CN204619384U - A kind of toy for launching annular wing - Google Patents
A kind of toy for launching annular wing Download PDFInfo
- Publication number
- CN204619384U CN204619384U CN201520263470.7U CN201520263470U CN204619384U CN 204619384 U CN204619384 U CN 204619384U CN 201520263470 U CN201520263470 U CN 201520263470U CN 204619384 U CN204619384 U CN 204619384U
- Authority
- CN
- China
- Prior art keywords
- wing
- annular
- toy
- annular wing
- wing frame
- 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.)
- Active
Links
Abstract
The utility model relates to launches type toy technical field, being specifically related to a kind of toy for launching annular wing, comprising parts, an annular wing, a wing frame, a propulsion element, a return element and a trigger.A kind of toy for launching annular wing of the present utility model; the structural design of the approximate wing of annular wing makes its flight path close to level; flying quality is superior; the flexible design of annular wing makes it clash into without destructive; safe and reliable; shell protection can effectively prevent each movable part impaired, long service life, the design of return element direct body contact's movable part can be prevented hinder by movable part.
Description
Technical field
The utility model relates to launches type toy technical field, is specifically related to a kind of toy for launching annular wing.
Background technology
Although many years have appearred in the wing of annular, they have not obtained the popularity as other flying toy.This may be the intrinsic safety problem in the comparatively near and occupation mode of the flying distance that overcomes air drag due to wing on heading.
Most known wing is designed to launch with hand, but, launch wing with hand and have many shortcomings: first, effectively launch with hand and usually the scope of application of wing can be placed in outside the ability of accidental player or children, because wing must be had suitable technical ability by effective transmitting and intensity provides the power maintained needed for airfoil flight motion; The second, launch with hand and easily cause safety problem, wing is along abnormal path or be launched with too many energy, adds destructive possibility of clashing into.3rd, launch must use rigid wing with hand, the shock of rigid wing is dangerous large.
Except the movable part by pulling annular wing self or toy, existing toy is not used for mechanism toy being placed in engaged configuration, but, annular wing oneself requirement annular wing is pulled to be rigidity, and pull the moving-member of toy to require movable part to expose, thus there is larger safety problem.
Summary of the invention
In order to overcome the shortcoming and defect existed in prior art, the purpose of this utility model is to provide a kind of toy for launching annular wing, and its annular wing flight path is close to level, flying quality is superior, clash into without destructive, safe and reliable, long service life.
The purpose of this utility model is achieved through the following technical solutions: a kind of toy for launching annular wing, comprising:
One parts;
One annular wing, described annular wing is annular, and described annular wing is flexible, and the cross sectional shape of described annular wing is close with the cross sectional shape of aircraft wing;
One wing frame, described wing frame to be arranged in described parts and to contact the inner surface of described annular wing;
One propulsion element, described propulsion element makes described wing frame accelerate to move to the second place along the primary importance of described parts;
One return element, described return element makes described wing frame move to the primary importance prepared when pulling the trigger along described parts from second place when completing transmitting;
One trigger, described wing frame is remained on primary importance by described trigger, and can discharge described wing frame to allow its primary importance along described parts to move to the second place.
Wherein, described toy also comprises shell, described shell encloses described parts and wing frame between the first position and the second position, a part for described shell can move relative to described parts, so that be loaded on described wing frame by described annular wing, described shell allows wing frame described in visual determination whether to be in selected primary importance or the second place.
Wherein, described wing frame comprises tab, for contacting the first supporting structure and second supporting structure of the inner surface of described annular wing; When the inner surface of described annular wing contacts with described first supporting structure, described first supporting structure contact is maintained roughly symmetrical shape, described second supporting structure contacts the trailing edge of described annular wing, slips away from described wing frame to prevent described annular wing during launching.
Wherein, described first supporting structure comprises multiple rib, and multiple rib stretches out along the axis connecting primary importance and the second place.
Wherein, complete under the state of launching and prepare percussion, described return element is separated with described wing frame.
Wherein, described parts part is between the first position and the second position cylindrical, and described wing frame has the through hole receiving described parts, and described wing frame is arranged between primary importance on described parts and the second place movably.
