CN205806301U - A kind of double-helix spring - Google Patents

A kind of double-helix spring Download PDF

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Publication number
CN205806301U
CN205806301U CN201620703848.5U CN201620703848U CN205806301U CN 205806301 U CN205806301 U CN 205806301U CN 201620703848 U CN201620703848 U CN 201620703848U CN 205806301 U CN205806301 U CN 205806301U
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CN
China
Prior art keywords
spring
external spiral
vortex
turn
internal coiling
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.)
Expired - Fee Related
Application number
CN201620703848.5U
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Chinese (zh)
Inventor
楼志明
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.)
Zhejiang Marriott Spring Co Ltd
Original Assignee
Zhejiang Marriott Spring 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 Zhejiang Marriott Spring Co Ltd filed Critical Zhejiang Marriott Spring Co Ltd
Priority to CN201620703848.5U priority Critical patent/CN205806301U/en
Application granted granted Critical
Publication of CN205806301U publication Critical patent/CN205806301U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of double-helix spring, including back-shaped double-helix spring body, described double-helix spring body is by the internal coiling spring of multi-turn, the external spiral spring of multi-turn, vortex-like spring composition under the upper vortex-like spring of multi-turn and multi-turn, described internal coiling spring and external spiral spring are distributed and the most equal with one heart, coupled by upper vortex-like spring between upper starting point and the upper starting point of external spiral spring of described internal coiling spring, between lower terminal and the lower terminal of external spiral spring of described internal coiling spring by under vortex-like spring couple, this utility model simple in construction, manufacture easy to use, cost-effective, so that internal coiling spring and external spiral spring concentric all the time and stress equalization, ensure the performance of spring, improve service life, practical, it is worthy to be popularized.

Description

A kind of double-helix spring
Technical field:
This utility model relates to spring technical field, a kind of double-helix spring.
Background technology:
Spring is a kind of machine components utilizing elasticity to carry out work, in order to control parts motion, relax impact or vibrations, Storage or saving energy, the size etc. of measurement power, be widely used in machine, instrument, through conventional two equal height different inner diameters in reality Spring concentric locking collar use together, but between two springs easily with respect to mobile cause concentric, so that spring is subject to Unbalanced being easy for of power produces tilt phenomenon, the most not only affects the service behaviour of spring, is more easy to make spring breaking down, reduces spring Service life.
Utility model content:
The purpose of this utility model is to overcome the deficiencies in the prior art, it is provided that a kind of simple in construction, concentric all the time and stress The double-helix spring of equilibrium.
This utility model solves the scheme of described technical problem: a kind of double-helix spring, including back-shaped Double helix bullet Spring body, described double-helix spring body is by the internal coiling spring of multi-turn, the external spiral spring of multi-turn, the upper vortex-like spring of multi-turn Vortex-like spring forms with under multi-turn, and described internal coiling spring and external spiral spring are distributed and the most equal with one heart, described interior spiral shell Coupled by upper vortex-like spring between upper starting point and the upper starting point of external spiral spring of rotation spring, the lower end of described internal coiling spring Point with the lower terminal of external spiral spring between by under vortex-like spring couple.
The hand of spiral of described internal coiling spring and external spiral spring is contrary.
Prominent effect of the present utility model is: the internal coiling spring being arranged concentrically and external spiral spring are by upper vortex-like spring Under with, vortex-like spring couples becomes an entirety so that stabilized structure, it is ensured that during use, internal coiling spring and external spiral spring begin It is in concentric eventually, vortex-like spring under the upper vortex-like spring being respectively multi-turn up and down of double-helix spring and multi-turn, it is ensured that Spring stress equalizes and firm without tilting, and the hand of spiral of internal coiling spring and external spiral spring is contrary, improves entirety Rigidity, this utility model simple in construction, manufacture and easy to use, cost-effective, improve the performance and used life of spring, economical Practicality, has the highest economic and social benefit, is worthy to be popularized.
Accompanying drawing illustrates:
Fig. 1 is perspective view of the present utility model.
Fig. 2 is the perspective view at another visual angle of this utility model.
Detailed description of the invention:
Below by embodiment, and combine accompanying drawing, the technical solution of the utility model is described in further detail.
As shown in Figure 1 and Figure 2, this utility model provides a kind of technical scheme: a kind of double-helix spring, including back-shaped double Helical spring body, described double-helix spring body by the internal coiling spring 1 of multi-turn, the external spiral spring 2 of multi-turn, multi-turn upper Under vortex-like spring 3 and multi-turn, vortex-like spring 4 forms, and described internal coiling spring 1 and external spiral spring 2 are distributed and height phase with one heart Deng, coupled by upper vortex-like spring 3 between upper starting point and the upper starting point of external spiral spring 2 of described internal coiling spring 1, described interior Between lower terminal and the lower terminal of external spiral spring 2 of helical spring 1 by under vortex-like spring 4 couple.
The hand of spiral of described internal coiling spring 1 and external spiral spring 2 is contrary.
When in use, the internal coiling spring 1 being arranged concentrically and external spiral spring 2 are by upper vortex-like bullet for this utility model Spring 3 and under vortex-like spring 4 couple and become an entirety so that stabilized structure, it is ensured that internal coiling spring 1 and external spiral bullet during use Spring 2 is in concentric all the time, vortex-like spring under the upper vortex-like spring 3 being respectively multi-turn up and down of double-helix spring and multi-turn 4, it is ensured that spring stress equalizes and firm without tilting, and the hand of spiral of internal coiling spring 1 and external spiral spring 2 is contrary, carries High overall rigidity, this utility model simple in construction, manufacture and easy to use, cost-effective, improve performance and the use of spring Life-span, economical and practical, there is the highest economic and social benefit, be worthy to be popularized.
Finally, embodiment of above is merely to illustrate this utility model, and is not limitation of the utility model, relevant skill The those of ordinary skill in art field, in the case of without departing from spirit and scope of the present utility model, it is also possible to make various change Changing and modification, the technical scheme of the most all equivalents falls within category of the present utility model, patent protection model of the present utility model Enclose and should be defined by the claims.

