CN109519494A - A kind of vibration and noise reducing spring of double helix periodic structure - Google Patents
A kind of vibration and noise reducing spring of double helix periodic structure Download PDFInfo
- Publication number
- CN109519494A CN109519494A CN201811470174.9A CN201811470174A CN109519494A CN 109519494 A CN109519494 A CN 109519494A CN 201811470174 A CN201811470174 A CN 201811470174A CN 109519494 A CN109519494 A CN 109519494A
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- China
- Prior art keywords
- spring
- vibration
- noise reducing
- connection ring
- periodic structure
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- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F3/00—Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic
- F16F3/02—Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic with springs made of steel or of other material having low internal friction
- F16F3/04—Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic with springs made of steel or of other material having low internal friction composed only of wound springs
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/02—Springs made of steel or other material having low internal friction; Wound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant
- F16F1/04—Wound springs
- F16F1/041—Wound springs with means for modifying the spring characteristics
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2228/00—Functional characteristics, e.g. variability, frequency-dependence
- F16F2228/06—Stiffness
- F16F2228/066—Variable stiffness
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The invention belongs to aircraft vehicle vibrations and field of noise control, and in particular to a kind of vibration and noise reducing spring of double helix periodic structure, including the first spring, second spring, connection ring；Connection ring and connection ring tandem arrange to form periodic arrangement, is connected with the first spring and second spring between connection ring simultaneously.Using the intrinsic frequency of periodic structure there is band gap properties progress vibration and noise reducing, the vibration for being effectively isolated driving source is transmitted, and improves damping property.There are bearer properties using spring arrangement, the loss of weight of aircaft configuration may be implemented.Due to there is no rubber type of material, material ageing problem is not present, improves structural life-time, reduces maintenance cost.
Description
Technical field
The invention belongs to aircraft vehicle vibrations and field of noise control, and in particular to a kind of vibration and noise reducing of double helix periodic structure
Spring, for reducing vibration and noise transmitting.Be related to include the strong vibrations such as engine and high revolving speed, the vibration of strong noise equipment and
Noise control.
Background technique
In aircraft vehicle vibrations and field of noise control, damper is a kind of common vibration and noise control device.These vibration dampings
Device common structure form is the structure type of spring-damper.Vibration attenuation mechanism is that damper has certain rigidity, the meeting in vibration
Generate the restoring force directly proportional to vibration displacement；And damper has damping, and when vibration, can also generate and vibration velocity is at just
The damping force of ratio keeps the vector sum of two power minimum by rigidity and damping design, and reaches vibration damping purpose.
Installation form common on aircraft at present, if the installation of engine uses more bar types of attachment (i.e. installation leverage),
The rack form etc. that the installation of most airborne equipments is also constituted using installation leverage.For this connection type, common vibration damping
Form is mounting dampers/vibration isolator at bracing stick joint.This kind of damper/vibration isolator is bright in single direction vibration-damping function
It is aobvious, but in joint area, the direction of vibration and damper/vibration isolator vibration damping direction for being transmitted to the position are difficult holding one
It causes, therefore effectiveness in vibration suppression is poor.
Since current damper only has vibration-damping function, it is difficult to bear external force, therefore the impost as aircraft
Installation uses.Especially in the case where stringent to weight demands, which is likely difficult to receive, and causes damper can not
Installation, to influence the effect of aircraft vibration and noise reducing.
Common damper/vibration isolator is mostly rubber type of material, is affected by temperature larger, and it is existing to there is aging in the high temperature environment
As, it is necessary to often replacement increases maintenance cost.
Summary of the invention
Both there is bearing function the purpose of the present invention is to provide a kind of, it may have the aircraft airborne system of vibration and noise reducing function
System/equipment mounting means.
The purpose of the present invention is achieved through the following technical solutions: a kind of vibration and noise reducing spring of double helix periodic structure, is used
It is installed in the vibration damping of the installation of aircraft engine vibration damping and airborne equipment.It include: the first spring, second spring, connection ring；Connection ring
It arranges to form periodic arrangement with connection ring tandem, is connected with the first spring and second spring between connection ring simultaneously.
In above scheme: the vibration and noise reducing spring of double helix periodic structure is mainly by the groups of springs of connection ring and two packet sizes
At the spring sizes in every group are identical.
In any of the above-described scheme preferably: connection ring and connection ring tandem arrange to form periodic arrangement；Two groups of springs
In each spring connected between two connection rings side by side.
In any of the above-described scheme preferably, change the bandgap frequency model of the vibration and noise reducing spring of double helix periodic structure
It encloses, makes external noise/vibration driving frequency in bandgap frequency range, the transmitting of external noise and vibration can be inhibited.
In any of the above-described scheme preferably, the vibration and noise reducing spring arrangement period of double helix periodic structure is at least 5；Week
Phase is more, and effectiveness in vibration suppression is better.