Wherein, the passage that described parts are provided with the part along its length and arrange, described passage helically extends around described parts.
Wherein, described toy also comprises a pin through one end of described wing frame, described passage and described propulsion element, described propulsion element comprises spring, one end of described spring is attached on described parts, the other end of described spring is attached on described pin, described spring, described wing frame keeps on the part by described pin and described passage, and, when described propulsion element pulls described wing frame to move, described annular wing moves along with described wing frame and rotates under the effect of passage, when described wing frame slows down in the second place, described annular wing overcomes the contact with described wing frame, be launched when forward travel and rotary motion.
Wherein, described toy also comprises the safety element that unscheduled annular wing is launched in a restriction; Described safety element comprises the capping being provided with safety vent, and safety vent is for limiting the size of described annular wing.
The beneficial effects of the utility model are: a kind of toy for launching annular wing of the present utility model; the structural design of the approximate wing of annular wing makes its flight path close to level; flying quality is superior; the flexible design of annular wing makes it clash into without destructive; safe and reliable; shell protection can effectively prevent each movable part impaired, long service life, the design of return element direct body contact's movable part can be prevented hinder by movable part.
Accompanying drawing explanation
Fig. 1 is stereogram of the present utility model.
Fig. 2 is the front view of annular wing.
Fig. 3 is the schematic diagram of annular wing.
Fig. 4 is annular wing compressive deformation schematic diagram.
Fig. 5 is the flight path schematic diagram of annular wing.
Fig. 6 is sectional side elevation of the present utility model.
Fig. 7 is the detailed view of the fore-end of Fig. 6.
Fig. 8 is the sectional view of Fig. 7.
Fig. 9 is the hindfoot portion sectional view of Fig. 6.
Figure 10 is the sectional side elevation being in the toy launching form.
Figure 11 is the front view of the wing frame intercepted along the straight line 11-11 in Figure 10.
Figure 12 is the sectional side elevation being in the toy preparing percussion form.
Figure 13 is the front perspective view of the alternative wing frame of embodiment 2 and 3.
Figure 14 is another front perspective view of the alternative wing frame of embodiment 2 and 3.
Figure 15 is the rear view of the alternative wing frame of embodiment 2 and 3.
Reference numeral is:
20--toy, 58--parts, 200--annular wing,
62--propulsion element, 60--wing frame, 202--inner surface,
38--trigger, 68--passage, 204--outer surface,
206--leading edge, 208--trailing edge, 64--bumper,
106--sliding part, 109--bar, 108--arc tongue,
110--sliding tray, 116--pivot pin, 112--hinge portion,
114--first flange, 118--second flange, 128--the 3rd flange,
113--second alignment pin, 120--edge, 122--bevelled leading edge,
124--thrust, 22--nose, 23--window,
24--handle, 40--first far-end, 42--first indenture,
26--gun stock, 44--second far-end, 47--second indenture,
46--gun stock hole, 28--projection, 48-open slot,
30--fore sight, 32--thorax mouth, 126--thorax mouth return spring,
127--extension, 36--rear sight, 50--hollow pipe,
52--sight hole, 54--cross foresight, 56--chamber,
34--shakes hands, 84--first handle part, 90--second handle part,
86--first extension rod, 88--pulling plug, 92--bellmouth,
78--sells, 94--taper hole leading edge, 96--handle pin,
98--return spring, 100--first end, 104--second end,
102--tenon, 70--tab, 76--surface,
72--rib, 74--rib leading edge, 82--knob,
66--flange, 67--connecting hole, 80--hole,
134--capping, 132-safety vent, 360--first projectile support,
370--first tab, 372--first rib, 380--first hole,
374--first leading edge, 381--first inner surface, 379--brace projections thing,
372a--second rib, 376--first holdback, 376a--second holdback.