Claims (2)

1. a double-helix spring, it is characterised in that: include back-shaped double-helix spring body, described double-helix spring body by Vortex-like spring under the internal coiling spring (1) of multi-turn, the external spiral spring (2) of multi-turn, the upper vortex-like spring (3) of multi-turn and multi-turn (4) composition, described internal coiling spring (1) and external spiral spring (2) are distributed and the most equal with one heart, described internal coiling spring (1) Upper starting point and the upper starting point of external spiral spring (2) between by upper vortex-like spring (3) couple, described internal coiling spring (1) Between the lower terminal of lower terminal and external spiral spring (2) by under vortex-like spring (4) couple.
A kind of double-helix spring the most according to claim 1, it is characterised in that: described internal coiling spring (1) and external spiral The hand of spiral of spring (2) is contrary.
CN201620703848.5U 2016-07-01 2016-07-01 A kind of double-helix spring Expired - Fee Related CN205806301U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620703848.5U CN205806301U (en) 2016-07-01 2016-07-01 A kind of double-helix spring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620703848.5U CN205806301U (en) 2016-07-01 2016-07-01 A kind of double-helix spring

Publications (1)

Publication Number Publication Date
CN205806301U true CN205806301U (en) 2016-12-14

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620703848.5U Expired - Fee Related CN205806301U (en) 2016-07-01 2016-07-01 A kind of double-helix spring

Country Status (1)

Country Link
CN (1) CN205806301U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3712500A1 (en) * 2019-03-20 2020-09-23 Safran Aircraft Engines Fuel injector for a turbine engine
CN111706635A (en) * 2020-06-30 2020-09-25 博罗县福田精峰弹簧五金有限公司 High-strength composite spring and manufacturing method thereof

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3712500A1 (en) * 2019-03-20 2020-09-23 Safran Aircraft Engines Fuel injector for a turbine engine
FR3094074A1 (en) * 2019-03-20 2020-09-25 Safran Aircraft Engines FUEL INJECTOR FOR A TURBOMACHINE
CN111706635A (en) * 2020-06-30 2020-09-25 博罗县福田精峰弹簧五金有限公司 High-strength composite spring and manufacturing method thereof

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20161214

Termination date: 20170701