CN1059875A - The manufacture method of high-strength marine air bag shaped by lapping - Google Patents

The manufacture method of high-strength marine air bag shaped by lapping Download PDF

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Publication number
CN1059875A
CN1059875A CN 91106526 CN91106526A CN1059875A CN 1059875 A CN1059875 A CN 1059875A CN 91106526 CN91106526 CN 91106526 CN 91106526 A CN91106526 A CN 91106526A CN 1059875 A CN1059875 A CN 1059875A
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CN
China
Prior art keywords
cord
rubber plate
capsule
rubber
capsule body
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Granted
Application number
CN 91106526
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Chinese (zh)
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CN1022747C (en
Inventor
屠福根
潘华堂
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.)
Ji'nan Eagle air bag manufacturing Co., Ltd.
Original Assignee
LUYING AIR-BAG CONTAINER FACTORY JINAN
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Application filed by LUYING AIR-BAG CONTAINER FACTORY JINAN filed Critical LUYING AIR-BAG CONTAINER FACTORY JINAN
Priority to CN 91106526 priority Critical patent/CN1022747C/en
Publication of CN1059875A publication Critical patent/CN1059875A/en
Application granted granted Critical
Publication of CN1022747C publication Critical patent/CN1022747C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The invention discloses a kind of new technology for making marine rolling air bag.Air bag capsule body adopts the rubber buttress of band nylon cord to carry out the cutting splicing according to the utricule size, then many rubber plates that cut piled up together, and the shaped by lapping of reeling, and be bonded as one with adhesives.This new process has saved manufactures the inner tube of a tyre and Wrapping formed inconvenience on the type tire, manufactures easyly, feasible, and utricule is well-balanced, firm, and it is convenient to repair.The utricule air-tightness of manufacturing than old technology is good, long service life.

