CN103697495B - Reusable lighter - Google Patents
Reusable lighter Download PDFInfo
- Publication number
- CN103697495B CN103697495B CN201410020612.7A CN201410020612A CN103697495B CN 103697495 B CN103697495 B CN 103697495B CN 201410020612 A CN201410020612 A CN 201410020612A CN 103697495 B CN103697495 B CN 103697495B
- Authority
- CN
- China
- Prior art keywords
- fuselage
- liquefied gas
- storage part
- mounting groove
- valve rod
- 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
Links
- 238000003860 storage Methods 0.000 claims abstract description 57
- 239000002184 metal Substances 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 238000007789 sealing Methods 0.000 claims description 4
- 238000005192 partition Methods 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 7
- 238000010892 electric spark Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical group [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 230000036642 wellbeing Effects 0.000 description 2
- 241001191009 Gymnomyza Species 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229920006332 epoxy adhesive Polymers 0.000 description 1
- 229920006335 epoxy glue Polymers 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Landscapes
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
The invention discloses a reusable lighter. The reusable lighter comprises an independent machine body gas storage part, wherein a spring mounting groove extending to the interior of a gas storage chamber is formed in an upper end partition board of the machine body gas storage part; a through hole is formed in the bottom of the spring mounting groove; a spring is arranged inside the spring mounting groove; the top end of the spring is contacted with the lower bottom surface of a cap body of a liquefied gas outlet valve rod; an air outlet which does not run through a rod body is formed in the interior of the liquefied gas outlet valve rod; the rod body integrally penetrates through the interior of a limiting cap body; the air outlet is communicated with an air inlet formed in the rod body; the upper end face of the cap body of the liquefied gas outlet valve rod is clamped on the lower bottom surface of the limiting cap body; the limiting cap body is fixed at the interior of the upper end of the spring mounting groove. A machine head and a machine body are two independent parts, and after liquefied gas in the machine body is used up, a new lighter can be formed by replacing a new machine body. The machine head part can be used repeatedly, thus the energy is saved.
Description
Technical field
The present invention relates to a kind of non-once lighter, belong to lighter technical field.
Background technology
Civilian lighter market type is various, and China is that the country that world production lighter output is maximum consumes most big country, national lighter annual requirement about 12,000,000,000.Most sale is disposable lighter in the market, this disposable lighter mainly includes ignition section and gas storage part two parts, by pressing head downwards when this lighter uses, make piezoelectric ceramics in igniter under pressure, mechanical energy is converted to electric energy, produce electric spark by conductive wire head end, thus light the liquefied gas of gas nozzle ejection.This lighter market price is generally 1 yuan 1, and price is inexpensive, but this lighter exists a problem is exactly, and after the liquefied gas of this lighter uses, whole lighter is just discarded, can only be abandoned.But head ignition section of this lighter or intact, smaller being not easy of lighter is reclaimed, and its waste plastics of the words of directly abandoning, useless liquefied gas, useless electronics etc. all can bring severe contamination to environment.
Summary of the invention
The object of the invention is to: a kind of non-once lighter is provided, head ignition section of this lighter and fuselage gas storage part are 2 independently parts, after the gas of fuselage gas storage part uses, change a new fuselage gas storage part and just can reuse.
Technical scheme of the present invention: a kind of non-once lighter, include independently fuselage gas storage part, endplate is provided with fuselage gas storage part the spring fitting groove stretching into air storage chamber inside, spring fitting trench bottom is provided with through hole, spring fitting groove inside is provided with spring, spring top contacts with liquefied gas outlet valve pole cap body bottom surface, liquefied gas outlet stem internal is provided with the venthole of non-through shaft, shaft entirety is passed from limited cap body inside, venthole is communicated with the air admission hole that shaft is provided with, liquefied gas outlet valve pole cap body upper surface is stuck on limited cap body bottom surface, it is inner that limited cap body is fixed on spring fitting groove upper end.
Aforesaid non-once lighter, the head end of described fuselage gas storage part is boss structure, and the fuselage lateral outer of boss structure is provided with location locking mechanism.
Aforesaid non-once lighter, during use, the head end of described fuselage gas storage part snaps in the lower end fuselage mounting groove of independently head ignition section, the casing inner wall that fuselage mounting groove is corresponding is provided with the positioning spigot locked groove coordinated with location locking mechanism, on the left of the installing plate of fuselage mounting groove upper end, igniter is installed, the sheet metal that igniter side is stretched out contacts with the end of the conductive wire in plug-in unit, the top of the corresponding gas nozzle of conductive wire head end, gas nozzle lower end is connected with hollow push rod, when the head end fuselage of fuselage gas storage part snaps in fuselage mounting groove, the groove of hollow push rod end is just to the head end of liquefied gas outlet valve rod, and liquefied gas is exported valve rod promote downwards.