Detailed description of the invention
For the ease of the understanding of those skilled in the art, be further described the utility model below in conjunction with embodiment and accompanying drawing 1-15, the content that embodiment is mentioned is not to restriction of the present utility model.
embodiment 1
A kind of toy 20 for launching annular wing of the present embodiment, comprising:
One parts 58;
One annular wing 200, described annular wing 200 is annular, and described annular wing 200 is flexible, and the cross sectional shape of described annular wing 200 is close with the cross sectional shape of aircraft wing;
One wing frame 60, described wing frame 60 to be arranged in described parts 58 and to contact the inner surface 202 of described annular wing 200;
One propulsion element 62, described propulsion element 62 makes described wing frame 60 accelerate to move to the second place along the primary importance of described parts 58;
One return element, described return element makes described wing frame 60 move to the primary importance prepared when pulling the trigger along described parts 58 from second place when completing transmitting;
One trigger 38, described wing frame 60 is remained on primary importance by described trigger 38, and can discharge described wing frame 60 to allow its primary importance along described parts 58 to move to the second place.
In the present embodiment, described annular wing 200 comprises inner surface 202, outer surface 204, leading edge 206 and trailing edge 208.Annular wing 200 is similar to the cylinder of both ends open, and annular wing 200 cross section is similar to the aerofoil section of aircraft wing.This cross section relative centre line Q is symmetrical.Annular wing 200 is flexible, thus reduces the shock of people, object dangerous.The annular wing 200 of this flexibility can rotate and Selfstabilizing around central axis S, rotates the form making annular wing 200 keep roughly symmetrical.Even if this annular wing 200 owing to producing, inappropriately to deposit or other environmental factor and being out of shape, this annular wing 200 also can ensure the stability of launching.
In the present embodiment, described propulsion element 62 comprises makes wing frame 60 at the second place bumper 64 being roughly ring-type slowed down and the spring with two ends, and described bumper 64 is sheathed on the left side of parts 58.Bumper 64 plays a role by blocking the mobile route of wing frame 60, and bumper 64 is made up of whippy material, bears collision performance excellence.
In the present embodiment, described trigger 38 comprises sliding part 106 and hinge portion 112.
Described sliding part 106 comprises bar 109, arc tongue 108, sliding tray 110 and pivot pin 116.The major axis of the bar 109 extended is approximately perpendicular to the tongue 108 of arc, and bar 109 is roughly parallel to the major axis of toy 20.The sliding tray 110 being located at the both sides of bar 109 interacts with the first alignment pin be located in shell, and sliding part 106 can be slided along the long axis direction being roughly parallel to bar 109.
Described hinge portion 112 comprises the first flange 114, second flange 118, the 3rd flange 126 and the second alignment pin 113.Described hinge portion 112 utilizes the second alignment pin 113 to be pivotally mounted on parts 58.Hinge portion 112 is hinged via pivot pin 116 and sliding part 106, make sliding part 106 and hinge portion 112 can around common axis pivotable.When toy 20 is in preparation percussion form, the second flange 118 engages with wing frame 60.Second flange 118 comprises for the bevelled leading edge 122 keeping the edge 120 of wing frame 60 and be obliquely installed for ease of wing frame 60 slips into bonding station.Thrust 124 on 3rd flange 126 engages with the second end 104 of the return spring 98 of trigger 38, makes sliding part 106 and hinge portion 112 remain on the biased form of joint.
In the present embodiment, also comprise shell, described shell encloses described parts 58 and wing frame 60 between the first position and the second position, a part for described shell can move relative to described parts 58, so that be loaded on described wing frame 60 by described annular wing 200, described shell allows wing frame 60 described in visual determination whether to be in selected primary importance or the second place.Described shell will prevent toy 20 to be damaged and prevent movable part 58 from damaging user.Described housing profile is spray gun.
Described shell comprises: be sheathed on the nose 22 of parts 58 left end, for see the internal part 58 of toy 20 window 23, for keeping and locating the handle 24 of toy 20 and gun stock 26 and for irremovable parts such as the projections 28 of depositing annular wing 200, also comprise fore sight 30, for support fore sight 30 and for cover movable part selected by toy 20 thorax mouth 32, for aiming at the rear sight 36 of toy 20.Nose 22, window 23, projection 28, fore sight 30 and thorax mouth 32 are positioned near the F of front end; Gun stock 26 is positioned near the R of rear end; Near handle 24, rear sight 36 and the centre position of trigger 38 between front end F and rear end R.
