CN103541773A - 一种丝状涡轮 - Google Patents

一种丝状涡轮 Download PDF

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Publication number
CN103541773A
CN103541773A CN201210241691.5A CN201210241691A CN103541773A CN 103541773 A CN103541773 A CN 103541773A CN 201210241691 A CN201210241691 A CN 201210241691A CN 103541773 A CN103541773 A CN 103541773A
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filiform
rotor
blades
turbine
thread
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CN103541773B (zh
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时剑
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Priority to CN201210241691.5A priority Critical patent/CN103541773B/zh
Priority to PCT/CN2013/077216 priority patent/WO2014008800A1/zh
Priority to US14/413,363 priority patent/US9260967B2/en
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    • 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
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F01D1/36—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes using fluid friction
    • 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
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2210/00—Working fluids
    • F05D2210/10—Kind or type
    • F05D2210/12—Kind or type gaseous, i.e. compressible

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

一种丝状涡轮，包括喷嘴，壳体和转子，所述转子叶片为丝状，丝状叶片可以相互平行呈多层鸟笼状，也可纵横交错呈三维网状。转子轴中空并开有排气孔。这种丝状涡轮用丝状叶片取代传统特斯拉涡轮的薄圆盘，由于丝状叶片固定在两个厚圆盘上，所以比薄圆盘刚度好，不易变形，使转子可以做得直径更大而不易变形。丝状叶片形成的丝网结构还可对喷嘴气流具有一定的消音效果，降低机器噪音。

Description

一种丝状涡轮
所属技术领域
本发明涉及一种丝状涡轮，属汽轮机技术领域。
背景技术
特斯拉涡轮又称无叶涡轮，其形状是一根轴上按一定间距固定有多个光滑且薄的圆盘，气流从切线方向冲击这些圆盘，利用边界层效应带动这些圆盘和轴一起转动。该涡轮虽然具有结构简单、体积紧凑、效率高、成本低等优点，但因为圆盘尺寸大时刚度不够易变形，导致盘间涡流挠动大，振动大等缺点而未能普及应用。
发明内容
为克服现有技术的不足，本发明提供一种丝状涡轮，该丝状涡轮包括喷嘴，壳体和转子，所述转子叶片为丝状，一般为金属丝，丝状叶片固定于两个圆盘之间，丝状叶片可以相互平行呈多层鸟笼状，也可纵横交错呈三维网状。转子轴中空并开有排气孔。喷嘴沿切线方向向转子喷气，气流会在壳体内侧的导向作用下形成涡流，由于布满转子的丝状叶片大大增加了转子与气流的接触面，根据边界层效应，转子将被气流带动一起旋转，从而实现转子的转动。这种丝状涡轮用丝状叶片取代传统特斯拉涡轮的薄圆盘，由于丝状叶片固定在两个厚圆盘上，所以比薄圆盘刚度好，不易变形，使转子可以做得直径更大而不易变形。丝状叶片形成的丝网结构还可对喷嘴气流具有一定的消音效果，降低机器噪音。
本发明的有益效果是，可以使涡轮的尺寸做大，从而功率加大且运行更平稳可靠，噪音降低。
附图说明
图1是本发明的结构示意图。
图2是本发明的剖视图。
图中1.喷嘴，2.壳体，3.固定盘，4.丝状叶片，5.排气口，6.排气孔，7.转子轴。
具体实施方式
在图中，壳体(2)上有喷嘴(1)，壳体(2)内有转子，转子由固定盘(3)和固定于固定盘(3)之间的丝状叶片(4)构成，转子轴(7)中空并开有排气孔(6)联通到排气口(5)。
工作时气体由喷嘴(1)，喷入壳体(2)内，气流会在壳体(2)内侧的导向作用下形成涡流，由于固定盘(3)之间布满丝状叶片(4)大大增加了转子与气流的接触面，根据边界层效应，转子将被气流带动一起旋转，从而实现转子的转动，做完功的泛气由转子轴(7)上的排气孔(6)通到排气口(5)排出。

Claims (3)

