• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    1530898 Rotary positive-displacement fluid-machines SVENSKA ROTOR MASKINER AB 21 Oct 1975 [29 Oct 1974] 46838/74 Heading F1F In an I.C. engine similar to that described in Specification 1392174 one or each of the main and abutment rotors 9, 10 has a system of liquidcoolant channels comprising an inlet pipe 18 coaxial with an outlet bore 16 and at least one bore 20 extending radially from the bore 16 into each lobe of the rotor and containing a co-axial pipe 22, which intersects the pipe 18, the interior of the pipe 22 and the bore 20 being inter-connected by slits 24. Owing to centrifugal action and differences in the densities of the liquid within the or each pipe 22 and that in the bore 20 caused by temperature differences the coolant is drawn through the pipes and returned through the bores. A pump (not shown) may be used to increase the flow-rate. Alternatively, the coolant may flow outwardly through the bore(s) 20 and return through bores (not shown) on either side of the or each bore 20, the pipe(s) 22 being dispensed with.
    公开号:SU786928A3
    申请号:SU752187146
    申请日:1975-10-29
    公开日:1980-12-07
    发明作者:Памлин Роланд
    申请人:Свенска Ротор Маскинер Актиеболаг (Фирма)；
    IPC主号:
    专利说明:

    I
    The invention relates to the design, and cooling systems of rotary internal combustion engines with interacting gear rotors.
    Known internal rotary engines5
    Combustion with two interacting gear rotors, equipped with a teeth cooling system, made with radial feed and return channels in each tooth, connected to axial inlet and outlet 10 pipelines placed in the rotor hub 11.
    A disadvantage of the known engine is the low efficiency of cooling of the rotor teeth.
    The purpose of the invention is to increase the cooling efficiency.
    This is achieved by the fact that the supply and return channels of the teeth are placed coaxially, and the supply and output pipes are 20 oooosno, and the supply channel is preferably formed by a tube located along the axis of the return channel. The external end of the tube, which forms the radial feed channel, is made with axial slits. In addition, radial 25
    feed and return channels can be located in a row along the longitudinal axis of the tooth.
    FIG. 1 shows the general kinematic scheme of the proposed engine; in fig. 2 Transverse section of one of the rotors along the radial channels of the cooling system; in fig. 3 is a longitudinal section of one of the rotors.
    The rotary internal combustion engine comprises a housing 1 with a working chamber formed by the intersection of two cylindrical cavities 2 and 3 and side flaps closed from the ends (not shown). In the working chamber, interacting gear rotors 4 and 5 are installed on two parallel shafts. Gas exchange channels are made in case 1 and a nozzle is installed to inject light fuel. A candle for igniting the nauseated mixture is placed in one of the rotors. Both rotors (or one of them, for example, rotor 5) are equipped with a teeth cooling system made with radial feed 6 and return 7 channels placed coaxially and connected with axial feed 8 and outlet 9 coaxial pipes placed in the rotor hub. Feed channel 6 is formed
    a tube 10 located along the axis of the return channel 7 and fixed in the rotor 5. The outer tube 10 is made with axial slots II, provided to allow cooling fluid to circulate in the system, cooling. With a large axial length of the rotor 5, the radial channels 6 and 7 can be located in a row along the longitudinal axis of the tooth (see Fig. 3) to equalize its temperature field.
    During engine operation, a cooling fluid, such as water or oil, is supplied from an external source (not shown) to the axial supply line 8 and through the holes in the walls of this line to feed the 6 rotor teeth to Canada 6. Pass the axial slots 11 of the tube 10, forming the supply channel 6, the cooling fluid through the return channel 7 is directed to the discharge line 9, and from there through the radiator of the cooling system (not shown) goes to an external source. During circulation, the cooling fluid takes heat from the outermost heated zones of the rotor teeth and heats up, causing the density of the fluid in return channel 7 to decrease in comparison with the density of the liquid in supply channel 6. And the centrifugal forces acting during rotation rotor to liquid in channels 6 and 7 will also become different, which leads to the appearance of an additional thermosyphon effect, which facilitates the circulation of coolant and its flow from channel 6 to channel 7. The indicated effect m provides a distribution of the coolant, in which most of the liquid
    enters the most heated parts of the rotor and intensively cools them, ensuring that the rotor is maintained at practically the same temperature in different parts of the rotor.
    权利要求:
    Claims (4)
    [1]
    1. A rotary internal combustion engine with two interacting gear rotors equipped with a teeth cooling system made with radial feed and return channels in each tooth associated with axial inlet and outlet
    pipelines located in the rotor hub, characterized in that, in order to increase the cooling efficiency, the feed and return channels of the teeth are placed coaxially, and the feed and discharge
    pipelines - coaxially.,
    [2]
    2. The engine according to claim 1, that is, that the supply channel is formed by a tube located along the axis of the return channel.
    [3]
    3. The engine for PP. 1 and 2, about tl and h a yusch and with the fact that the outer end of the tube,
    forming a radial feed channel, is made with axial slits.
