CN101747537A - Trend rubber for helicopter tires - Google Patents
Trend rubber for helicopter tires Download PDFInfo
- Publication number
- CN101747537A CN101747537A CN200910114699A CN200910114699A CN101747537A CN 101747537 A CN101747537 A CN 101747537A CN 200910114699 A CN200910114699 A CN 200910114699A CN 200910114699 A CN200910114699 A CN 200910114699A CN 101747537 A CN101747537 A CN 101747537A
- Authority
- CN
- China
- Prior art keywords
- rubber
- trend
- helicopter
- favorable
- carbon black
- 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
Landscapes
- Compositions Of Macromolecular Compounds (AREA)
Abstract
The invention discloses a trend rubber for helicopter tires. The rubber is made from natural rubber as the main material, and 3-polybutadiene rubber, intermediate super abrasion resistant carbon black and anti-vulcanization reducer as auxiliary materials which are mixed in certain proportions. By adding the 3-polybutadiene rubber, and intermediate super abrasion resistant carbon black, the trend rubber can be resulted to have appropriate dampness and favorable abrasion resistance; by adding the anti-vulcanization reducer, the rubber material can be resulted to have favorable thermal stability. Compared with the prior art, the trend rubber for helicopter tires of the invention has the advantages of high tensile strength, favorable flex cracking resistance, favorable thermal stability and higher dampness. The helicopter tires using the trend rubber have favorable damping performance and increases the riding comfort when the helicopter lands on the ground.
Description
Technical field
The present invention relates to aviation tire tread glue, be specifically related to trend rubber for helicopter tires.
Background technology
The vibrations of generation when vertiplane when landing mainly reduces to land with tire by the damping device of vertiplane jointly, at present the used aviation tire tread glue of vertiplane is to improve wear resistance and thermotolerance, because its damping capacity is not high, the vibrations that make vertiplane produce when landing can not be alleviated preferably.
Summary of the invention
The technical problem to be solved in the present invention provides a kind of trend rubber for helicopter tires.This tread rubber has higher damping capacity when possessing good thermotolerance and fatigue performance.
For solving the problems of the technologies described above, the present invention by the following technical solutions:
The vertiplane aviation tire tread glue is made of following component by weight:
1
#Smoke sheet rubber or 20
#Standard glue, 80~100 parts;
Cis-1,4-polybutadiene rubber, 0~20 part;
Intermediate super abrasion furnace black, 35~55 parts;
Zinc oxide, 3~10 parts;
Stearic acid, 1~4 part;
P phenylenediamine type antioxidant, 1~4 part;
Ketoamine class anti-aging agent, 1~4 part;
Paraffin or protection wax, 1~3 part;
Insoluble sulfuy, 1~4 part;
Sulfenamide type accelerators, 1~4 part;
1, two (the lemon imide methyl) benzene (being called for short anti-reversion agent PK900) of 3-, 0.5~1.0 part.
In the above-mentioned prescription:
Described intermediate super abrasion furnace black is N234 carbon black or N220 carbon black.
Described p phenylenediamine type antioxidant is N-(1, the 3-dimethylbutyl) N
/-diphenyl-para-phenylene diamine (being called for short anti-aging agent 4020), or N-sec.-propyl-N-diphenyl-para-phenylene diamine (abbreviation antioxidant 4010NA).
Described ketoamine class anti-aging agent is 2,2,4-trimethylammonium-1, and 2-dihyaroquinoline polymer (is called for short anti-aging agent RD.
Described insoluble sulfuy is insoluble sulfuy IS-60 or insoluble sulfuy IS-90.
Described sulfenamide type accelerators is N-oxydiethylene-2-[4-morpholinodithio base sulphenamide (being called for short accelerant N OBS), or N, N-dicyclohexyl-2-[4-morpholinodithio base sulphenamide (abbreviation accelerator DZ).
