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WO2010081469A3 - Rotary force machine having three rotating displacement bodies with entry pressure flaps and a controller of the inlet openings into the combustion pipe - Google Patents

Rotary force machine having three rotating displacement bodies with entry pressure flaps and a controller of the inlet openings into the combustion pipe Download PDF

Info

Publication number
WO2010081469A3
WO2010081469A3 PCT/DE2010/000030 DE2010000030W WO2010081469A3 WO 2010081469 A3 WO2010081469 A3 WO 2010081469A3 DE 2010000030 W DE2010000030 W DE 2010000030W WO 2010081469 A3 WO2010081469 A3 WO 2010081469A3
Authority
WO
WIPO (PCT)
Prior art keywords
primary rotor
stage
secondary rotors
combustion chamber
controller
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.)
Ceased
Application number
PCT/DE2010/000030
Other languages
German (de)
French (fr)
Other versions
WO2010081469A2 (en
Inventor
Oleg Tchebunin
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
Priority to DE112010000152T priority Critical patent/DE112010000152A5/en
Publication of WO2010081469A2 publication Critical patent/WO2010081469A2/en
Anticipated expiration legal-status Critical
Publication of WO2010081469A3 publication Critical patent/WO2010081469A3/en
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/08—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
    • F01C1/12—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type
    • F01C1/123—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with tooth-like elements, extending generally radially from the rotor body cooperating with recesses in the other rotor, e.g. one tooth
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/08—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
    • F01C1/12—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type
    • F01C1/14—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F01C1/20—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with dissimilar tooth forms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C19/00—Sealing arrangements in rotary-piston machines or engines
    • F01C19/02—Radially-movable sealings for working fluids
    • F01C19/025—Radial sealing elements specially adapted for intermeshing engagement type machines or engines, e.g. gear machines or engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

The invention relates to a rotary piston machine, comprising a compressor stage (5), an expansion stage (7), a combustion chamber (21), and a synchronization transmission (2), wherein the compression stage (5) and the expansion stage (7) have a substantially identical design and each have a primary rotor (11) and three secondary rotors (4), wherein the secondary rotors (4) each are made of a cylindrical body having a displacement comb (12) with sealing strips (13), wherein the displacement combs (12) of the secondary rotors (4) engage in three profiled longitudinal depressions (23) of the primary rotor (11), and the ratio of the diameters between the secondary rotors (4) and primary rotor (11) as well as the transmission ratio of the synchronization transmission (2) and consequently the rotational speed of the secondary rotors (4) relative to the primary rotor (11) are 1:3, wherein the combustion chamber (21) extends over the compressor stage (5) and over the expansion stage (7) and is arranged on the inside of the primary rotor (11), wherein the combustion chamber (21) is provided with an inlet pipe, which is fixed on a housing, for feeding fuel and air and with a combustion pipe (19) having inlet and outlet openings (25, 26), wherein an entry pressure flap (41) is provided on the compressor stage (5) and a controller of the inlet opening (17) is provided in the combustion pipe and the expansion stage (7), wherein the free inside spaces (42) of the primary rotor (11) are provided as compressed air accumulators and distributors for cooling the primary rotor in both stages before the gas entry into the combustion chamber (21).
PCT/DE2010/000030 2009-01-19 2010-01-19 Rotary force machine having three rotating displacement bodies with entry pressure flaps and a controller of the inlet openings into the combustion pipe Ceased WO2010081469A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE112010000152T DE112010000152A5 (en) 2009-01-19 2010-01-19 TURNING MACHINE WITH THREE ROTATING DISPLACERS WITH INLET PRESSURE VALVES AND A CONTROL OF THE INTAKE OPENINGS IN THE TUBE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102009005107.4 2009-01-19
DE200910005107 DE102009005107B3 (en) 2009-01-19 2009-01-19 Rotary machine with three rotating displacers with inlet pressure flaps and a control of the inlet openings in the combustion tube

Publications (2)

Publication Number Publication Date
WO2010081469A2 WO2010081469A2 (en) 2010-07-22
WO2010081469A3 true WO2010081469A3 (en) 2012-01-19