    [4]
    4. The engine of PP. 1-3, characterized in that the radial feed
    and return channels are located in a row along the longitudinal axis of the tooth.
    Sources of information taken into account during the examination 1. French Patent No. 1507681, cl. F 02 B, 1967.
    类似技术:
    公开号 | 公开日 | 专利标题
    SU786928A3|1980-12-07|Internal combustion rotor engine
    SU1240366A3|1986-06-23|Driving unit,particularly for automobile
    US2783613A|1957-03-05|Cooling system employing fuel for cooling the blades of gas turbine engines
    US3385273A|1968-05-28|Cooling system for internal combustion engine
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    US2525804A|1950-10-17|Aircraft rotary boiler turbine air condenser power plant
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    US2098718A|1937-11-09|Supercharger mechanism for internal combustion engines
    US2849210A|1958-08-26|Turbine blade cooling system
    SE8700773D0|1987-02-24|VERMEVEXLARE
    US2631430A|1953-03-17|Gas turbine power plant having coaxially arranged combustors and regenerator
    SU704472A3|1979-12-15|Rotor-piston internal combustion engine
    US1475510A|1923-11-27|Cooling system for rotary internal-combustion engines
    US2641904A|1953-06-16|Apparatus for cooling combustion chambers of movable power plants with an oxidizing agent
    US3659562A|1972-05-02|Air cooling system for rotary internal combustion engine
    US2387485A|1945-10-23|Heat exchange unit for radial type engines
    US1741957A|1929-12-31|Cooling device for the reversing stator blades of turbines
    RU2182237C2|2002-05-10|Liquid cooling jacket of internal combustion engine cylinder block
    US1986556A|1935-01-01|Rotary internal combustion engine
    US1723515A|1929-08-06|Combustion turbine
    SU909236A1|1982-02-28|I.c. engine cooling system
    US2873087A|1959-02-10|Means for cooling gas turbines
    SU868072A1|1981-09-30|I.c. engine cylinder
    SU553438A1|1977-04-05|Heat transfer device
    同族专利:
    公开号 | 公开日
    JPS5166915A|1976-06-10|
    DE2547592A1|1976-05-06|
    FI753004A|1976-04-30|
    AU8608175A|1977-05-05|
    GB1530898A|1978-11-01|
    US4005955A|1977-02-01|
    SE7511711L|1976-04-30|
    IT1043698B|1980-02-29|
    FR2289732A1|1976-05-28|
    SE414659B|1980-08-11|
    BR7507035A|1976-08-17|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US1098440A|1913-06-09|1914-06-02|P H & F M Roots Company|Rotary blower.|
    FR524897A|1917-10-03|1921-09-12|Edmond Berthelon|Device for improvements made to pistons operating in pumps or rotary motors|
    GB893938A|1958-10-02|1962-04-18|Nsu Mohorenwerke Ag|Improvements in or relating to rotary engines|
    GB1172828A|1965-12-06|1969-12-03|Svenska Rotor Maskiner Ab|Improvements in and relating to Rotary Positive-Displacement Internal Combustion Engines.|
    US3472210A|1967-09-29|1969-10-14|Hilbert J Savoie Jr|Synchronized counterrotary engine|
    US3531227A|1968-07-05|1970-09-29|Cornell Aeronautical Labor Inc|Gear compressors and expanders|EP0062087A1|1981-04-08|1982-10-13|Gerhard Rödiger|Rotary-piston machine with periodically variable rotating speed|
    CH669974A5|1985-10-08|1989-04-28|Wankel Felix|
    DE3545818C2|1985-12-23|1989-10-19|Wankel Gmbh, 1000 Berlin, De|
    KR100510939B1|2000-07-21|2005-08-30|김경환|Rotary engine|
    US6539913B1|2002-01-14|2003-04-01|William P. Gardiner|Rotary internal combustion engine|
    US6988482B2|2003-11-26|2006-01-24|Neal Lockett|Dual rotor internal combustion engine|
    CN100400820C|2006-01-27|2008-07-09|赵耀芝|Concavo-convex gear type rotor engine|
    US7993118B2|2007-06-26|2011-08-09|GM Global Technology Operations LLC|Liquid-cooled rotor assembly for a supercharger|
    GB2508141A|2012-11-21|2014-05-28|Gilo Ind Res Ltd|Closed-loop cooling system of a rotary engine|
    US9291095B2|2013-03-15|2016-03-22|Randy Koch|Rotary internal combustion engine|
    US9683569B2|2015-08-27|2017-06-20|Ingersoll-Rand Company|Compressor system having rotor with distributed coolant conduits and method|
    US10495090B2|2015-08-27|2019-12-03|Ingersoll-Rand Company|Rotor for a compressor system having internal coolant manifold|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    GB46838/74A|GB1530898A|1974-10-29|1974-10-29|Rotary positive-displacement internal-combustion engine|
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