In the above-mentioned materials, natural rubber has extraordinary strength and extension property and best over-all properties; Cis-1,4-polybutadiene rubber has the advantage that the flex cracking resistance performance is good, ageing-resistant performance is good; The intermediate super abrasion furnace black that adds can improve the dissipation factor of sizing material, increases its damping capacity, so that tire has good damping performance; Adding anti-reversion agent PK900 in the sizing material can make cross-linked rubber have good thermostability and anti-recovery performance.
Trend rubber for helicopter tires of the present invention can adopt the ordinary method preparation.The performance of the sizing material of gained is as shown in table 1:
Table 1:
Project | Unit | Performance range |
Tensile strength | ??MPa | ??21~29 |
Tensile yield | ??% | ??450~650 |
Tear strength | ??kN/m | ??110~150 |
300% stress at definite elongation | ??MPa | ??7.0~15.0 |
Loss tangent value tan δ (60 ℃, 0.5 °, 60cpm) | ??/ | ??0.1~0.3 |
Compression fatigue is given birth to heat | ??℃/25min | ??17~30 |
Elongation change rate after the 100 ℃ * 24h hot air aging | ??% | ??-15~-30 |
Wear loss (Akron) | ??cm 3/1.61km | ??0.1~0.5 |
Flex crack rank (300,000 times) | Level | ??0~6 |
Compared with prior art, trend rubber for helicopter tires sizing material of the present invention have that tensile strength height, flex cracking resistance performance are good, the advantage of Heat stability is good and higher damping.Use vertiplane tire tire when vertiplane lands of this tread rubber that good damping performance is arranged, improve riding comfort.
Embodiment
Describe the present invention with embodiment below, but the present invention does not limit to these embodiment.
Below amounts of components among each embodiment be weight part.
Embodiment 1
Refine glue by specified each component in the following table 2, the mixing branch of sizing material carries out for two sections.One section mixing carries out in XHM-140 type Banbury mixer, and two-stage mixing carries out in XHM-140 type Banbury mixer.Order of addition(of ingredients) is conventional order of addition(of ingredients).Sizing material to gained carries out performance test then, has listed test result in table 2.
Embodiment 2
Refine glue by specified each component in the following table 2, sizing material mixing with embodiment 1 listed test result in table 2.
Embodiment 3
Refine glue by specified each component in the following table 2, sizing material mixing with embodiment 1 listed test result in table 2.
Embodiment 4
Refine glue by specified each component in the following table 2, sizing material mixing with embodiment 1 listed test result in table 2.
Table 2
The starting material title | Implement 1 | Implement 2 | Implement 3 | Implement 4 |
??1 #Smoke sheet rubber | ??80 | ??90 | ??0 | ??0 |
??20 #Standard glue | ??0 | ??0 | ??100 | ??85 |
Cis-1,4-polybutadiene rubber | ??20 | ??10 | ??0 | ??15 |
The N234 carbon black | ??55 | ??45 | ??0 | ??0 |
The N220 carbon black | ??0 | ??0 | ??35 | ??40 |
Zinc oxide | ??3 | ??4 | ??5 | ??8 |
Stearic acid | ??2 | ??2 | ??2 | ??4 |
Anti-aging agent 4020 | ??3 | ??3 | ??0 | ??0 |
Antioxidant 4010NA | ??0 | ??0 | ??3 | ??1 |
Anti-aging agent RD | ??1 | ??1 | ??1 | ??4 |
Paraffin | ??1 | ??2 | ??0 | ??0 |
Protection wax RP-3 | ??0 | ??0 | ??3 | ??1 |
Insoluble sulfuy IS-60 | ??1.5 | ??2 | ??0 | ??0 |
Insoluble sulfuy IS-90 | ??0 | ??0 | ??2.5 | ??3.5 |
Accelerant N OBS | ??1.4 | ??1.2 | ??0 | ??0 |
Accelerator DZ | ??0 | ??0 | ??1.0 | ??3 |
Anti-reversion agent PK900 | ??0.5 | ??0.8 | ??1.0 | ??0.8 |
Tensile strength (MPa) | ??23.0 | ??26.0 | ??24.2 | ??22.0 |
The starting material title | Implement 1 | Implement 2 | Implement 3 | Implement 4 |
Tensile yield (%) | ??430 | ??460 | ??500 | ??460 |
Tear strength (kN/m) | ??136 | ??142 | ??132 | ??130 |
300% stress at definite elongation (MPa) | ??14.4 | ??13.6 | ??13.6 | ??14.0 |
Loss tangent value tan δ (60 ℃, 0.5 °, 60cpm) | ??0.171 | ??0.145 | ??0.135 | ??0.138 |
The living heat of compression fatigue (℃/25min) | ??23 | ??22 | ??18 | ??19 |
Elongation change rate (%) after the 100 ℃ * 24h hot air aging | ??-27 | ??-22 | ??-25 | ??-22 |
Wear loss (Akron) (cm 3/1.61km) | ??0.123 | ??0.130 | ??0.135 | ??0.131 |
Flex crack rank (300,000 times) (level) | ??2 | ??1 | ??2 | ??2 |
Claims (5)
1. trend rubber for helicopter tires is made of following component by weight:
1
#Smoke sheet rubber or 20
#Standard glue, 80~100 parts;
Cis-1,4-polybutadiene rubber, 0~20 part;
Intermediate super abrasion furnace black, 35~55 parts;
Zinc oxide, 3~10 parts;
Stearic acid, 1~4 part;
P phenylenediamine type antioxidant, 1~4 part;
Ketoamine class anti-aging agent, 1~4 part;
Paraffin or protection wax, 1~3 part;
Insoluble sulfuy, 1~4 part;
Sulfenamide type accelerators, 1~4 part;
1, two (the lemon imide methyl) benzene of 3-, 0.5~1.0 part.
2. trend rubber for helicopter tires according to claim 1 is characterized in that: described intermediate super abrasion furnace black is N234 carbon black or N220 carbon black.
3. trend rubber for helicopter tires according to claim 1 is characterized in that: described p phenylenediamine type antioxidant is N-(1, the 3-dimethylbutyl) N
/-diphenyl-para-phenylene diamine, or N-sec.-propyl-N-diphenyl-para-phenylene diamine.
4. trend rubber for helicopter tires according to claim 1 is characterized in that: described ketoamine class anti-aging agent is 2,2,4-trimethylammonium-1,2-dihyaroquinoline polymer.
5. trend rubber for helicopter tires according to claim 1 is characterized in that: described sulfenamide type accelerators is N-oxydiethylene-2-[4-morpholinodithio base sulphenamide, or N, N-dicyclohexyl-2-[4-morpholinodithio base sulphenamide.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200910114699A CN101747537A (en) | 2009-12-30 | 2009-12-30 | Trend rubber for helicopter tires |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200910114699A CN101747537A (en) | 2009-12-30 | 2009-12-30 | Trend rubber for helicopter tires |
Publications (1)
Publication Number | Publication Date |
---|---|
CN101747537A true CN101747537A (en) | 2010-06-23 |
Family
ID=42475199
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN200910114699A Pending CN101747537A (en) | 2009-12-30 | 2009-12-30 | Trend rubber for helicopter tires |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101747537A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102134335A (en) * | 2010-12-30 | 2011-07-27 | 中国第一汽车集团公司 | Intermediate supporting cushion rubber of transmission shaft |
CN102146169A (en) * | 2010-12-28 | 2011-08-10 | 山东美晨科技股份有限公司 | High fatigue resistance rubber preparing raw material applied to automobile damping product |
CN103849012A (en) * | 2012-11-29 | 2014-06-11 | 中国化工橡胶桂林有限公司 | Environmentally-friendly cutting-resistant off-the-road tyre tread rubber |
CN104262718A (en) * | 2014-09-10 | 2015-01-07 | 中国化工集团曙光橡胶工业研究设计院有限公司 | High oil-resistant accumulator capsule gel |
CN106188679A (en) * | 2016-08-29 | 2016-12-07 | 樊之雄 | A kind of automobile wear-resistant vibration-damping rubber and preparation method thereof |
CN106589501A (en) * | 2016-12-10 | 2017-04-26 | 钦州学院 | Marine environment aviation tire tread rubber and preparation method thereof |
-
2009
