CN205980295U - Hot air gun - Google Patents

Hot air gun Download PDF

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Publication number
CN205980295U
CN205980295U CN201620914749.1U CN201620914749U CN205980295U CN 205980295 U CN205980295 U CN 205980295U CN 201620914749 U CN201620914749 U CN 201620914749U CN 205980295 U CN205980295 U CN 205980295U
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China
Prior art keywords
groove
closing piece
fuselage
head
connection end
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Active
Application number
CN201620914749.1U
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Chinese (zh)
Inventor
韩挺
杨伟明
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Zhejiang Prade Electric Co.,Ltd.
Original Assignee
Zhejiang Prulde Electric Appliance Co Ltd
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.)
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Application filed by Zhejiang Prulde Electric Appliance Co Ltd filed Critical Zhejiang Prulde Electric Appliance Co Ltd
Priority to CN201620914749.1U priority Critical patent/CN205980295U/en
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Publication of CN205980295U publication Critical patent/CN205980295U/en
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Abstract

The utility model discloses a hot air gun belongs to the mechanical technical field of heating, including aircraft nose and fuselage, the aircraft nose includes head shell, is equipped with motor, fan and heating element in the head shell, and the fuselage includes the fuselage casing, head shell and fuselage casing rotate and link together, are equipped with between head shell and the fuselage casing to be used for making aircraft nose and fuselage to keep relatively fixed's locking mechanism. The utility model provides a hot air gun sets aircraft nose and fuselage to split type structure, and aircraft nose and fuselage rotate to be connected, and sets up locking mechanism between aircraft nose and the fuselage, and the user can improve hot air gun's commonality and use the convenience according to the angle between in service behavior and use needs adjustment fuselage and the aircraft nose.

