CN105649686A - Novel connected turbine structure - Google Patents
Novel connected turbine structure Download PDFInfo
- Publication number
- CN105649686A CN105649686A CN201410399964.8A CN201410399964A CN105649686A CN 105649686 A CN105649686 A CN 105649686A CN 201410399964 A CN201410399964 A CN 201410399964A CN 105649686 A CN105649686 A CN 105649686A
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- CN
- China
- Prior art keywords
- turbine structure
- turbine
- novel connected
- connected turbine
- design
- 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.)
- Pending
Links
- 238000009434 installation Methods 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000002912 waste gas Substances 0.000 description 1
Landscapes
- Gears, Cams (AREA)
Abstract
The invention relates to the technical field of automobile accessories, in particular to a novel connected turbine structure. The novel connected turbine structure comprises an upper gear (1) and a lower turbine (2) which are in an integrated design. The novel connected turbine structure is reasonable in structural design, the problem of tightness caused by assembling is avoided due to the integrated design, and the novel connected turbine structure is convenient to install, easy to operate and capable of effectively improving the performance of an engine.
Description
Technical field:
The present invention relates to auto-parts technical field, be specifically related to a kind of novel conjoined turbine structure.
Background technology:
Turbine (turbo), is the fan in the engine of automobile or aircraft, by utilizing waste gas (exhaustgases) that fuel vapour (fuelvapour) is blown into engine, to improve the performance of engine.
Turbine is a kind of rotary power machinery that the energy of flow working medium is converted to mechanical power. It is one of critical piece of aero-engine, gas turbine and steam turbine.
Existing turbine is all assemble, and abrasion is big in operation, can cause the compactness connected between turbine, once compactness goes wrong, the work of turbine will be subject to serious impact, also can reduce the performance of engine.
Summary of the invention:
It is an object of the invention to provide a kind of novel conjoined turbine structure, its reasonable in design, the design of integral type avoids and assembles the tightness problems brought, and it is easy for installation, simple to operate, it is possible to the effective performance improving engine.
In order to solve the problem existing for background technology, the present invention is by the following technical solutions: it comprises gear 1, lower turbine 2, described gear 1 and lower turbine 2 and designs for integral type.
Operation principle of the present invention: gear 1 and lower turbine 2 design for disjunctor, very close to each other between them, installs with to operate all hinge structure convenient a lot.
The method have the advantages that its reasonable in design, the design of integral type avoids and assembles the tightness problems brought, and it is easy for installation, simple to operate, it is possible to the effective performance improving engine.
Accompanying drawing illustrates:
Fig. 1 is present configuration schematic diagram.
Detailed description of the invention:
Referring to Fig. 1, this detailed description of the invention by the following technical solutions: it comprises gear 1, lower turbine 2, described gear 1 and lower turbine 2 and designs for integral type.
This detailed description of the invention operation principle: gear 1 and lower turbine 2 design for disjunctor, very close to each other between them, installs with to operate all hinge structure convenient a lot.
This detailed description of the invention has the advantages that its reasonable in design, and the design of integral type avoids and assembles the tightness problems brought, and it is easy for installation, simple to operate, it is possible to the effective performance improving engine.
Claims (1)
1. a novel conjoined turbine structure, it is characterised in that it comprises gear (1), lower turbine (2), and described gear (1) and lower turbine (2) design for integral type.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410399964.8A CN105649686A (en) | 2014-08-14 | 2014-08-14 | Novel connected turbine structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410399964.8A CN105649686A (en) | 2014-08-14 | 2014-08-14 | Novel connected turbine structure |
Publications (1)
Publication Number | Publication Date |
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CN105649686A true CN105649686A (en) | 2016-06-08 |
Family
ID=56482238
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410399964.8A Pending CN105649686A (en) | 2014-08-14 | 2014-08-14 | Novel connected turbine structure |
Country Status (1)
Country | Link |
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CN (1) | CN105649686A (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201344092Y (en) * | 2008-12-10 | 2009-11-11 | 张宗智 | Improved blade structure of gardening windmill |
CN101702927A (en) * | 2007-05-08 | 2010-05-05 | 耐可斯特驱动有限公司 | Automotive air blower |
US20110012361A1 (en) * | 2009-07-16 | 2011-01-20 | Lee S Peter | Integrated turbine generator/motor and method |
CN102943832A (en) * | 2012-11-22 | 2013-02-27 | 重庆津德福科技开发有限公司 | Hydrodynamic retarder rotating impeller |
-
2014
- 2014-08-14 CN CN201410399964.8A patent/CN105649686A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101702927A (en) * | 2007-05-08 | 2010-05-05 | 耐可斯特驱动有限公司 | Automotive air blower |
CN201344092Y (en) * | 2008-12-10 | 2009-11-11 | 张宗智 | Improved blade structure of gardening windmill |
US20110012361A1 (en) * | 2009-07-16 | 2011-01-20 | Lee S Peter | Integrated turbine generator/motor and method |
CN102943832A (en) * | 2012-11-22 | 2013-02-27 | 重庆津德福科技开发有限公司 | Hydrodynamic retarder rotating impeller |
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Legal Events
Date | Code | Title | Description |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160608 |