1.一种丝状涡轮，包括喷嘴，壳体和转子，其特征是：转子叶片为丝状，丝状叶片固定于两个圆盘之间，转子轴中空并开有排气孔。
2.根据权利要求书1所述的一种丝状涡轮，其特征是丝状叶片相互平行呈多层鸟笼状。
3.根据权利要求书1所述的一种丝状涡轮，其特征是丝状叶片纵横交错呈三维网状。
CN201210241691.5A 2012-07-13 2012-07-13 一种丝状涡轮 Active CN103541773B (zh)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN201210241691.5A CN103541773B (zh) 2012-07-13 2012-07-13 一种丝状涡轮
PCT/CN2013/077216 WO2014008800A1 (zh) 2012-07-13 2013-06-14 一种丝状涡轮
US14/413,363 US9260967B2 (en) 2012-07-13 2013-06-14 Filamentous turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210241691.5A CN103541773B (zh) 2012-07-13 2012-07-13 一种丝状涡轮

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CN103541773A true CN103541773A (zh) 2014-01-29
CN103541773B CN103541773B (zh) 2016-04-06

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US (1) US9260967B2 (zh)
CN (1) CN103541773B (zh)
WO (1) WO2014008800A1 (zh)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104895617A (zh) * 2015-05-19 2015-09-09 集美大学 无扇叶涡轮发动机
CN105201559A (zh) * 2014-06-20 2015-12-30 时剑 一种穿透式涡轮
CN105879540A (zh) * 2014-12-16 2016-08-24 时剑 一种离心式空气净化器
CN110114554A (zh) * 2016-09-08 2019-08-09 绿青蛙涡轮机(英国)有限公司 边界层涡轮机

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* Cited by examiner, † Cited by third party
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US6890142B2 (en) * 2001-10-09 2005-05-10 James G. Asseken Direct condensing turbine
US20070296219A1 (en) * 2005-02-28 2007-12-27 Horia Nica Boundary Layer Wind Turbine
WO2008134868A1 (en) * 2007-05-05 2008-11-13 Gordon David Sherrer System and method for extracting power from fluid
US20100232968A1 (en) * 2009-03-13 2010-09-16 Rolls-Royce Plc Vibration damper
WO2011057019A1 (en) * 2009-11-04 2011-05-12 Wilson Erich A Composite boundary layer turbine
CN102373958A (zh) * 2010-08-18 2012-03-14 时剑 一种环形特斯拉涡轮
CN202851088U (zh) * 2012-07-13 2013-04-03 时剑 一种丝状涡轮

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Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6890142B2 (en) * 2001-10-09 2005-05-10 James G. Asseken Direct condensing turbine
US20070296219A1 (en) * 2005-02-28 2007-12-27 Horia Nica Boundary Layer Wind Turbine
WO2008134868A1 (en) * 2007-05-05 2008-11-13 Gordon David Sherrer System and method for extracting power from fluid
US20100232968A1 (en) * 2009-03-13 2010-09-16 Rolls-Royce Plc Vibration damper
WO2011057019A1 (en) * 2009-11-04 2011-05-12 Wilson Erich A Composite boundary layer turbine
CN102373958A (zh) * 2010-08-18 2012-03-14 时剑 一种环形特斯拉涡轮
CN202851088U (zh) * 2012-07-13 2013-04-03 时剑 一种丝状涡轮

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105201559A (zh) * 2014-06-20 2015-12-30 时剑 一种穿透式涡轮
CN105879540A (zh) * 2014-12-16 2016-08-24 时剑 一种离心式空气净化器
CN104895617A (zh) * 2015-05-19 2015-09-09 集美大学 无扇叶涡轮发动机
CN104895617B (zh) * 2015-05-19 2016-08-24 集美大学 无扇叶涡轮发动机
CN110114554A (zh) * 2016-09-08 2019-08-09 绿青蛙涡轮机(英国)有限公司 边界层涡轮机

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Publication number Publication date
CN103541773B (zh) 2016-04-06
WO2014008800A1 (zh) 2014-01-16
US20150192018A1 (en) 2015-07-09
US9260967B2 (en) 2016-02-16

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