Description

A kind of heat gun
Technical field
This utility model is related to heated mechanical technical field, more particularly, to a kind of heat gun.
Background technology
Heat gun is a kind of heated mechanical for heating formation thermal current after air, has multiple use functions, specifically For, heat gun can be used for removing the old paint of metal surface, removal autohension paster, heating of plastic sebific duct make it bend, dry Moist wood, heating make packaging film and packing tube thermal contraction, rust cleaning, heating be used in the vinyon contraction connecting metal and Heating makes welding thing softening etc., using the thermal current of the rifle core blowout of heating resistance wire, element can also be welded or pluck Remove.
Heat gun is typically made up of components such as housing, the motor being placed in housing, fan, heating element heater, switches, existing heat The housing of air pressure gun generally adopts symmetrical split-type structural, is fixed using screw or bolt during assembling housing.Assembling Afterwards, the head of heat gun and fuselage are one, and head can not rotate with respect to fuselage, and user can not pass through according to service condition Rotate head or fuselage to adjust the shape of heat gun, heat gun using limited.
Utility model content
In order to solve shortcoming and defect present in above-mentioned prior art, this utility model provides a kind of head and fuselage Using split-type structural, and head and the relatively turnable heat gun of fuselage.
In order to realize above-mentioned technical purpose, the heat gun that this utility model provides, including head and fuselage, described head bag Include head shell, in head shell, be provided with motor, fan and heating assembly, fuselage includes body shell;Head shell and fuselage Housing into rotation links together, and is provided with for making head and fuselage keep relatively-stationary lock between head shell and body shell Tight mechanism.
Preferably, described retaining mechanism includes cage knob, cage knob be circumferentially with least one closing piece;Head shell be provided with The connection end of body shell cooperation, connection end is provided with the draw-in groove with closing piece cooperation;Body shell is provided with the dress for installing cage knob Distribution, body shell is in the groove being circumferentially with closing piece cooperation of pilot hole;Closing piece is inserted in draw-in groove and groove simultaneously and makes machine Head and fuselage are relatively fixed.
Preferably, the quantity of described draw-in groove and the quantity of closing piece are consistent, and the quantity of groove is M times of closing piece quantity, M >=2 And be natural number, closing piece disengaging groove opportunity is in rotary state;Or, the quantity one of the quantity of described groove and closing piece Cause, the quantity of draw-in groove is N times of closing piece quantity, N >=2 and be natural number, closing piece disengaging draw-in groove when head be in rotary state.
Preferably, described cage knob be circumferentially with two closing pieces, and two closing pieces be located at same radially;Head shell is even Connect and two draw-in grooves are arranged with the outer wall at end;The inwall that body shell is located at pilot hole circumference is provided with four or six or eight Individual groove, and groove is symmetrical two-by-two.
Preferably, described retaining mechanism also includes the spring resetting for catch knob, and cage knob is towards the one of connection end Side is provided with shrinkage pool;When the quantity of groove is M times of closing piece quantity, the two ends of spring are against the outer wall of connection end and shrinkage pool respectively On diapire, when closing piece departs from groove, spring is in compressive state;Or, when the quantity of draw-in groove is N times of closing piece quantity, spring Two ends are individually fixed on the outer wall of connection end and the diapire of shrinkage pool, and when closing piece departs from draw-in groove, spring is in extended state.
Preferably, the circumferential edge of described pilot hole bends inwards and forms the flange being used for spacing cage knob;The quantity of groove When being M times of closing piece quantity, between flange end face and connection end outer wall, it is smaller than closing piece along the length of cage knob axial direction;Or Person, when the quantity of draw-in groove is N times of closing piece quantity, the spacing between flange end face and connection end outer wall is more than or equal to closing piece edge The length of cage knob axial direction.
Preferably, the diapire of described shrinkage pool is provided with the locating dowel of connection end protrusion, connection end is provided with location hole, Locating dowel is inserted in location hole, and spring housing is located at the outside of locating dowel.
Preferably, described connection end is in oblateness, including curved curved rotation section and in plane installation portion, On installation portion, the inwall of body shell is provided with the arc with rotation section cooperation to retaining mechanism.
Preferably, described heat gun includes cable, and connection end is provided with the wire lead slot for penetrating for cable, connection end Inwall is provided with the passage for housing cable, and body shell inwall is provided with the limited post for preventing cable from getting loose, fuselage Also include being removably fixed in the pressing plate on limited post top.