Description

The manufacture method of high-strength marine air bag shaped by lapping
The present invention relates to the manufacturing process of air sac container.
At present, domesticly manyly repair, the shipbuilding yard in, the upper and lower water conservancy project skill of craft adopted boats and ships air bag water conservancy project skill up and down, as using hoisting air chamber jacking boats and ships, so that beat pier or tear pier open, the use scroll airbag moves the upper and lower water of boats and ships etc.As for the manufacturing process of air-bag for ship, the inner tube of a tyre formula air bag with high intensity of introducing in the existing disclosed CN85203958 of the having patent, its method is that natural fiber or chemical fiber are twined and be bonded on the inner tube of a tyre, the inner tube of a tyre is one or more layers, the offset plate or the rubber of sulfuration.Other has the CN87101374 patent application to disclose to heat after vinylon cord that a kind of employing presses rubber twines the manufacture method of the air-bag for ship that press cure forms, and this method also is to process on the inner tube of a tyre.Through long-time production practice and use proof, preceding a kind of air bag has stopped producing and using because working strength is not enough, fragile; A kind of production method in back, though adopted the offset plate of the higher band cord of intensity, owing to be Wrapping formed on the inner tube of a tyre, the one, it is big to manufacture difficulty, and bladder shape is difficult to well-balanced, and technology is difficult to grasp, and the 2nd, owing to the utricule unshapeliness, influence the result of use of air bag.
The manufacturing process that the purpose of this invention is to provide the high-strength air-bag for ship of a kind of inner tube free of practical and type tire.
This utricule that is overlapped to form finger formula high-strength air-bag for ship is that the rubber buttress that adopts multilayer to have continuous synthetic fibre cord (or cord of other syntheticfibres, natural fiber, metal filament etc.) carries out cutting according to the air bag size, and will cut out good rubber buttress according to its cord trend, stagger and pile up together after the lapped seam, the overlap joint of reeling then, and carry out every layer of rubber plate and lap-joint bonding with adhesives, it is bonded as one, last, with the utricule made through high temperature vulcanized and moulding.
This air bag with high intensity has adopted shaped by lapping, is bonded as the technology of one again, and making is got up more feasible, easy, and utricule is more well-balanced, firm, has saved the inconvenience of making the inner tube of a tyre and twining on the type tire, has improved product design and has made work efficiency.As the rolling air-bag for ship of being with the rubber coiled sheet of vinylon cords around shaped by lapping with 3 layers, proof is functional in using practice, and it allows working pressure greater than 2 kilograms per centimeter 2, air-tightness is good, has prolonged service life.And can adopt different number of plies rubber plates to process according to customer requirement, breakage occurs and also can adopt the overlap joint bonding mode to repair.
Description of drawings.
Fig. 1, Fig. 2 are the part sectional view of roller air-bag for ship of the present invention, and wherein (1) is the capsule body; (2) be the capsule head; (3) be Nang Zui.
Fig. 3 is Figure 1A-A place section-drawing, and wherein (4) are the nexine offset plate; (5) be the middle level offset plate; (6) be outer offset plate.
Fig. 4 is three layers of rubber plate before the overlap joint of reeling piles up scheme drawing, wherein (7) for overlap joint with stitching.
Below in conjunction with embodiment and accompanying drawing the present invention is elaborated.
Present embodiment is around overlap joint and the high-strength marine scroll airbag of moulding with three layers of rubber coiled sheet with continuous synthetic fibre cord.Being with every pulling force of continuous synthetic fibre cord fabric thread is 22 kilograms, and the rubber plate adopts No. 101 rubber of standard, and adhesives adopts gasoline.The size of three layers of rubber plate and disposing way thereof are: the inside one deck rubber board placing is below for utricule, its disposing way is parallel with utricule according to cord-thread direction, its length equals the length of capsule body and two capsule heads, and its width is spliced into the girth that equals the capsule body with the rubber plate; Interlayer rubber plate piles up on nexine rubber plate, it is vertical with the cord of nexine offset plate according to the cord trend that it piles up mode, its length is longer than 30 centimetres of capsule body girths, grow part and give over to overlap joint usefulness, its width is spliced into the rubber plate and equals capsule height degree, reserve the overlap joint seam when piling up topmost, and two-layer rubber plate is bonded together with gasoline; Outer rubber plate piles up on the rubber plate of middle level, and its cord trend and size are identical with middle level rubber plate when piling up, and just move downwards its top again when piling up, and reserves overlap joint with seam, also with gasoline skin and middle level rubber plate is bonded together.Then, three layers of offset plate that are bonded into one are awarded certain pressure, as using the compacting of iron alkali.At last, three layers of rubber plate of compacting are reeled inwards, each layer overlaps with seam with the overlap joint of reserving respectively and is bonding with gasoline, makes tubular capsule body like this.Two acrocyst heads are coniform, use coniform mould during making, for put, the delivery tool is convenient, a part was not bonding in the middle of capsule can be reserved when last overlap joint is bonding, capsule head innermost layer is by nexine rubber plate two ends it to be cut into strip to be layered on the mould, carry out fissure of displacement overlap joint with the trapezoidal rubber plate that is cut into above it, bonding with gasoline, be bonded in capsule head and capsule body seam with the offset plate bar then, gain in strength, use the trapezoidal rubber plate of one deck fissure of displacement bonding above again, this two-layer trapezoidal rubber plate cord trend is vertical with undermost offset plate bar.After making two capsule heads, capsule head mould tool is taken out from the centre joint, with gasoline that the capsule body centre joint is bonding again, and with whole airbag aeration.The inflation back is twined a circle and bonding at capsule head and capsule body junction with kiss-coating cord line adhesive lath, the outside again with broad not with the thick 5 millimeters 101 rubber laths winding adhesive seal of cord, simultaneously, the longitudinal seam place of capsule body also uses this rubber lath adhesive seal.For improving the air bag working strength, the rubber plate of capsule body and capsule head outermost layer band cord uses thickening rubber plate, thick 2mm.All outermost layer seams of capsule body and capsule head all with thick 5mm not with the rubber lath adhesive seal of cord.After whole air bag is made, utricule is put into direct vulcanizing tank vulcanize, in 4 kilograms per centimeter 2Down sulfuration 50~90 minutes of pressure.