In any of the above-described scheme preferably, the first spring (1) is different with second spring (2) size.
In any of the above-described scheme preferably, change the quality of connection ring (3), thus it is possible to vary bandgap frequency.
In any of the above-described scheme preferably, change the rigidity of the first spring (1) or second spring (2), thus it is possible to vary band
Gap frequency.
In any of the above-described scheme preferably, change the material of the first spring (1) or second spring (2), thus it is possible to vary bullet
Spring rigidity.
In any of the above-described scheme preferably, change the number of active coils of the first spring (1) or second spring (2), Ke Yigai
Become spring rate.
In any of the above-described scheme preferably, change the spring filament diameter of the first spring (1) or second spring (2), Ke Yigai
Become spring rate.
In any of the above-described scheme preferably, change the central diameter of the first spring (1) or second spring (2), thus it is possible to vary bullet
Spring rigidity.
In any of the above-described scheme preferably, change the length of the first spring (1) and second spring (2), thus it is possible to vary bullet
Spring rigidity.
The beneficial effect of double helix periodic structure vibration and noise reducing spring provided by the present invention is, utilizes periodic structure
Intrinsic frequency there is band gap properties carry out vibration and noise reducing, be effectively isolated driving source vibration transmitting, improve damping
Energy.There are bearer properties using spring arrangement, the loss of weight of aircaft configuration may be implemented.Due to not having rubber type of material, it is not present
Material ageing problem improves structural life-time, reduces maintenance cost.
Detailed description of the invention
Fig. 1 is the vibration and noise reducing spring structure schematic diagram of double helix periodic structure,
Fig. 2 is the vibration and noise reducing spring vibration frequency effects figure of double helix periodic structure,
Wherein, 1 is the first spring, and 2 be second spring, and 3 be connection ring.
Specific embodiment
To keep the purposes, technical schemes and advantages of the invention implemented clearer, below in conjunction in the embodiment of the present invention
Attached drawing, technical solution in the embodiment of the present invention is further described in more detail.Before this it should be noted that this theory
It is the meaning in common meaning or dictionary that term or word used in bright book and claims, which is unable to limited interpretation, and
Should based in order to illustrate in the best way its invent inventor can be to the principle solution that the concept of term is suitably defined
It is interpreted as meaning and concept of the technical idea of the present invention.Therewith, it is indicated in embodiment and attached drawing documented by this specification
Structure is one of preferred embodiment, technical idea of the invention can not be represented completely, it will therefore be appreciated that right
May there are the various equivalents and variation for being able to carry out replacement for the present invention.Based on the embodiments of the present invention,
Every other embodiment obtained by those of ordinary skill in the art without making creative efforts, belongs to this hair
The range of bright protection.
The invention proposes a kind of vibration and noise reducing springs of double helix periodic structure, are related to existing noise reduction technology
It improves.
As shown in Figure 1, the vibration and noise reducing spring of double helix periodic structure includes the first spring (1), second spring (2) connects
Connect ring (3).
Change in the rigidity of the first spring (1) or second spring (2), including change spring material, spring filament diameter, spring
Diameter, length or number of coils etc., or change the quality of connection ring (3), thus it is possible to vary make bandgap frequency range；Work as the external world
Effectiveness in vibration suppression may be implemented in bandgap range in driving frequency.
As shown in Fig. 2, in the specific use process, since the inherent characteristic of double helix periodic structure makes vibration and noise reducing bullet
There are frequency band gaps for spring, when the driving frequency of extraneous vibration or noise is within the scope of the bandgap frequency of vibration and noise reducing spring,
Energy transmission significantly reduces, and vibration and noise reducing spring can be made to have high vibration and noise reducing performance.
The principle of foundation of the present invention is when propagating in a periodic structure using elastic wave, to generate elastic wave band gaps,
Elastic wave within the scope of bandgap frequency cannot be propagated in the structure.Therefore the knot constituted in One Dimension Periodic spring mass form
In structure, elastic wave propagation, by being designed to periodic structure, is changed bandgap frequency range, made external sharp based on longitudinal wave
The main frequency of vibrator source and sound source is fallen in bandgap range, achievees the purpose that vibration and noise controls.
The present invention has bearer properties using double helix periodic structure, and carrying, vibration damping, decrease of noise functions integration may be implemented
Design, is effectively reduced construction weight.
The material that the present invention uses is metal, without rubber type of material, material ageing problem is not present, can effectively improve
The service life of attachment device reduces maintenance cost.
Claims (5)
1. a kind of vibration and noise reducing spring of double helix periodic structure, including the first spring, second spring, connection ring；Its feature exists
It arranges to form periodic arrangement in: connection ring and connection ring tandem, is connected with the first spring and the second bullet between connection ring simultaneously
Spring.
