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YU29284A - DEVICE POWERED BY ENGINE EXHAUST GASES SUS - Google Patents

DEVICE POWERED BY ENGINE EXHAUST GASES SUS

Info

Publication number
YU29284A
YU29284A YU29284A YU29284A YU29284A YU 29284 A YU29284 A YU 29284A YU 29284 A YU29284 A YU 29284A YU 29284 A YU29284 A YU 29284A YU 29284 A YU29284 A YU 29284A
Authority
YU
Yugoslavia
Prior art keywords
rotor
hub
inlet
shaft
sus
Prior art date
Application number
YU29284A
Other languages
Serbo-Croatian (sh)
Inventor
T. Stojičić
Original Assignee
Stojičić, Tode
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 Stojičić, Tode filed Critical Stojičić, Tode
Priority to YU29284A priority Critical patent/YU29284A/en
Priority to DE19853503829 priority patent/DE3503829A1/en
Priority to FR858502175A priority patent/FR2559839B1/en
Priority to GB08508433A priority patent/GB2173260A/en
Publication of YU29284A publication Critical patent/YU29284A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G5/00—Profiting from waste heat of combustion engines, not otherwise provided for
    • 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
    • F01D1/32—Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
    • 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
    • F02B77/00—Component parts, details or accessories, not otherwise provided for
    • F02B77/11—Thermal or acoustic insulation
    • 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
    • F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Supercharger (AREA)

Abstract

Uredjaj pogonjen izduvnim gasovima motora SUS prema pronalasku, sadrži rotor (5) koji ima na levom radijalnom zidu ulaznu glavčinu (5a) sa velikim aksijalnim ulaznim otvorom, a na desnom radijalnom zidu uobičajenu glavčinu (5b) preko koje je rotor učvršćen na levom kraju vratila (19). Na perifernom zidu rotora učvršćene su radijalno uvodne komore (24), čiji su veći ulazni otvori usmereni radijalno u šupljinu rotora, dok su u njihovim manjim izlaznim otvorima postavljeno de Laval-ove mlaznice (25) koje omogućavaju nadzvučno isticanje mlazeva i time obrazovanje reaktivnog obrtnog momenta. Rotor (5) i njegovo vratilo (19) postavljeni su koaksijalno u kućištu (6), na čijem levom radijalnom zidu je pričvršćen poklopac (2) sa koaksijalnom glavčinom (2a) koja obuhvata ulaznu glavčinu (5a) rotora i za koju je spojen sa bočne strane širi kraj ulazne cevi (1), dok je njen uži kraj spojen sa izduvnom cevi motora SUS. Na desnom radijalnom zidu kućišta (6) izvedena je koaksijalno dugačka glavčina (6a) sa aksijalnim otvorom u kome je preko para ležišta (18) oslonjen srednji deo vratila (19). Na perifernom zidu kućišta (6) postavljena je tangencijalno izlazna cev (26) za odvodjenje gasova. Na desnom kraju vratila (19) učvršćena je remenica (13) za prenos reaktivnog obrtnog momenta.The SUS engine exhaust device according to the invention comprises a rotor (5) having an inlet hub (5a) on the left radial wall with a large axial inlet and a conventional hub (5b) on the right radial wall over which the rotor is fixed at the left end of the shaft. (19). Radial inlet chambers (24) are fixed on the peripheral wall of the rotor, whose larger inlets are directed radially into the rotor cavity, while de Laval nozzles (25) are placed in their smaller outlets, which enable supersonic jet discharge and thus the formation of a reactive rotary. moment. The rotor (5) and its shaft (19) are placed coaxially in the housing (6), on the left radial wall of which is attached a cover (2) with a coaxial hub (2a) which includes the inlet hub (5a) of the rotor and to which it is connected to the side extends the end of the inlet pipe (1), while its narrower end is connected to the exhaust pipe of the SUS engine. A coaxially long hub (6a) with an axial opening is made on the right radial wall of the housing (6), in which the middle part of the shaft (19) is supported over a pair of bearings (18). A tangential outlet pipe (26) for gas drainage is placed on the peripheral wall of the housing (6). A pulley (13) for transmitting reactive torque is fixed at the right end of the shaft (19).

YU29284A 1984-02-17 1984-02-17 DEVICE POWERED BY ENGINE EXHAUST GASES SUS YU29284A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
YU29284A YU29284A (en) 1984-02-17 1984-02-17 DEVICE POWERED BY ENGINE EXHAUST GASES SUS
DE19853503829 DE3503829A1 (en) 1984-02-17 1985-02-05 EXHAUST GAS EXHAUST GAS FROM COMBUSTION ENGINES
FR858502175A FR2559839B1 (en) 1984-02-17 1985-02-15 ROTARY REGULATOR FOR EXHAUST GASES OF INTERNAL COMBUSTION ENGINES
GB08508433A GB2173260A (en) 1984-02-17 1985-04-01 A radial flow turbine for utilizing energy in exhaust gases from an engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
YU29284A YU29284A (en) 1984-02-17 1984-02-17 DEVICE POWERED BY ENGINE EXHAUST GASES SUS

Publications (1)

Publication Number Publication Date
YU29284A true YU29284A (en) 1992-09-07

Family

ID=25549242

Family Applications (1)

Application Number Title Priority Date Filing Date
YU29284A YU29284A (en) 1984-02-17 1984-02-17 DEVICE POWERED BY ENGINE EXHAUST GASES SUS

Country Status (4)

Country Link
DE (1) DE3503829A1 (en)
FR (1) FR2559839B1 (en)
GB (1) GB2173260A (en)
YU (1) YU29284A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
YU23586A (en) * 1986-02-17 1990-04-30 Tode Stojicic Circulation expander of lost energy of heat machines
US7722313B1 (en) 2006-12-12 2010-05-25 Di Iorio Crescencio Device for converting kinetic energy contained in a fluid, into mechanical energy
GB2491536B (en) * 2010-03-05 2016-07-27 Di Iorio Crescencio Variable-speed tube turbine
RU2667847C1 (en) * 2017-04-24 2018-09-24 Алексей Маратович Рогульченко Combined wankel engine with jet effect

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH9045A (en) * 1894-07-24 1895-02-28 Salaud Jean Marie Device for utilizing the exhaust gases or vapors from engines
US2245163A (en) * 1939-04-07 1941-06-10 Gen Electric Power plant for aircraft
CH210266A (en) * 1939-06-13 1940-06-30 Oerlikon Maschf Temperature protection device for rotating heat engines.
GB683138A (en) * 1948-10-25 1952-11-26 Weser Ag Piston engine with exhaust steam turbine
GB820096A (en) * 1956-08-11 1959-09-16 Daimler Benz Ag New or improved method and means for the operation of a piston internal combustion engine installation comprising an exhaust gas turbine
GB856788A (en) * 1958-01-18 1960-12-21 Daimler Benz Ag Improvements relating to supercharged internal combustion engine installations
GB895166A (en) * 1958-08-25 1962-05-02 Peter Laws Improvements in expansion turbines
GB1013351A (en) * 1963-10-24 1965-12-15 Westwind Developments Ltd Improvements in or relating to air driven turbines
US3707336A (en) * 1970-11-27 1972-12-26 Hollymatic Corp Fluid engine
CA996862A (en) * 1973-04-23 1976-09-14 James V. Theis (Jr.) Fluid engine
US3930744A (en) * 1973-10-10 1976-01-06 Hollymatic Corporation Pressure gas engine
GB1521265A (en) * 1975-10-06 1978-08-16 Penny Turbines Ltd Noel Exhaust gas power extractor for internal combustion engin
DE2607600A1 (en) * 1976-02-25 1977-09-01 Georg Sontheimer Turbine rotor disc with axial apertures - has tangential nozzles causing rotation by reaction when pressurised fluid passes through apertures

Also Published As

Publication number Publication date
FR2559839B1 (en) 1991-10-25
FR2559839A1 (en) 1985-08-23
GB2173260A (en) 1986-10-08
DE3503829A1 (en) 1985-08-29
GB8508433D0 (en) 1985-05-09

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