CN104233920B - Super coating of aircraft carrier runway - Google Patents

Super coating of aircraft carrier runway Download PDF

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Publication number
CN104233920B
CN104233920B CN201310735689.8A CN201310735689A CN104233920B CN 104233920 B CN104233920 B CN 104233920B CN 201310735689 A CN201310735689 A CN 201310735689A CN 104233920 B CN104233920 B CN 104233920B
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CN
China
Prior art keywords
woven fabrics
aramid fiber
coating
fanglun
surface layer
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
CN201310735689.8A
Other languages
Chinese (zh)
Other versions
CN104233920A (en
Inventor
张达
张文知
孟琳
曲军
肖永霞
何振华
袁磊
宋富雷
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.)
Li Yousheng
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201310735689.8A priority Critical patent/CN104233920B/en
Publication of CN104233920A publication Critical patent/CN104233920A/en
Application granted granted Critical
Publication of CN104233920B publication Critical patent/CN104233920B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention discloses a super coating of an aircraft carrier runway. The super coating is prepared from a water-based fluorine carbon emulsion, nano white carbon black, nano anatase titanium dioxide, an aramid fiber non-woven fabric, a silane coupling agent and the like. The coating of the aircraft carrier runway, which is prepared by coating and patching, is extremely high in intensity, is cleaned automatically to prevent bacteria, has effects of fire prevention, high temperature resistance and impact resistance, and is long in service life.

Description

The superpower coating of carrier-based aircraft runway
Technical field
The present invention relates to advanced manufacturing technology field, the espespecially superpower coating of carrier-based aircraft runway.
Background technology
Aircraft carrier is big country's sharp weapon, and carrier-borne aircraft is the primary armament of its attack and defense all dependence, and carrier-borne aircraft is to runway Dependence also need not query;The carrier-based aircraft strength of runways making is very big, self-cleaning fungi-proofing, fire-proof high-temperature resistant, shock resistance, the longevity The long carrier-based aircraft runway coating of life has caused the attention of a lot of people.
Content of the invention
The purpose of the present invention aims to solve the problem that the deficiency of prior art, provides carrier-based aircraft runway superpower coating, its skill Art scheme is as follows: the superpower coating of carrier-based aircraft runway, and it comprises the different aramid fiber non-woven fabrics of three layer functions, three tack coats With One function surface layer;The different aramid fiber non-woven fabrics of three described layer functions, the respectively superpower Fanglun l414 of bottom are no Spin cloth, the aramid fiber 1313 non-woven fabrics of the fine fire resisting of intensity of surface layer, intermediate layer is Fanglun l414 and 1313 blending non-woven fabrics;Three Individual tack coat is to be made into by water-base fluorocarbon emulsion, Nano carbon white titanium dioxide, silane coupler;Menu surface layer is coated in table Face, is made into by water-base fluorocarbon emulsion, Wastewater by Nanometer Anatase titanium dioxide, silane coupler.
The present invention is compared with conventional art following distinguishing feature and good effect: the carrier-based aircraft runway of making applies Layer intensity maximum, self-cleaning fungi-proofing, fire-proof high-temperature resistant, shock resistance, life-span length.
Specific embodiment
In order to more fully understand and implement the present invention, specific embodiment be given below:
The superpower coating of carrier-based aircraft runway, it comprises the different aramid fiber non-woven fabrics of three layer functions, three tack coats and One function surface layer;The superpower Fanglun l414 nonwoven of the different aramid fiber non-woven fabrics of three described layer functions, respectively bottom Cloth, the aramid fiber 1313 non-woven fabrics of the fine fire resisting of intensity of surface layer, intermediate layer is Fanglun l414 and 1313 blending non-woven fabrics;Three Tack coat is to be made into by water-base fluorocarbon emulsion, Nano carbon white titanium dioxide, silane coupler;Menu surface layer is coated in table Face, is made into by water-base fluorocarbon emulsion, Wastewater by Nanometer Anatase titanium dioxide, silane coupler.
Construction process is:
1. deck cleaning-drying, coats first tack coat, lays Fanglun l414 non-woven fabrics, is dried;
2. second tack coat is coated on Fanglun l414 non-woven fabrics, lays Fanglun l414 and 1313 blending non-woven fabrics, It is dried;
3. Fanglun l414 and 1313 blending non-woven fabrics on coat the 3rd tack coat, lay aramid fiber 1313 non-woven fabrics, It is dried;
4. coating functions surface layer on aramid fiber 1313 non-woven fabrics, it is superpower that drying completes carrier-based aircraft runway The making of coating.