Preferably, described heat gun also includes the controlling organization for realizing adjusting function, and controlling organization includes keypad, Keypad includes housing and some buttons being connected to housing, and each button is spaced and is independently distributed in outer inframe.
After technique scheme, the heat gun that this utility model provides has the advantage that:
1st, the heat gun that this utility model provides, head and fuselage are arranged to split-type structural, and head and fuselage rotate Connect, and retaining mechanism is set between head and fuselage, user can be according to service condition and use demand adjustment fuselage and machine Angle between head, improves the versatility of heat gun and property easy to use.
2nd, retaining mechanism includes cage knob, cage knob arranges closing piece, the connection end setting draw-in groove of head shell, on body shell Setting groove, when closing piece is inserted simultaneously in draw-in groove and groove, head and fuselage are in relatively-stationary state, it is to avoid head makes With during rotate with respect to fuselage, impact is normal to be used.
3rd, the quantity of groove is arranged to M times of closing piece quantity, or, the quantity of draw-in groove is arranged to N times of closing piece quantity, just In realizing the adjustment of the multi-angle between head and fuselage, meet different service conditions.
4th, spring catch knob resets, and retaining mechanism overall structure is simple, meets use requirement, head and machine well Be in when relatively rotating state, camber of spring, head and fuselage adjustment terminate after, unclamp cage knob, spring reinstatement process Middle catch knob resets.
5th, the edge of pilot hole is bent to form flange, and the spacing between flange end face and connection end outer wall forms the shifting of cage knob Dynamic stroke, it is to avoid depart from fuselage impact normal use when cage knob is mobile, simultaneously, it is to avoid cage knob shift motion leads to spring when excessive Deformation is excessive and lost efficacy, maintain retaining mechanism effectiveness, thus ensureing the service life of whole machine.
The 6th, locating dowel, the location hole that connection end setting is coordinated with locating dowel are arranged on cage knob, locating dowel is in head and fuselage It is in the state of being relatively fixed or relatively rotate all to be inserted in location hole under state, effectively improve the Assembly stability of cage knob and make With stability, prevent from partially affecting normal use when cage knob is mobile.
7th, connection end is in oblateness, and the inwall of body shell arranges arc, head shell and machine with rotation section cooperation Coordinated by curved surface between body housing, effectively improve head and guidance quality when fuselage relatively rotates, and be effectively ensured head and The stability of connection is rotated between fuselage.
8th, power being used for or transmit signal cable integrated after be stuck between limited post, and by pressing plate spacing, then Cable penetrates in head shell by wire lead slot, and cable is arranged in passage, and the mounting stability of cable is good.Further, since machine When head and fuselage relatively rotate, there is the deformation stretched and bend in cable, and passage is arranged to the shape bending it is ensured that cable has Enough length meets the use requirement rotating adjustment.
9th, on keypad button interval and have independent connections to housing, it is to avoid force in wherein certain button when affect other Button, has using effect, keypad or the entirety preventing button linkage, facilitates implementation quick assembling.
Brief description
Fig. 1 is in schematic diagram during first state for this utility model heat gun embodiment one;
Fig. 2 is in schematic diagram during the second state for this utility model heat gun embodiment one;
Fig. 3 is the axonometric chart of cage knob in this utility model heat gun embodiment one;
Fig. 4 is the schematic diagram of head shell in this utility model heat gun embodiment one;
Fig. 5 a, 5b are the schematic diagram of this utility model heat gun embodiment one middle fuselage housing;
Fig. 6 a, 6b are the schematic diagram of retaining mechanism two states in this utility model heat gun embodiment one;
Fig. 7 is the explosive view of controlling organization in this utility model heat gun embodiment one;
Fig. 8 is the schematic diagram of keypad in this utility model heat gun embodiment one;
Fig. 9 a, 9b are the scheme of installation of cable in this utility model heat gun embodiment one.
In figure, 1- head shell, 11- connection end, 111- rotation section, 112- installation portion, 12- cannelure, 13- boss, 14- Location hole, 15- draw-in groove, 16- stopper slot, 17- cylinder, 171- circular hole, 18- air vent, 19- wire lead slot, 2- body shell, 21- Handle, 22- insulation sleeve, 23- pilot hole, 231- flange, 24- groove, 25- stem stem, 26- baffle plate, 27- storage tank, 28- divulges information Window, 29- arc, 3- switching mechanism, 4- controlling organization, 41- panel, 411- button, 42- display screen, 43- end cap, 431- Key hole, 44- keypad, 441- button, 442- housing, 443- dowel, 5- retaining mechanism, 51 springs, 6- cage knob, 61- locks Block, 62- shrinkage pool, 63- locating dowel, 64- leg, 7- cable, 71- collar, 81- limited post, 82- pressing plate, 83- lead plate, 9- props up Support member.
Specific embodiment
The utility model is described in further detail with specific embodiment below in conjunction with the accompanying drawings.
Embodiment one
