• 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:
    The exhaust pipe has an axial compensator to compensate for changes in length in the elongated part as well as a pair of props which compensate for changes in length in the bent parts. The props are each articulated to a fixed support point and to the axially elongated part of the pipe. In addition, the props are disposed in different planes relative to each other.
    公开号:SU862838A3
    申请号:SU772546391
    申请日:1977-11-14
    公开日:1981-09-07
    发明作者:Гегеле Герд
    申请人:Гебрюдер Зульцер, Аг (Фирма)；
    IPC主号:
    专利说明:

    (54) EXHAUST MANIFOLD
      T, -. . The invention relates to a structure ejector, in particular, to the design of exhaust systems of a reciprocating internal combustion engine. The devices of the exhaust manifolds of the piston engine in the internal combustion are known, which contain a section with an axial compensator, a curved section and a rotary bearing rod located between the collector and deiigate. Lem 1. The device provides a collector to the engine. The disadvantage of such devices is their low reliability; it is impossible to ensure movement in several directions due to thermal stresses. 11eL of the invention is to increase, reliability and service life. This is achieved by the fact that the collector is provided with an additional leg connected to the support one, with both ti free ends hinged to the engine and connected to the collector connected ones. T-gs are connected by bearing points on the engine and the collector using ball bearings. In FIG. 1 shows an exhaust manifold, a general view of g in FIG. 2 - the same cross section. Collector 1 contains elements 2 and 3 curved at right angles. mounted on a piston engine of internal combustion by means of flanges 4 and 5, a gas exhaust duct 6, a compensator 7, pieces of pipes 8 and 9, interconnected by means of a tubular coupling 10. Both pieces of pipe are fitted with flanges 11 and 12, and the flange 11 has a radial extension 13-. The exhaust manifold 1 is equipped with a support thrust 14 and an additional thrust 15: extending between the radial extension 13 and the piston engine of the internal combustion, shown in the figures by two hard points 16 and 17. At the same time, the radial continuation 13 is equipped with two forks 18 and 19, B 14 and 15 are fixed by means of ball bearings 20 and 21. The ends 14 and 15 are fixed by their ends by means of ball bearings 22 and 23 in forks 24; and 25. When the engine is running, the ha 15 is positioned relative to the fork 18 in such a way that support T ha 14 when the room temperature is tilted in a counterclockwise direction under Glom ci. This arrangement allows
    权利要求:
    Claims (2)
    [1]
    Claim
    1. The exhaust manifold of a reciprocating internal combustion engine, comprising a section with an axial compensator, a curved section and a rotary support rod located between the collector and the engine, characterized in that, in order to increase reliability and service life, the collector is equipped with an additional rod connected to the reference, moreover, both rods with free ends are pivotally attached to the engine, and connected to the collector.
    [2]
    2. Collector pop. 1, characterized in that the rods are connected to the reference points on the engine and manifold using ball bearings.
    类似技术:
    公开号 | 公开日 | 专利标题
    SU862838A3|1981-09-07|Exhaust collector
    CA2617719A1|2007-02-15|Radially expanding turbine engine exhaust cylinder interface
    US4090358A|1978-05-23|Heat exchanger support system
    US2414788A|1947-01-28|Turbine construction
    GB2258500A|1993-02-10|Supporting recuperative heat exchanger on gas turbine engine.