Aforesaid non-once lighter, during use, the head end of described fuselage gas storage part snaps in the lower end fuselage mounting groove of independently head ignition section, the casing inner wall that fuselage mounting groove is corresponding is provided with the positioning spigot locked groove coordinated with location locking mechanism, casing above fuselage mounting groove is provided with roller, idler wheel bottom contacts with firestone, idler wheel bottom side is gas nozzle, gas nozzle lower end is connected with hollow push rod, when the head end fuselage of fuselage gas storage part snaps in fuselage mounting groove, the groove of hollow push rod end is just to the head end of liquefied gas outlet valve rod, and liquefied gas is exported valve rod promote downwards.
Aforesaid non-once lighter, described location locking mechanism is positioning spigot tapered end or circular orientation bulge loop.
Aforesaid non-once lighter, is provided with sealing gasket between described limited cap body bottom surface and liquefied gas outlet valve pole cap body upper surface.
Aforesaid non-once lighter, described spring fitting groove lower end base lead to the hole site place is provided with 1 sponge bar.
Beneficial effect of the present invention: when the present invention uses, fuselage gas storage part is entrapped in the fuselage holddown groove of head ignition section by location locking mechanism, thus is fixed by fuselage; Snap in process, liquefied gas is exported valve rod and releases downwards by hollow push rod, thus makes the liquefied gas in air storage chamber can enter into hollow push rod, sprays in use from gas nozzle.Lighter of the present invention has the advantage of the following aspects compared with existing lighter:
1, head ignition section and fuselage gas storage part are two independently parts, after the liquefied gas in fuselage gas storage part is used to complete, only need the new fuselage gas storage part of replacing 1 just can form 1 new lighter.Head ignition section can Reusability, thus has saved the energy.
2, because the main parts size of lighter concentrates on head section, and the parts of fuselage sections are fewer, with 1 head ignition section of the present invention corresponding 5-10 fuselage gas storage part, calculate with China's 12,000,000,000 annual requirements, only need to produce 12-24 hundred million head ignition section just can satisfy the demands, factory's fuselage gas storage part that then main centralized production parts are fewer, thus improve the production efficiency of factory, for factory brings economic well-being of workers and staff larger.
3, with corresponding 5-10 the fuselage gas storage part of 1 head ignition section, for consumers, if with 1 yuan, the present market words that 1 lighter calculates, fuselage gas storage part market price is the words of 5 maos, consumer uses 5-10 lighter can save 2-4.5 yuan, decreases the consumption expenditure for consumers.
4, the ignition of head ignition section of the present invention is by independently igniter and plug-in unit two parts form, eliminate Wear Characteristics of Epoxy Adhesive in original lighter and connect the technique of single metal copper core, thus eliminate a corresponding gluing equipment and corresponding operating personnel, decrease manpower to export, reduce production cost, the ignition structure that this plug-in unit is corresponding is simple, easy to assembly, 70% can be saved time with originally connecting compared with copper sheet wire with epoxy glue, save artificial 60%, reduce workshop floor space, realize mechanization modular operation, enhance productivity, thus bring larger economic well-being of workers and staff for enterprise.
5, after lighter of the present invention is finished using, the fuselage gas storage part more renewed, and the parts of fuselage gas storage part are fewer, easily split recovery, decrease and at will abandon lighter pollution on the environment.
Accompanying drawing explanation
Accompanying drawing 1 is the main TV structure schematic diagram of fuselage of the present invention;
Accompanying drawing 2 is fuselage close-up schematic view of the present invention;
Accompanying drawing 3 is the plan structure schematic diagram of fuselage band positioning spigot tapered end of the present invention;
Accompanying drawing 4 is the plan structure schematic diagram of fuselage band of the present invention annular positioning convex ring;
Accompanying drawing 5 is the handpiece structure schematic diagram of first embodiment of the invention;
Accompanying drawing 6 is that the head of first embodiment of the invention coordinates schematic diagram with fuselage;
Accompanying drawing 7 is the handpiece structure schematic diagram of second embodiment of the invention;
Accompanying drawing 8 is that the head of second embodiment of the invention coordinates schematic diagram with fuselage;
Reference numeral: 1-head ignition section, 2-fuselage gas storage part, 3-dividing plate, 4-air storage chamber, 5-spring fitting groove, 6-through hole, 7-spring, 8-liquefied gas outlet valve rod, 9-venthole, 10-air admission hole, 11-shaft, 12-limited cap body, 13-positioning spigot tapered end, 14-fuselage mounting groove, 15-positioning spigot locked groove, 16-igniter, 17-sheet metal, 18-plug-in unit, 19-conductive wire, 20-gas nozzle, the hollow push rod of 21-, 22-groove, 23-roller, 24-firestone, 25-circular orientation bulge loop, 26-sealing gasket, 27-sponge bar.
Detailed description of the invention
Embodiments of the invention 1: a kind of non-once lighter, as shown in figures 1-6, include the independently inner fuselage gas storage part 2 for cavity, endplate 3 is provided with fuselage gas storage part 2 the spring fitting groove 5 that 1 is stretched into air storage chamber 4 inside, 1 through hole 6 is provided with bottom spring fitting groove 5, spring fitting groove 5 inside is provided with 1 spring 7, spring 7 top and liquefied gas export valve rod 8 lower endcaps body bottom surface and contact, shaft 11 inside of liquefied gas outlet valve rod 8 is provided with venthole 9, venthole 9 is communicated with the air admission hole 10 that shaft 11 is provided with, liquefied gas outlet valve rod 8 lower endcaps body upper surface is stuck on limited cap body 12 bottom surface, shaft 11 entirety is inner through limited cap body 12, its head end stretches out outside limited cap body 12, it is inner that limited cap body 12 is fixed on spring fitting groove 5 upper end, its fixed form can be and is threaded.
The head end of fuselage gas storage part 2 is boss structure, and the fuselage lateral outer of boss structure is provided with location locking mechanism.Location locking mechanism is positioning spigot tapered end 13 or circular orientation bulge loop 25, and location locking mechanism can be symmetricly set on the forward and backward lateral surface of fuselage, in order to make it fixing relatively more firm, can arrange multiple location locking mechanism.
Limited cap body 12 bottom surface and liquefied gas export between valve rod 8 lower endcaps body upper surface and are provided with sealing gasket 26, prevent liquefied gas when fuselage gas storage part 2 is in air-tight state, spill from the space China and foreign countries between limited cap body 12 and shaft 11.
Spring fitting groove 5 lower end base through hole 6 position is provided with 1 sponge bar 27, sponge bar 27 extend in the inner bottom part of fuselage gas storage part 2, when to have additional sponge bar 27 be to make lighter use, liquefied gas can enter into liquefied gas outlet valve rod 8 quickly through spring fitting groove 5.
During use, the head end of fuselage gas storage part 2 snaps in the fuselage mounting groove 14 of head ignition section 1 lower end, the casing inner wall of fuselage mounting groove 14 correspondence is provided with the positioning spigot locked groove 15 coordinated with location locking mechanism, on the left of the installing plate of fuselage mounting groove 14 upper end, igniter 16 is installed, the sheet metal 17 that igniter 16 side is stretched out contacts with the end of the conductive wire 19 in plug-in unit 18, the top of the corresponding gas nozzle 20 of conductive wire 19 head end, gas nozzle 20 lower end is connected with hollow push rod 21, when the head end fuselage of fuselage gas storage part 2 snaps in the fuselage mounting groove 14 of head ignition section 1, the groove 22 of hollow push rod 21 end is just to the head end of liquefied gas outlet valve rod 8, and liquefied gas is exported valve rod 8 and promote downwards.
When the lighter of the present embodiment assembles, fuselage gas storage part 2 head end is independently snapped in the fuselage mounting groove 14 of head ignition section 1 lower end, now positioning spigot tapered end 13 or circular orientation bulge loop 25 snap in positioning spigot locked groove 15 with matching, and this positioning spigot locked groove 15 for groove one by one or can directly make a-circle-by-a-circle annular groove.After head ignition section 1 and fuselage gas storage part 2 fix, the groove 22 of hollow push rod 21 end of head ignition section 1 is just to the head end of liquefied gas outlet valve rod 8, snap in process hollow core push rod 21 liquefied gas can be exported valve rod 8 promote downwards, air admission hole 10 now on shaft 11 moves down and exposes out, thus make the liquefied gas in air storage chamber 4 enter into spring fitting groove 5 by through hole 6, enter into venthole 9 from air admission hole 10, then enter into the hollow push rod 21 contacted with it from venthole 9 top inner.During use, by downward press points firearm 16 head end, make the piezoelectric ceramics of igniter 16 inside under pressure mechanical energy is converted to electric energy, electric energy passes to conductive wire 19 from sheet metal 17, and conductive wire 19 head end can produce electric spark.During downward press points firearm 16, can press lower metal bridge plate, this metal bridge plate can will gas nozzle 20 be lifted, thus makes liquefied gas from hollow push rod 21, enter into gas nozzle 20 and spray simultaneously, the liquefied gas of ejection and electric spark effect, thus liquefied gas is lighted.
After the liquefied gas in air storage chamber 4 is finished, a little firmly inwardly extrude fuselage gas storage part 2 headend wall, fuselage gas storage part 2 is exited from the fuselage mounting groove 14 of head ignition section 1, now hollow push rod 21 is separated with venthole 9 end face, liquefied gas outlet valve rod 8 can under the effect of spring 7 on move, liquefied gas outlet valve rod 8 cap body upper surface contacts with limited cap body 12 bottom surface, air admission hole 10 on shaft 11 moves and sinks to limited cap body 12 inside, this time, air storage chamber 4 just defined an airtight space, the liquefied gas of its internal residual just can not be discharged to the outside.The fuselage gas storage part 2 changed can be thrown away or centralized recovery, and head ignition section 1 only needs to change a fuselage gas storage part 2 being full of liquefied gas again and just can continue to use.
Embodiments of the invention 2: as shown in accompanying drawing 1-4 and accompanying drawing 7-8, lighter in the present embodiment also by independently head ignition section 1 and independently fuselage gas storage part 2 form, the fuselage gas storage part 2 of the present embodiment 2 and identical in embodiment 1, difference is its head ignition section 1, head ignition section 1 in the present embodiment includes the fuselage mounting groove 14 of lower end, the casing inner wall of fuselage mounting groove 14 correspondence is provided with the positioning spigot locked groove 15 coordinated with location locking mechanism, casing above fuselage mounting groove 14 is provided with roller 23, contact with firestone 24 bottom roller 23, bottom roller 23, side is gas nozzle 20, gas nozzle 20 lower end is connected with hollow push rod 21, when the head end fuselage of fuselage gas storage part 2 snaps in the fuselage mounting groove 14 of head ignition section 1, the groove 22 of hollow push rod 21 end is just to the head end of liquefied gas outlet valve rod 8, and liquefied gas is exported valve rod 8 and promote downwards.Location locking mechanism is positioning spigot tapered end 13 or circular orientation bulge loop 25.
The producing method of the electric spark of the present embodiment 2 and the slightly different of embodiment 1, and liquefied gas extraction mode is the same.The present embodiment, by rotating roller 23, makes to produce electric spark between the roller 23 of rotation and the firestone 24 contacted, after some spark contacts with the liquefied gas sprayed in the gas nozzle 20 on roller 23 side, is lighted by liquefied gas.After liquefied gas uses, changing a new fuselage gas storage part 2 by the mode that exchanges for of embodiment 1 can reuse.
Claims (7)
1. a non-once lighter, it is characterized in that: include independently fuselage gas storage part (2), the upper endplate (3) of fuselage gas storage part (2) is provided with and stretches into the inner spring fitting groove (5) of air storage chamber (4), spring fitting groove (5) bottom is provided with through hole (6), spring fitting groove (5) inside is provided with spring (7), spring (7) top and liquefied gas export valve rod (8) cap body bottom surface and contact, liquefied gas outlet valve rod (8) inside is provided with the venthole (9) of non-through shaft (11), shaft (11) entirety is passed from limited cap body (12) inside, venthole (9) is communicated with the air admission hole (10) that shaft (11) is provided with, liquefied gas outlet valve rod (8) cap body upper surface is stuck on limited cap body (12) bottom surface, it is inner that limited cap body (12) is fixed on spring fitting groove (5) upper end.
2. non-once lighter according to claim 1, is characterized in that: the head end of described fuselage gas storage part (2) is boss structure, and the fuselage lateral outer of boss structure is provided with location locking mechanism.
3. non-once lighter according to claim 2, it is characterized in that: during use, the head end of described fuselage gas storage part (2) snaps in lower end fuselage mounting groove (14) of independently head ignition section (1), the casing inner wall that fuselage mounting groove (14) is corresponding is provided with the positioning spigot locked groove (15) coordinated with location locking mechanism, on the left of the installing plate of fuselage mounting groove (14) upper end, igniter (16) is installed, the sheet metal (17) that igniter (16) side is stretched out contacts with the end of the conductive wire (19) in plug-in unit (18), the top of the corresponding gas nozzle (20) of conductive wire (19) head end, gas nozzle (20) lower end is connected with hollow push rod (21), when the head end fuselage of fuselage gas storage part (2) snaps in fuselage mounting groove (14), the groove (22) of hollow push rod (21) end is just to the head end of liquefied gas outlet valve rod (8), and liquefied gas is exported valve rod (8) and promote downwards.
4. non-once lighter according to claim 2, it is characterized in that: during use, the head end of described fuselage gas storage part (2) snaps in lower end fuselage mounting groove (14) of independently head ignition section (1), the casing inner wall that fuselage mounting groove (14) is corresponding is provided with the positioning spigot locked groove (15) coordinated with location locking mechanism, the casing of fuselage mounting groove (14) top is provided with roller (23), roller (23) bottom contacts with firestone (24), side, roller (23) bottom is gas nozzle (20), gas nozzle (20) lower end is connected with hollow push rod (21), when the head end fuselage of fuselage gas storage part (2) snaps in fuselage mounting groove (14), the groove (22) of hollow push rod (21) end is just to the head end of liquefied gas outlet valve rod (8), and liquefied gas is exported valve rod (8) and promote downwards.
5. non-once lighter according to claim 2, is characterized in that: described location locking mechanism is positioning spigot tapered end (13) or circular orientation bulge loop (25).
6. non-once lighter according to claim 1, is characterized in that: described limited cap body (12) bottom surface and liquefied gas export between valve rod (8) cap body upper surface and be provided with sealing gasket (26).
7. non-once lighter according to claim 1, is characterized in that: described spring fitting groove (5) lower end base through hole (6) position is provided with 1 sponge bar (27).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410020612.7A CN103697495B (en) | 2014-01-17 | 2014-01-17 | Reusable lighter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410020612.7A CN103697495B (en) | 2014-01-17 | 2014-01-17 | Reusable lighter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103697495A CN103697495A (en) | 2014-04-02 |
| CN103697495B true CN103697495B (en) | 2015-05-27 |
Family
ID=50359112
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410020612.7A Expired - Fee Related CN103697495B (en) | 2014-01-17 | 2014-01-17 | Reusable lighter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103697495B (en) |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BR5600400U (en) * | 1976-04-08 | 1977-10-25 | J Glaser | LIGHTER WITH DISPOSABLE RECHARGEABLE TANK |
| JPH0612173B2 (en) * | 1990-08-31 | 1994-02-16 | 芳晴 岩松 | Fuel container exchangeable pocket tryter |
| DE19608258B4 (en) * | 1995-03-04 | 2005-07-14 | Chau, Phat Chon, Dipl.-Ing. | lighter |
| CN2367917Y (en) * | 1999-03-30 | 2000-03-08 | 杨凡赤 | Clamping-type lighter |
| JP2001012737A (en) * | 1999-06-28 | 2001-01-19 | Yoshinaga Tekunika Kk | Fuel tank exchange type gas lighter |
| CN2823837Y (en) * | 2005-09-29 | 2006-10-04 | 谢亦玲 | Lighter with changeable fuel box and changeable fuel box thereof |
| CN2932114Y (en) * | 2006-08-01 | 2007-08-08 | 张萧林 | cigarette lighter capable of changing general gas bottle |
| US20080044779A1 (en) * | 2006-08-15 | 2008-02-21 | Park Keith K | Multi-component lighter |
| CN101532676B (en) * | 2006-11-06 | 2011-02-16 | 谢亦玲 | Lighter with conveniently replaceable fuel cassette |
| CN201242169Y (en) * | 2008-05-30 | 2009-05-20 | 黄逢竞 | Igniter capable of exchanging gas box conveniently |
| CN202056908U (en) * | 2011-03-01 | 2011-11-30 | 宁波新海电气股份有限公司 | Lighter capable of replacing gas tank |
| CN203810448U (en) * | 2014-01-17 | 2014-09-03 | 曾利祥 | Non-disposable lighter |
-
2014
- 2014-01-17 CN CN201410020612.7A patent/CN103697495B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN103697495A (en) | 2014-04-02 |
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Effective date of registration: 20171122 Address after: 551200 Guizhou Province, Qiannan Buyei and Miao Autonomous Prefecture Longli County Economic Development Zone Industrial Park Valley foot Patentee after: Heng Bo Longli Electronic Co. Ltd. Address before: 550005 Guizhou city of Guiyang province Jinyang New Dry Drawing Center Plaza Building 2 unit B No. 16-9 Patentee before: Zeng Lixiang |
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