As shown in Figure 1, 2, the heat gun that this utility model embodiment one provides, including head and fuselage, head includes machine Casing 1, is provided with motor, fan and heating assembly in head shell 1, fuselage includes body shell 2, and body shell is provided with out Shutting mechanism 3 and controlling organization 4.Head shell 1 and body shell 2 are rotatably connected, head shell 1 and body shell 2 it Between be provided with for making head and fuselage keep relatively-stationary retaining mechanism 5.
Retaining mechanism 5 includes cage knob 6 as shown in Figure 3, and cage knob 6 is in cylinder, and the side wall of cage knob circumference is provided with two Closing piece 61, two closing pieces 61 be located at same radially and be symmetrical arranged, cage knob is axially arranged with the shrinkage pool 62 of a side opening, shrinkage pool 62 Diapire be provided with the locating dowel 63 of protrusion.In order to prevent filling by mistake, the side wall of cage knob 6 circumference is additionally provided with leg 64.
As shown in figure 4, head shell 1 is fixedly connected by securing member by symmetrical two half-shell constituting, head shell Body 1 is provided with the connection end 11 being connected with body shell 2, and connection end 11 is in oblateness, including curved curved rotation section 111 And in plane installation portion 112.
The outer wall of the installation portion 112 of the one of half-shell of head shell 1 is provided with the cannelure 12 with cage knob 6 cooperation, peace Dress portion 112 forms the boss 13 with shrinkage pool 62 cooperation in the part in cannelure 12, and boss 13 is provided with and locating dowel 63 Cooperation location hole 14, cannelure 12 be circumferentially with and closing piece 61 cooperation draw-in groove 15 and with leg 64 cooperation stopper slot 16.In the present embodiment, draw-in groove 15 is provided with two, and two draw-in grooves be located at same radially.
The installation portion 112 of another half-shell of head shell 1 is provided with the cylinder 17 coaxial with boss 13, the axial direction of cylinder 17 Center is provided with circular hole 171.
The connection end 11 of head shell 1 is in plane towards the side wall of body shell 2, and this side wall is provided with for ventilation Air vent 18 and the wire lead slot 19 for penetrating for cable 7.
As Fig. 5 a, 5b, body shell 2 is also fixedly connected by securing member by symmetrical two half-shell and constitutes, fuselage One end of housing 2 is coordinated with the connection end 11 of head shell 1.Body shell 2 is provided with handle 21, and switching mechanism 3 is located at handle On 21, switching mechanism 3 pushes away chip switch using existing, and body shell 2 is additionally provided with the insulation sleeve 22 for installing cable.
The one of half-shell of body shell 2 is provided with the pilot hole 23 for installing cage knob 6, and body shell 2 is located at assembling The inwall of hole 23 circumference is provided with four grooves 24 with closing piece 61 cooperation, and four grooves 24 are symmetrically formed two pair of a groove two-by-two, And the angle α between two pair of a groove centrage is 60 °.Certainly, the angle α between two pair of a groove 24 centrage in the present embodiment Other angles can be arranged to, such as 40 °, 45 °, 50 °, 65 °, 70 ° etc..
Another half-shell of body shell 2 is provided with coaxial with pilot hole 23 and is coordinated with the circular hole 171 on head shell 1 Stem stem 25, the outer baffle plate 26 being circumferentially with a ring shape of stem stem 25, between stem stem 25 periphery wall and baffle plate 26 internal perisporium Space forms the storage tank 27 with cylinder 17 cooperation on head shell 1.
Vent window 28 offered on the end that body shell 2 is connected with head shell 1,2 two half-shell of body shell interior Wall is provided with the arc 29 with rotation section 111 cooperation of connection end 11, the axial line of arc 29, the axle center of rotation section 111 The axial line of line, the axial line of pilot hole 23 and stem stem 25 is located on the same line.
Retaining mechanism 5 also includes spring 51, as shown in Figure 6 a, when head and fuselage are in relatively-stationary state, cage knob 6 On closing piece 61 simultaneously be located at draw-in groove 15 and groove 24 in, head and fuselage relatively unrotatable.Locating dowel 63 is plugged in positioning In hole 14, being positioned partially or entirely in stopper slot 16 of leg 64.Spring 51 is sleeved on the outside of locating dowel 63, and the two of spring 51 End is against on the outer wall of boss 13 and the diapire of shrinkage pool 62 respectively.
For spacing cage knob 6, the circumferential edge of pilot hole 23 bends inwards and forms the flange 231 being used for spacing cage knob 6, lock The upper surface of block 61 is against on 231 bottom surfaces of flange, and spring 51 is in compressive state.
As shown in Figure 6 b, during pressing cage knob 6, spring 51 compression, closing piece 61 completely disengages from groove 24, fuselage with respect to Head is in rotatable state.In order that fuselage can rotate with respect to head, flange 231 bottom surface and connection end 11 outer wall it Between be smaller than closing piece 61 along the length of cage knob 6 axial direction, after the pressurized movement of cage knob 6, closing piece 61 completely disengages from groove 24 and position In draw-in groove 15, closing piece 61 does not cause to the rotation of fuselage to interfere.
Controlling organization 4 is arranged on one end that body shell 2 is connected with head shell 1, as shown in fig. 7, in the present embodiment Controlling organization 4 includes panel 41, display screen 42, end cap 43 and the keypad 44 integrating, and controlling organization passes through end cap 43 and the cooperation of body shell 2 be fixedly arranged on body shell.On panel, 41 are provided with the button 411 for realizing regulation and control, show Display screen 42 is provided with the hole for passing through for button 411, and keypad 44 is provided with button 441 corresponding with button 411, end cap 43 It is provided with the key hole 431 with button 441 cooperation.