Claims (7)

1, a kind of manufacture method of the high-strength marine air bag shaped by lapping made from the offset plate that has continuous synthetic fibre cord (or other syntheticfibres, natural fiber, metal filament cord), the manufacturing that it is characterized in that the capsule body is that the offset plate that will have continuous synthetic fibre cord carries out the cutting splicing according to the utricule size, and will cut out good offset plate and move towards according to cord, stagger and pile up together after the lapped seam, and with adhesives stick to one, compacting, the overlap joint of reeling then, and seam is bonding.
2, the manufacture method of air-bag for ship as claimed in claim 1, it is characterized in that capsule body (1) is around overlap joint and moulding by three layers of rubber coiled sheet with continuous synthetic fibre cord, the size of three layers of rubber plate and disposing way are: nexine rubber plate (4) is according to cord trend and capsule body laid parallel, its length equals the length of capsule body and two capsule heads, and its width equals the girth of capsule body; Middle level rubber plate (5) piles up on nexine rubber plate, moves under the top and reserves overlap joint with stitching (7), and its cord trend is vertical with nexine offset plate cord, and its length slightly is longer than capsule body girth, and its width equals capsule height degree; Outer rubber plate (6) piles up on the rubber plate of middle level, move under the same top and reserve overlap joint with stitching, its cord trend and size dimension are identical with middle level rubber plate, with adhesives that three layers of rubber plate are bonding, and compacting, then, three layers of rubber plate that are bonded into one are reeled inwards, each layer overlaps with seam with the overlap joint of reserving respectively, and bonding with adhesives, makes simple shape capsule body; Capsule head (2) innermost layer is the offset plate bar that is cut into by nexine rubber plate, and upper two layers is carried out fissure of displacement overlap joint with a plurality of trapezoidal offset plate pieces respectively, and is bonded as one with adhesives.
3, the manufacture method of air-bag for ship as claimed in claim 2 is characterized in that the capsule head adopts coniform mould when making.
4, the manufacture method of air-bag for ship as claimed in claim 2, it is characterized in that capsule body and capsule head outermost junction with vertical cord rubber lath wind with one circuit the overlap joint and bonding with adhesives.
5, the manufacture method of air-bag for ship as claimed in claim 1 or 2 is characterized in that described outermost layer band cord rubber plate is thickening rubber plate.
6, the manufacture method of air-bag for ship as claimed in claim 1 or 2 is characterized in that capsule body and the outmost lap side seam of capsule head place all adopt the rubber lath adhering and sealing of not being with cord.
7, the manufacture method of air-bag for ship as claimed in claim 1 or 2 is characterized in that described adhesives is a gasoline.
CN 91106526 1991-08-28 1991-08-28 Method for making high-strength marine air bag shaped by lapping Expired - Fee Related CN1022747C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 91106526 CN1022747C (en) 1991-08-28 1991-08-28 Method for making high-strength marine air bag shaped by lapping

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 91106526 CN1022747C (en) 1991-08-28 1991-08-28 Method for making high-strength marine air bag shaped by lapping

Publications (2)

Publication Number Publication Date
CN1059875A true CN1059875A (en) 1992-04-01
CN1022747C CN1022747C (en) 1993-11-17

Family

ID=4907927

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 91106526 Expired - Fee Related CN1022747C (en) 1991-08-28 1991-08-28 Method for making high-strength marine air bag shaped by lapping

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CN (1) CN1022747C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113371162A (en) * 2021-07-15 2021-09-10 哈尔滨工程大学 Anti-winding fixing frame for seabed sonar robot

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113371162A (en) * 2021-07-15 2021-09-10 哈尔滨工程大学 Anti-winding fixing frame for seabed sonar robot

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CN1022747C (en) 1993-11-17

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C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C06 Publication
PB01 Publication
C14 Grant of patent or utility model
GR01 Patent grant
C15 Extension of patent right duration from 15 to 20 years for appl. with date before 31.12.1992 and still valid on 11.12.2001 (patent law change 1993)
OR01 Other related matters
C57 Notification of unclear or unknown address
DD01 Delivery of document by public notice

Addressee: Guo Qunjie

Document name: Deemed not to advise

ASS Succession or assignment of patent right

Owner name: JINAN LUYING AIRBAG MANUFACTURING CO., LTD.

Free format text: FORMER OWNER: LUYING AIR-BAG CONTAINER FACTORY, JINAN

Effective date: 20041231

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20041231

Address after: Ji'nan City, Shandong province Xu Luo 250032 North South Industrial Park of Stone Road No. B-3

Patentee after: Ji'nan Eagle air bag manufacturing Co., Ltd.

Address before: 250000, 213, Chen Zhuang Street, Shizhong District, Shandong City, Ji'nan Province

Patentee before: Luying Air-bag Container Factory, Jinan

C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee