CN201045499Y - Slippage electronic lighter - Google Patents

Slippage electronic lighter Download PDF

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Publication number
CN201045499Y
CN201045499Y CNU2007200013670U CN200720001367U CN201045499Y CN 201045499 Y CN201045499 Y CN 201045499Y CN U2007200013670 U CNU2007200013670 U CN U2007200013670U CN 200720001367 U CN200720001367 U CN 200720001367U CN 201045499 Y CN201045499 Y CN 201045499Y
Authority
CN
China
Prior art keywords
pushing mechanism
fuselage
piezo
electric device
electronic lighter
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
CNU2007200013670U
Other languages
Chinese (zh)
Inventor
陶央群
胡直
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.)
Individual
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 CNU2007200013670U priority Critical patent/CN201045499Y/en
Application granted granted Critical
Publication of CN201045499Y publication Critical patent/CN201045499Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a slidable electronic lighter, which comprises a main body, an ignition device arranged in the main body, and a pushing mechanism. The utility model is characterized in that a chute is arranged on the upper end of the main body, and a convex column is mounted on the upper end of the pushing mechanism. The pushing mechanism and the main body are mutually slipped, and a down-stroke piezoelectric device which is connected with the main body through shafts is connected with the pushing mechanism. The distance from the shaft connection point to the down-stroke piezoelectric device contact point is smaller than the distance from the shaft connection point to the contact point of the down-stroke piezoelectric device and the convex column.

Description

A kind of slip electronic lighter
[technical field]
The utility model relates to a kind of electronic lighter, particularly a kind of slidably electronic lighter of igniting.
[background technology]
Existing electronic lighter is owing to all be to adopt push type sparking form, and the igniting of this form is easy to generate maloperation.As when being placed in the pocket of clothes, careless, be easy to run into button, make lighter that the danger of igniting or gas leakage take place.In addition, also there is the problem of being operated by children easily in this existing push type lighter, causes certain potential safety hazard to children, and therefore, many countries have launched respectively many security legislations, and the security performance of lighter has been proposed very high requirement.
[utility model content]
The technical assignment of technical problem to be solved in the utility model and proposition is to overcome above-mentioned prior art defective, provides a kind of easy to operate, the slidably ignition lighter that security performance is good.
The technical solution of the utility model is such: the upper end on fuselage of the present utility model is provided with a hurricane globe, also is provided with projection at the outer surface of fuselage, and described pushing mechanism surface is provided with space striped at interval.This structure is convenient to operation, and feel is convenient good.
Stretch out a projection in pushing mechanism upper end to fuselage, connect, can slide along the chute of fuselage upper end with the piezo-electric device that presses down that is coupling on fuselage.The both sides of pushing mechanism become arcuation, adapt with fuselage, guarantee that like this pushing mechanism and fuselage be close to, and the maintenance balance.
Ignition mechanism of the present utility model is included in back and is provided with piezoelectricity, the piezo-electric device that presses down on fuselage of being coupling that contacts with piezoelectricity top.Press down piezo-electric device from shaft contact to the distance that presses down the piezoelectricity contact point less than from shaft contact to the distance that presses down piezo-electric device and projection contact point.
Can up push away with the projection that thumb is pinned fuselage during sparking, remaining four finger is close to the space striped of pushing mechanism to lower slider, pushing mechanism epirelief post is pushed downwards and is pressed down piezo-electric device, pressing down piezo-electric device presses down piezoelectricity and presses down skid plate, the fuel gas that the high-voltage spark that piezoelectricity produces ignites and discharges owing to the skid plate lifting is finished whole igniting action.
[description of drawings]
Fig. 1 is a right view schematic diagram of the present utility model.
Fig. 2 is a front view schematic diagram of the present utility model.
Fig. 3 is a vertical view schematic diagram of the present utility model.
Fig. 4 is an internal structure schematic diagram of the present utility model.
Fig. 5 is a use operation chart of the present utility model.
[specific embodiment]
As Fig. 1, Fig. 2, Fig. 3, Fig. 4 and shown in Figure 5, the upper end on fuselage 1 of the present utility model is provided with a hurricane globe 2, also is provided with projection 3 at the outer surface of fuselage 1, and described pushing mechanism 4 surfaces are provided with space striped 5 at interval.This structure is convenient to operation, and feel is convenient good.
Stretch out a projection 6 in pushing mechanism 4 upper ends to fuselage 1, connect, can slide along the chute 8 of fuselage 1 upper end with the piezo-electric device 7 that presses down that is coupling on fuselage 1.The both sides of pushing mechanism 4 become arcuation, adapt with fuselage 1, guarantee that like this pushing mechanism 4 and fuselage 1 be close to, and keep balance.
Ignition mechanism of the present utility model is included in fuselage 1 top and is provided with piezoelectricity 9, and being coupling of contacting with piezoelectricity 9 tops presses down piezo-electric device 7 on fuselage 1.Press down in the piezo-electric device 7 from shaft contact 10 to the distance that presses down piezoelectricity contact point 11 less than from shaft contact 10 to the distance that presses down piezo-electric device and projection contact point 12.
Can up push away with the projection 3 that thumb is pinned fuselage 1 during sparking, remaining four finger is close to the space striped 5 of pushing mechanism 4 to lower slider, projection 6 is pushed downwards and is pressed down piezo-electric device 7 in the pushing mechanism 4, pressing down piezo-electric device 7 presses down piezoelectricity 9 and presses down skid plate 13, the fuel gas that the high-voltage spark that piezoelectricity 9 produces ignites and discharges owing to skid plate 13 liftings is finished whole igniting action.
The utility model includes but not limited to the foregoing description.

Claims (5)

1. slip electronic lighter, comprise fuselage, an igniter that places in the fuselage, a pushing mechanism, it is characterized in that there is a chute described fuselage upper end, there is a projection described pushing mechanism upper end, and the piezo-electric device that presses down that described pushing mechanism slides mutually with fuselage, is coupling at fuselage connects with described pushing mechanism.
2. a kind of slip electronic lighter according to claim 1, described pushing mechanism surface is provided with space striped at interval.
3. a kind of slip electronic lighter according to claim 1, described pushing mechanism surface is provided with convex stripe at interval.
4. according to claim 1 or 2 or 3 described a kind of slip electronic lighters, described fuselage is provided with projection.
5. a kind of slip electronic lighter according to claim 4, described press down piezo-electric device from shaft contact to the distance that presses down the piezoelectricity contact point less than from shaft contact to the distance that presses down piezo-electric device and projection contact point.
CNU2007200013670U 2007-01-13 2007-01-13 Slippage electronic lighter Expired - Fee Related CN201045499Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2007200013670U CN201045499Y (en) 2007-01-13 2007-01-13 Slippage electronic lighter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2007200013670U CN201045499Y (en) 2007-01-13 2007-01-13 Slippage electronic lighter

Publications (1)

Publication Number Publication Date
CN201045499Y true CN201045499Y (en) 2008-04-09

Family

ID=39308969

Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2007200013670U Expired - Fee Related CN201045499Y (en) 2007-01-13 2007-01-13 Slippage electronic lighter

Country Status (1)

Country Link
CN (1) CN201045499Y (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20080409

Termination date: 20100220