Family

ID=42340134

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2010/000030 Ceased WO2010081469A2 (en) 2009-01-19 2010-01-19 Rotary force machine having three rotating displacement bodies with entry pressure flaps and a controller of the inlet openings into the combustion pipe

Country Status (2)

Country Link
DE (2) DE102009005107B3 (en)
WO (1) WO2010081469A2 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010006487B4 (en) 2010-02-02 2012-03-01 Oleg Tchebunin Rotary engine with three rotating displacers, with additional pre-expansion stage, retractable sealing strips and external toothing all rotors
DE102010020681B4 (en) 2010-05-15 2024-03-21 Oleg Tchebunin Screw engine with four secondary rotors, a compressor stage controlled by working pressure and a combustion chamber optimally controlled by feedback to the exhaust chamber
RU2477377C2 (en) * 2011-06-16 2013-03-10 Игорь Юрьевич Исаев Internal combustion engine: five-stroke rotary engine with one central rotary gate shared by separate working medium compression and expansion sections, and isolated invariable-volume combustion chambers
DE102012011068B4 (en) 2012-06-02 2015-09-10 Oleg Tchebunin Rotary piston engine with three rotating displacers, a control of the compression chamber, a control of the expansion chamber and with facilities for the realization of the gas-steam cycle.
DE102013016274B4 (en) * 2013-09-28 2015-11-26 Oleg Tchebunin Three-stage rotary engine with continuous combustion process
ES2666423T3 (en) * 2015-12-21 2018-05-04 Fuelsave Gmbh Cogeneration plant and procedure to operate a cogeneration plant
DE102017108543B4 (en) 2016-04-23 2022-04-28 Oleg Tchebunin Vertical take-off aircraft, the propulsion of which has rotary piston engines with a continuous combustion process and thrust direction pivoting systems
DE102017009911B4 (en) 2017-10-24 2020-07-09 Oleg Tchebunin Method for multiplying the power of an engine and power plant with an engine
EP3527781A1 (en) 2018-02-14 2019-08-21 Fuelsave GmbH Rotary piston engine and method for operating a rotary piston engine
DE102021001227A1 (en) 2020-03-10 2021-10-14 Oleg Tchebunin Airplanes with different designs, engines and types of VTOL / STOL platforms
RU199412U1 (en) * 2020-04-13 2020-08-31 Николай Сергеевич Лапшин ROTARY FOUR-STROKE INTERNAL COMBUSTION ENGINE "ROLAN"
DE102024109684A1 (en) 2023-04-19 2024-10-24 Oleg Tchebunin Contemporary Stirling engine based on a drive with a continuous working process

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR676625A (en) * 1928-07-16 1930-02-25 Warren Engine Company Improvements to rotary steam engines
US3203406A (en) * 1960-11-28 1965-08-31 Dettwiler Georges Rotary engine
DE102006038957B3 (en) * 2006-08-18 2008-01-03 Oleg Tchebunin Three rotary displacer rotary engine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2009732A1 (en) * 1970-03-03 1971-09-16 TeIe Alarm Hofmann & Simon, 8501 Behnn gersdorf Rotary piston internal combustion engine
DE19711084A1 (en) * 1997-03-18 1998-09-24 Jochen Dr Ahrendt Rotary piston machine, e.g. engine or pump
DE202006008158U1 (en) * 2006-05-22 2006-11-09 Tchebunin, Oleg Propeller-power machine e.g. gas turbine, for airplane`s drive system, has combustion chamber placed between compressor and pressure reducer stages having propeller plant with main and adjacent rotors having circular arcs and epicycloids

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR676625A (en) * 1928-07-16 1930-02-25 Warren Engine Company Improvements to rotary steam engines
US3203406A (en) * 1960-11-28 1965-08-31 Dettwiler Georges Rotary engine
DE102006038957B3 (en) * 2006-08-18 2008-01-03 Oleg Tchebunin Three rotary displacer rotary engine

Also Published As

Publication number Publication date
WO2010081469A2 (en) 2010-07-22
DE102009005107B3 (en) 2010-09-23
DE112010000152A5 (en) 2012-05-24

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