    SU814286A3|1981-03-15|Exaust collector
    FR2356000A1|1978-01-20|TURBOMACHINE COMBUSTION CHAMBER SUPPORT DEVICE
    US4696224A|1987-09-29|Piston for internal combustion engine
    US3327552A|1967-06-27|Temperature compensated linkage
    US3130592A|1964-04-28|Motion converting means
    US5183223A|1993-02-02|Interlocking ring fan jet engine support system
    US3735587A|1973-05-29|Engine exhaust turbine inlet screen
    US2458635A|1949-01-11|Expansion joint for exhaust structures
    US2345540A|1944-03-28|Turbine system
    US3426974A|1969-02-11|Variable area nozzle synchronous hinge
    CN108708789A|2018-10-26|Gas turbine support construction
    GB1136698A|1968-12-11|A pipe joint
    SU465484A1|1975-03-30|Exhaust manifold for internal combustion engine
    JPS59211718A|1984-11-30|Exhaust system of engine with turbo-supercharger
    SU419147A1|1976-09-05|Turbocharger
    SU352573A1|1983-06-23|Annular combustion chamber of gas turbine engine
    JPS55103112A|1980-08-07|Structure of crankshaft for engine
    DK60094A|1995-11-28|Large self-contained internal combustion engine
    KR100198121B1|1999-06-15|The supporting structure of turbo-charger for an automobile
    RU13816U1|2000-05-27|STEAM TURBINE INSTALLATION
    同族专利:
    公开号 | 公开日
    NL7710879A|1978-07-04|
    US4192142A|1980-03-11|
    JPS5637405B2|1981-08-31|
    CH615247A5|1980-01-15|
    NO774505L|1978-07-03|
    GB1539873A|1979-02-07|
    IT1088373B|1985-06-10|
    FI65649B|1984-02-29|
    DK145764B|1983-02-21|
    JPS5385219A|1978-07-27|
    FR2376293B1|1983-05-20|
    ATA19377A|1978-10-15|
    DK564077A|1978-07-01|
    FR2376293A1|1978-07-28|
    DE2700565A1|1978-07-06|
    AT350332B|1979-05-25|
    FI65649C|1984-06-11|
    DK145764C|1983-08-15|
    FI773223A|1978-07-01|
    SE7713707L|1978-07-01|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    RU2646166C1|2014-07-24|2018-03-01|Сканиа Св Аб|Pipe assembly for the gaseous media pipeline|US2439067A|1943-03-27|1948-04-06|Gen Spring Corp|Support device|
    US2372214A|1943-09-30|1945-03-27|Grinnell Corp|Sway brace|
    US2608819A|1946-09-27|1952-09-02|Boeing Co|Collector ring mount|
    US2533370A|1948-03-29|1950-12-12|Thaddeus L E Haug|Pipe support|
    US2688501A|1950-08-21|1954-09-07|Trans Canada Air Lines|Exhaust manifold joint|
    US3380246A|1966-01-03|1968-04-30|Gen Electric|Exhaust manifold system for internal combustion engines|
    JPS5018817U|1973-06-18|1975-03-03|DE3803320C2|1988-02-04|1992-02-13|Martin 8000 Muenchen De Wimmer|
    FR2631383A1|1988-02-19|1989-11-17|Giraudo Jean Claude|Motorcycle ŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸŸ engine which can swing - incorporates silencer attached by links to hold it horizontal|
    KR950001462B1|1991-03-25|1995-02-24|마쓰다 가부시끼가이샤|Exhaust system for engine|
    US5316346A|1992-04-10|1994-05-31|General Electric Company|Anti-rotation bracket for a flanged connection spaced from fixed structure|
    DE4229467A1|1992-09-03|1994-03-10|Mtu Friedrichshafen Gmbh|Storage device for the exhaust manifold of an internal combustion engine|
    CH691459A5|1996-05-13|2001-07-31|Scambia Ind Dev Ag|Exhaust system for a motor vehicle and motor vehicle.|
    US6267327B1|1999-04-02|2001-07-31|Allison Advanced Development Company|Coupling system for connecting a gas turbine engine to an aircraft mounted exhaust system|
    JP4207790B2|2004-02-02|2009-01-14|トヨタ自動車株式会社|Lower body structure|
    US7478700B2|2006-01-24|2009-01-20|Paccar Inc|Retention linkage for vehicle exhaust systems|
    CN103672176B|2013-12-17|2016-01-27|芜湖通和汽车管路系统股份有限公司|A kind of pipeline fixing fastener platform|
    US9216645B1|2014-07-22|2015-12-22|International Truck Intellectual Property Company, Llc|Cab-mounted exhaust pipe de-coupler|
    US10156171B2|2015-08-07|2018-12-18|Cummins Emission Solutions Inc.|Mounting aftertreatment systems from service joints|
    USD891605S1|2017-05-05|2020-07-28|David Bacon|Flare stack|
    CN109291786B|2018-09-26|2021-06-29|安徽安凯汽车股份有限公司|A connect protective structure for vehicle chassis exhaust duct|
    CN110067629B|2019-06-10|2020-06-23|中车大连机车车辆有限公司|Exhaust pipe assembly, compensating bracket and design method|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    CH1646076A|CH615247A5|1976-12-30|1976-12-30|
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