Claims (1)

1. the superpower coating of carrier-based aircraft runway, is characterized in that: it comprises the different aramid fiber non-woven fabrics of three layer functions, three Tack coat and One function surface layer;The different aramid fiber non-woven fabrics of three described layer functions, the respectively superpower aramid fiber of bottom 1414 non-woven fabrics, the aramid fiber 1313 non-woven fabrics of the fine fire resisting of intensity of surface layer, intermediate layer be Fanglun l414 with 1313 mix Spin non-woven fabrics;Three tack coats are to be made into by water-base fluorocarbon emulsion, Nano carbon white titanium dioxide, silane coupler;Menu Surface layer is coated in surface, is made into by water-base fluorocarbon emulsion, Wastewater by Nanometer Anatase titanium dioxide, silane coupler;Construction process is: 1). deck cleaning-drying, coat first tack coat, lay Fanglun l414 non-woven fabrics, be dried;2). in Fanglun l414 no Spin and second tack coat is coated on cloth, lay Fanglun l414 and 1313 blending non-woven fabrics, be dried;3). in Fanglun l414 Coat the 3rd tack coat with 1313 blending non-woven fabrics, lay aramid fiber 1313 non-woven fabrics, be dried;4). in aramid fiber 1313 Coating functions surface layer on non-woven fabrics, drying completes the making of the superpower coating of carrier-based aircraft runway.
CN201310735689.8A 2013-12-28 2013-12-28 Super coating of aircraft carrier runway Expired - Fee Related CN104233920B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310735689.8A CN104233920B (en) 2013-12-28 2013-12-28 Super coating of aircraft carrier runway

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310735689.8A CN104233920B (en) 2013-12-28 2013-12-28 Super coating of aircraft carrier runway

Publications (2)

Publication Number Publication Date
CN104233920A CN104233920A (en) 2014-12-24
CN104233920B true CN104233920B (en) 2017-02-01

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310735689.8A Expired - Fee Related CN104233920B (en) 2013-12-28 2013-12-28 Super coating of aircraft carrier runway

Country Status (1)

Country Link
CN (1) CN104233920B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4567085A (en) * 1983-02-08 1986-01-28 Metzeler Kautschuk Gmbh Floor covering, especially for airplanes
JPH06248545A (en) * 1993-02-19 1994-09-06 Suzuki Sogyo Co Ltd Composite material
CN101956326A (en) * 2009-12-03 2011-01-26 山东俊富无纺布有限公司 Polypropylene SMS (Spun-bond Melt-blown Spun-bond) composite non-woven fabric and processing method thereof
CN202006621U (en) * 2011-03-29 2011-10-12 泉州市信和涂料有限公司 Anticorrosion coating composite structure
CN102653652A (en) * 2012-05-02 2012-09-05 常州大学 Nano composite fluorocarbon coating and preparation method thereof
CN102676000A (en) * 2012-06-01 2012-09-19 广州四航材料科技有限公司 Self-cleaning anti-corrosive paint finishing coat and preparing method thereof

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4567085A (en) * 1983-02-08 1986-01-28 Metzeler Kautschuk Gmbh Floor covering, especially for airplanes
JPH06248545A (en) * 1993-02-19 1994-09-06 Suzuki Sogyo Co Ltd Composite material
CN101956326A (en) * 2009-12-03 2011-01-26 山东俊富无纺布有限公司 Polypropylene SMS (Spun-bond Melt-blown Spun-bond) composite non-woven fabric and processing method thereof
CN202006621U (en) * 2011-03-29 2011-10-12 泉州市信和涂料有限公司 Anticorrosion coating composite structure
CN102653652A (en) * 2012-05-02 2012-09-05 常州大学 Nano composite fluorocarbon coating and preparation method thereof
CN102676000A (en) * 2012-06-01 2012-09-19 广州四航材料科技有限公司 Self-cleaning anti-corrosive paint finishing coat and preparing method thereof

Also Published As

Publication number Publication date
CN104233920A (en) 2014-12-24

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
C41 Transfer of patent application or patent right or utility model
CB03 Change of inventor or designer information

Inventor after: Zhang Da

Inventor after: Zhang Wenzhi

Inventor after: Meng Lin

Inventor after: Qu Jun

Inventor after: Xiao Yongxia

Inventor after: He Zhenhua

Inventor after: Yuan Lei

Inventor after: Song Fulei

Inventor before: Zhang Wenzhi

COR Change of bibliographic data
TA01 Transfer of patent application right

Effective date of registration: 20161228

Address after: Luqiao District of Taizhou city in Zhejiang province 318050 Mai Zhi Qiao Road No. 888-16 Zhi Min building's laser

Applicant after: Li Yousheng

Address before: 264006 Yantai Province Development Zone, Shandong City District No. 35 building, unit 2, No. 1

Applicant before: Zhang Wenzhi

C14 Grant of patent or utility model
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: Super coating of aircraft carrier runway

Effective date of registration: 20181214

Granted publication date: 20170201

Pledgee: Zhejiang Tailong commercial bank Taizhou branch of Limited by Share Ltd

Pledgor: Li Yousheng

Registration number: 2018330000469

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: 20170201

Termination date: 20191228