- 2009-12-30 CN CN200910114699A patent/CN101747537A/en active Pending
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102146169A (en) * | 2010-12-28 | 2011-08-10 | 山东美晨科技股份有限公司 | High fatigue resistance rubber preparing raw material applied to automobile damping product |
CN102134335A (en) * | 2010-12-30 | 2011-07-27 | 中国第一汽车集团公司 | Intermediate supporting cushion rubber of transmission shaft |
CN102134335B (en) * | 2010-12-30 | 2013-04-24 | 中国第一汽车集团公司 | Intermediate supporting cushion rubber of transmission shaft |
CN103849012A (en) * | 2012-11-29 | 2014-06-11 | 中国化工橡胶桂林有限公司 | Environmentally-friendly cutting-resistant off-the-road tyre tread rubber |
CN104262718A (en) * | 2014-09-10 | 2015-01-07 | 中国化工集团曙光橡胶工业研究设计院有限公司 | High oil-resistant accumulator capsule gel |
CN104262718B (en) * | 2014-09-10 | 2016-08-24 | 中国化工集团曙光橡胶工业研究设计院有限公司 | A kind of high oil resistant accumulator capsule glue |
CN106188679A (en) * | 2016-08-29 | 2016-12-07 | 樊之雄 | A kind of automobile wear-resistant vibration-damping rubber and preparation method thereof |
CN106188679B (en) * | 2016-08-29 | 2018-05-11 | 浙江百朗士橡塑科技有限公司 | A kind of automobile using wear-resistant vibration-damping rubber and preparation method thereof |
CN106589501A (en) * | 2016-12-10 | 2017-04-26 | 钦州学院 | Marine environment aviation tire tread rubber and preparation method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101200559B (en) | Formula of high wear-resistant aviation tire tread glue | |
CN101319061B (en) | Tire tread glue formulation adapted for various pavement conditions | |
CN102634089B (en) | Tyre tread rubber composition used in hard mine area and production method of tyre tread rubber composition in hard mine area | |
CN101747537A (en) | Trend rubber for helicopter tires | |
CN104130462A (en) | Preparation method of rubber composition used for automobile and preparation method thereof | |
CN102746536B (en) | Formula of low-heat generation aircraft tire tread rubber | |
CN106977777B (en) | Radial air tire carcass layer kiss-coating | |
CN105419023A (en) | Tire tread rubber special for shop truck | |
CN103865119A (en) | Tire shoulder pad rubber of all-steel tire and preparation method of rubber | |
CN102617896A (en) | Tire shoulder mat rubber material of tire and mixing method thereof | |
CN104987549A (en) | Aviation tire reinforcing layer adhesive of high adhesive strength | |
CN101768294B (en) | Cord thread rubber compound for basic layer of automobile tire | |
CN104844850B (en) | Aircraft tire sidewall rubber with good solar radiation resistance performance | |
CN110157055B (en) | Sidewall rubber of aircraft tire | |
CN103435871B (en) | A kind of motor tyre casing tread rubber | |
CN102229713A (en) | Durable rubber and sample preparation method thereof | |
CN105524305A (en) | Tread rubber for engineering tire | |
CN112852029A (en) | Low-compression-heat-generation tire tread base rubber composite material and preparation method thereof | |
CN111732762A (en) | Formula capable of reducing dynamic heat generation of triangular belt primer | |
CN114752122B (en) | High-dynamic-adhesion-life carcass rubber as well as preparation method and application thereof | |
CN105566702A (en) | Agricultural tire crown compound of high filling tire reclaimed rubber | |
CN106046444A (en) | Special rubber material for side walls of tires | |
CN114181438B (en) | Aircraft tire shoulder rubber and preparation method and application thereof | |
CN106336535B (en) | Endless-track vehicle bogie wheel kiss-coating and preparation method thereof | |
CN104927114A (en) | Automobile chassis bushing rubber material and preparing method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20100623 |