2. the vibration and noise reducing spring of double helix periodic structure according to claim 1, it is characterised in that: periodic arrangement
Arrangement period is at least 5.
3. the vibration and noise reducing spring of double helix periodic structure according to claim 1, it is characterised in that: first bullet
Spring, second spring size be not identical.
4. the vibration and noise reducing spring of double helix periodic structure according to claim 1, it is characterised in that: the matter of connection ring
Amount, spring rate can be changed according to the actual situation, to change bandgap frequency.
5. the vibration and noise reducing spring of double helix periodic structure according to claim 1, it is characterised in that: the material of spring,
The number of active coils of spring, the spring filament diameter of spring, the central diameter of spring, the length of spring can be changed according to the actual situation, thus
Change spring rate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811470174.9A CN109519494A (en) | 2018-12-04 | 2018-12-04 | A kind of vibration and noise reducing spring of double helix periodic structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811470174.9A CN109519494A (en) | 2018-12-04 | 2018-12-04 | A kind of vibration and noise reducing spring of double helix periodic structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109519494A true CN109519494A (en) | 2019-03-26 |
Family
ID=65793931
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811470174.9A Pending CN109519494A (en) | 2018-12-04 | 2018-12-04 | A kind of vibration and noise reducing spring of double helix periodic structure |
Country Status (1)
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| CN (1) | CN109519494A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110472287A (en) * | 2019-07-16 | 2019-11-19 | 西北工业大学 | A kind of control method of periodic structure Propagation of Elastic Wave characteristic |
| CN110594331A (en) * | 2019-09-19 | 2019-12-20 | 哈尔滨工程大学 | Hierarchical periodic structure metamaterial beam suitable for multi-frequency-band vibration reduction |
| CN113007254A (en) * | 2021-02-08 | 2021-06-22 | 天津大学 | Elastic wave metamaterial vibration isolation device with particle damping characteristic |
| CN115638210A (en) * | 2022-10-13 | 2023-01-24 | 中国航空工业集团公司西安飞机设计研究所 | Vibration and noise reduction rotational symmetry device |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130127101A1 (en) * | 2011-11-21 | 2013-05-23 | Chrysler Group Llc | Three-stage concentric coil spring system |
| CN205371428U (en) * | 2015-12-21 | 2016-07-06 | 杭州勤业弹簧有限公司 | Novel compression spring |
| CN205841595U (en) * | 2016-07-18 | 2016-12-28 | 绍兴县柯利华汽车配件有限公司 | A kind of new automobile damping device |
| CN206017524U (en) * | 2016-08-19 | 2017-03-15 | 杭州勤业弹簧有限公司 | A kind of Double helix compression spring |
| CN206874728U (en) * | 2017-06-01 | 2018-01-12 | 中铁武汉电气化局集团科工装备有限公司 | One kind improves straddle-type monorail operation vehicle damping device |
| CN207715614U (en) * | 2018-01-09 | 2018-08-10 | 常州泰山弹簧有限公司 | Block brake spring |
-
2018
- 2018-12-04 CN CN201811470174.9A patent/CN109519494A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130127101A1 (en) * | 2011-11-21 | 2013-05-23 | Chrysler Group Llc | Three-stage concentric coil spring system |
| CN205371428U (en) * | 2015-12-21 | 2016-07-06 | 杭州勤业弹簧有限公司 | Novel compression spring |
| CN205841595U (en) * | 2016-07-18 | 2016-12-28 | 绍兴县柯利华汽车配件有限公司 | A kind of new automobile damping device |
| CN206017524U (en) * | 2016-08-19 | 2017-03-15 | 杭州勤业弹簧有限公司 | A kind of Double helix compression spring |
| CN206874728U (en) * | 2017-06-01 | 2018-01-12 | 中铁武汉电气化局集团科工装备有限公司 | One kind improves straddle-type monorail operation vehicle damping device |
| CN207715614U (en) * | 2018-01-09 | 2018-08-10 | 常州泰山弹簧有限公司 | Block brake spring |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110472287A (en) * | 2019-07-16 | 2019-11-19 | 西北工业大学 | A kind of control method of periodic structure Propagation of Elastic Wave characteristic |
| CN110594331A (en) * | 2019-09-19 | 2019-12-20 | 哈尔滨工程大学 | Hierarchical periodic structure metamaterial beam suitable for multi-frequency-band vibration reduction |
| CN113007254A (en) * | 2021-02-08 | 2021-06-22 | 天津大学 | Elastic wave metamaterial vibration isolation device with particle damping characteristic |
| CN115638210A (en) * | 2022-10-13 | 2023-01-24 | 中国航空工业集团公司西安飞机设计研究所 | Vibration and noise reduction rotational symmetry device |
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| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190326 |
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| RJ01 | Rejection of invention patent application after publication |