CN105649686A - Novel connected turbine structure - Google Patents

Novel connected turbine structure Download PDF

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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
Authority
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
Application number
CN201410399964.8A
Other languages
Chinese (zh)
Inventor
张发良
束庆林
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Haian Lianke Automobile Parts Co Ltd
Original Assignee
Haian Lianke Automobile Parts Co Ltd
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 Haian Lianke Automobile Parts Co Ltd filed Critical Haian Lianke Automobile Parts Co Ltd
Priority to CN201410399964.8A priority Critical patent/CN105649686A/en
Publication of CN105649686A publication Critical patent/CN105649686A/en
Pending legal-status Critical Current

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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

A kind of novel conjoined turbine structure
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.
CN201410399964.8A 2014-08-14 2014-08-14 Novel connected turbine structure Pending CN105649686A (en)

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
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
CN (1) CN105649686A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201344092Y (en) * 2008-12-10 2009-11-11 张宗智 Improved impeller structure of horticultural 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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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 impeller structure of horticultural 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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Application publication date: 20160608