283A true GB936283A (en) 1963-09-11

Family

ID=11125543

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15861/61A Expired GB936283A (en) 1960-05-04 1961-05-02 A device with rotating pistons, suitable for functioning as a motor, pump, movement or torque repeater

Country Status (3)

Country Link
BE (1) BE603364A (en)
ES (1) ES267102A1 (en)
GB (1) GB936283A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3809022A (en) * 1972-11-15 1974-05-07 J Dean Rotary power translation machine
WO1991002145A1 (en) * 1989-08-11 1991-02-21 Mechanology Toroidal hyper-expansion rotary engine, compressor, expander, pump and method
US5233954A (en) * 1989-08-11 1993-08-10 Mechanology Toroidal hyper-expansion rotary engine, compressor, expander, pump and method
RU2612873C1 (en) * 2016-04-06 2017-03-13 Аскер Аскерович Гейдаров Rotary internal combustion engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3809022A (en) * 1972-11-15 1974-05-07 J Dean Rotary power translation machine
WO1991002145A1 (en) * 1989-08-11 1991-02-21 Mechanology Toroidal hyper-expansion rotary engine, compressor, expander, pump and method
US5233954A (en) * 1989-08-11 1993-08-10 Mechanology Toroidal hyper-expansion rotary engine, compressor, expander, pump and method
RU2612873C1 (en) * 2016-04-06 2017-03-13 Аскер Аскерович Гейдаров Rotary internal combustion engine
JP2017187015A (en) * 2016-04-06 2017-10-12 ゲイダロフ・アスケル・アスケロヴィッチ Rotary internal combustion engine
US9803542B1 (en) 2016-04-06 2017-10-31 Asker Askerovich Geidarov Rotary internal combustion engine

Also Published As

Publication number Publication date
ES267102A1 (en) 1961-11-01
BE603364A (en) 1961-09-01

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