As shown in figure 8, keypad 44 also includes the housing 442 positioned at the outer circumference of button 44, each button 441 is spaced and solely Stand and be distributed in housing 442, in the present embodiment, each button 441 is connected to housing 442, outward by least one dowel 443 Frame 442 is arranged to arc outwardly at the position being connected with button 441.Avoid forcing in wherein certain button when impact Other buttons, have using effect, keypad or the entirety preventing button linkage, facilitate implementation quick assembling.
As shown in Fig. 9 a, 9b, integrated with the collar 71 of insulation for conductive or transmission signal cable 7, connect The inwall at end 11 is provided with the passage of accommodating cable, and body shell 2 inwall is provided with the limited post 81 for preventing cable from getting loose, Fuselage also includes being removably fixed in the pressing plate 82 on limited post 81 top.
Specific in the present embodiment, the inwall of connection end 11 is provided with the lead plate 83 of bending, lead plate side wall and connection The space between 11 inwalls is held to form the passage for housing cable 7.
By collar 71, the one end after integrated is stuck between two limited posts 81 cable 7 in body shell 2, and uses pressing plate 82 is spacing, integrated after the wire lead slot 19 that passes through on connection end 11 of the other end penetrate in head and be stuck in lead plate 83 side wall and company Connect between the inwall at end 11.When angle between head and fuselage is less, integrated after cable have fold, when head and fuselage it Between angle increase after, fold opens, and length of cable becomes big, when meeting head and fuselage angle change, length of cable is wanted Ask, it is to avoid cable deformation failure, the whole machine of impact uses.
Using the present embodiment heat gun when, switched on power by switching mechanism 3, wind-force adjusted by controlling organization 4 Size and the height of temperature.Extraneous air self-ventilation window 28, air vent 18 enter in head, after the heat effect of heated assembly Form thermal current to blow out from head.
When needing to adjust the angle between head and fuselage, press cage knob 6, closing piece 61 departs from groove 24, rotate fuselage extremely After correct position, unclamp cage knob 6, spring 51 restores to the original state, and spring catch knob 6 resets, make closing piece 61 be inserted in groove 24 simultaneously In draw-in groove 15, fuselage is fixed with respect to head, completes to adjust.When fuselage rotates, the arc 29 in body shell 2 is along connection On end 11, the outer wall of rotation section 111 moves, and has the position of laminating between arc and rotation section outer wall all the time, is easy to improve head Stability during adjustment.
Certainly, the quantity of the present embodiment further groove 24 can also be arranged to six or eight or ten etc., i.e. groove 24 Quantity can be M times of closing piece 61 quantity, M >=2 and be natural number.The centerlines α of adjacent two pair of a groove can also basis Service condition makes change, meets the use requirement of multi-angle adjustment between head and fuselage.
In addition, the quantity of cage knob 6 upper locking piece 61 can also make change, but it is to ensure that the quantity of closing piece 61 disclosure satisfy that The use requirement of locking between head and fuselage.
Embodiment two
It is in place of the present embodiment and the difference of embodiment one, the quantity of groove 24 is consistent with the quantity of closing piece 61, draw-in groove 15 quantity is N times of closing piece 61 quantity, N >=2 and be natural number, closing piece 61 depart from draw-in groove 15 when head be in rotary state.
In the present embodiment, the two ends of spring 51 are respectively fixedly connected with the outer wall of connection end 11 and the diapire of shrinkage pool 62, When closing piece 61 departs from draw-in groove 15, spring 51 is in extended state.In addition, the spacing between flange 231 bottom surface and connection end 11 outer wall More than or equal to closing piece 61 along cage knob 6 axial direction length, when pulling out cage knob 6, closing piece 61 completely disengages from draw-in groove 15, spring 51 Stretcher strain, head is in rotatable state.After head turns to correct position, unclamp cage knob 6, spring 51 restores to the original state, Catch knob 6 resets, thus driving closing piece to be inserted simultaneously in groove 24 and draw-in groove 15, head and fuselage are relatively fixed.
For the ease of operation, cage knob 6 can arrange draw ring.
Implement row three
It is in place of the present embodiment and the difference of embodiment one, for the ease of using, head shell 1 rotates and is provided with support Part 9, this support member adopts steel wire one brake forming, and head shell 1 is provided with the hole with the cooperation of support member 9 two ends, support member 9 End rotate be plugged in hole.This support member 9 can be used for supporting heat gun it can also be used to hang up heat gun.
In addition to above preferred embodiment, this utility model also has other embodiments, and those skilled in the art can root It is variously modified according to this utility model and deforms, without departing from spirit of the present utility model, this utility model all should be belonged to Scope as defined in the claims.

Claims (10)

1. a kind of heat gun, including head and fuselage it is characterised in that described head includes head shell, sets in head shell There are motor, fan and heating assembly, fuselage includes body shell;Head shell and body shell are rotatably connected, head It is provided between housing and body shell for making head and fuselage keep relatively-stationary retaining mechanism.
2. it is characterised in that described retaining mechanism includes cage knob, cage knob is circumferentially with heat gun according to claim 1 At least one closing piece;Head shell is provided with the connection end with body shell cooperation, and connection end is provided with the draw-in groove with closing piece cooperation;Machine Body housing is provided with the pilot hole for installing cage knob, and body shell is in the groove being circumferentially with closing piece cooperation of pilot hole;Lock Block is inserted in draw-in groove and groove simultaneously makes head and fuselage be relatively fixed.
3. heat gun according to claim 2 is it is characterised in that the quantity of described draw-in groove and the quantity of closing piece are consistent, recessed The quantity of groove is M times of closing piece quantity, M >=2 and be natural number, closing piece depart from groove opportunity be in rotary state;Or, institute The quantity stating groove is consistent with the quantity of closing piece, and the quantity of draw-in groove is N times of closing piece quantity, N >=2 and be natural number, closing piece take off From draw-in groove when head be in rotary state.
4. heat gun according to claim 3 is it is characterised in that described cage knob is circumferentially with two closing pieces, and two locks Block be located at same radially;Two draw-in grooves are arranged with the outer wall of head shell connection end;Body shell is located at pilot hole week To inwall be provided with four or six or eight grooves, and groove is symmetrical two-by-two.
5. heat gun according to claim 3 is it is characterised in that described retaining mechanism also includes resetting for catch knob Spring, cage knob is being provided with shrinkage pool towards the side of connection end;When the quantity of groove is M times of closing piece quantity, the two ends of spring It is against respectively on the outer wall of connection end and the diapire of shrinkage pool, when closing piece departs from groove, spring is in compressive state;Or, draw-in groove When quantity is N times of closing piece quantity, the two ends of spring are individually fixed on the outer wall of connection end and the diapire of shrinkage pool, and closing piece departs from During draw-in groove, spring is in extended state.
6. heat gun according to claim 5 it is characterised in that the circumferential edge of described pilot hole bends inwards, use by formation Flange in spacing cage knob;When the quantity of groove is M times of closing piece quantity, the spacing between flange end face and connection end outer wall is little In closing piece along the axial length of cage knob;Or, when the quantity of draw-in groove is N times of closing piece quantity, flange end face and connection end outer wall Between spacing be more than or equal to closing piece along cage knob axial direction length.
7. heat gun according to claim 6 protrudes it is characterised in that being provided with connection end on the diapire of described shrinkage pool Locating dowel, connection end is provided with location hole, and locating dowel is inserted in location hole, and spring housing is located at the outside of locating dowel.
8. the heat gun according to any one of claim 2-7 is it is characterised in that described connection end is in oblateness, including being in The rotation section of arc-shaped curved surface shape and in plane installation portion, retaining mechanism, on installation portion, the inwall of body shell sets There is the arc with rotation section cooperation.
9. the heat gun according to any one of claim 2-7 is it is characterised in that described heat gun includes cable, connection end It is provided with the wire lead slot for penetrating for cable, the inwall of connection end is provided with the passage of accommodating cable, on body shell inwall It is provided with the limited post for preventing cable from getting loose, fuselage also includes being removably fixed in the pressing plate on limited post top.
10. the heat gun according to any one of claim 1-7 is it is characterised in that described heat gun is also included for realizing The controlling organization of adjusting function, controlling organization includes keypad, and keypad includes housing and some buttons being connected to housing, often Individual button is spaced and is independently distributed in outer inframe.
CN201620914749.1U 2016-08-20 2016-08-20 Hot air gun Active CN205980295U (en)

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CN201620914749.1U CN205980295U (en) 2016-08-20 2016-08-20 Hot air gun

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106679172A (en) * 2016-08-20 2017-05-17 浙江普莱得电器有限公司 Hot air gun

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106679172A (en) * 2016-08-20 2017-05-17 浙江普莱得电器有限公司 Hot air gun

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CP03 "change of name, title or address"
CP03 "change of name, title or address"

Address after: 321035 Industrial Development Zone, Xiaoshun Town, Jindong District, Jinhua City, Zhejiang Province

Patentee after: Zhejiang Prade Electric Co.,Ltd.

Address before: 321035 Zhejiang Prade Electric Appliance Co., Ltd., Xiaoshun Town Industrial Development Zone, Jindong District, Jinhua City, Zhejiang Province

Patentee before: Zhejiang Prulde Electric Appliance Co.,Ltd.