Described handle 24 and described gun stock 26 are the standing shape things extended, for holding and locating toy 20.Handle 24 has the first far-end 40 and the first indenture 42 widened, the toy 20 so that user holds.Gun stock 26 has the second far-end 44 and the second indenture 47 and gun stock hole 46 widened, so that the toy 20 or under being clipped in arm of holding.
Described projection 28 is provided with open slot 48, projection 28 inner hollow.User compresses annular wing 200 simply makes it slip in projection 28 through open slot 48, after entering the inside of projection 28, annular wing 200 launches and the inwall being resisted against projection 28 is deposited, meanwhile, user can pull annular wing 200 to be taken out through open slot 48 simply.
Described rear sight 36, for being located at the overshooting shape thing on the top of toy 20, aiming at for helping eyes and launches.More specifically, rear sight 36 comprises: for aiming at the hollow pipe 50 of transmitting, hollow pipe 50 is located in the sight hole 52 in rear sight 36, and, support by cross foresight 54.Rear sight 36 mutually can be changed between the length direction of toy 20 and vertical length direction.Described shell also comprises the chamber 56 for receiving rear sight 36 to deposit along toy 20 length direction.
Described fore sight 30 is for being located at the overshooting shape thing at the top of thorax mouth 32.
Described window 23 and thorax mouth 32 can enclose a part for parts 58, wing frame 60 and parts 58 between the first position and the second position.Described thorax mouth 32 is included in the extension 127 used when loading toy 20, and extension 127 extends to the below of window 23 towards gun stock 26 from the below of thorax mouth 32.Thorax mouth 32 can move relative to parts 58, to be more easily loaded on wing frame 60 by annular wing 200.Whether window 23 partially transparent, be loaded with annular wing 200 to allow user's visual determination or whether wing frame 60 is in the first position and the chosen position of in the second place.
Described thorax mouth 32 also comprises the thorax mouth return spring 126 that one end and its underpart are attached, and the other end of thorax mouth return spring 126 is attached on shell.Annular wing 200 after having reprinted described thorax mouth return spring 126 make thorax mouth 32 turn back to original position under its pulling force.
In the present embodiment, described return element is handle 34.Described handle 34 comprises first handle part 84 and the second handle part 90 of the major axis being roughly parallel to parts 58.
Described first handle part 84 comprises the first extension rod 86, and it is attached with the pulling plug 88 that can be used for starting handle 34.First extension rod 86 is arranged on the inside of shell, and the pulling plug 88 that can firmly grasp is located at the outside of shell.
Described second handle part 90 comprises second extension rod for acceptance pin 78 with bellmouth 92.Pin 78 is used for pulling propulsion element 62 with the contact of the taper hole leading edge 94 of bellmouth 92, makes propulsion element 62 change by completing emission state the elongation state preparing to launch into.
Described handle 34 also comprises first handle part 84 and second handle part 90 is connected into holistic handle pin 96 and return spring 98.Handle 34 is operationally connected with wing frame 60, and first end 100, second end 104 of return spring 98 is attached on the thrust 124 of the tenon 102 of second handle part 90, trigger 38.Adopt the design of handle 34 to make user not need directly contact and pull wing frame 60 toy 20 to be in launch standby, security is high.
In the present embodiment, described wing frame 60 comprises tab 70, for contacting the first supporting structure and second supporting structure of the inner surface 202 of described annular wing 200; During contact between the inner surface 202 of described annular wing 200 and described first supporting structure, first supporting structure is maintained roughly symmetrical shape, described second supporting structure contacts the trailing edge 208 of described annular wing 200, slips away from described wing frame 60 to prevent described annular wing 200 during launching.Described second supporting structure also comprises the surface 76 of the major axis being approximately perpendicular to parts 58.When preparing to launch, described tab 70 engages with the hinge portion 112 of trigger 38.
In the present embodiment, described first supporting structure comprises 6 ribs, 72,6 ribs 72 and stretches out along the axis direction connecting primary importance and the second place.Rib has the rib leading edge 74 of inclination, so that be loaded on the rib 72 of wing frame 60 by annular wing 200.Further, a described rib is provided with the front end of inclination, to be loaded on described wing frame 60 by described annular wing 200.
Described rib 72 makes the CONTACT WITH FRICTION between described annular wing 200 and described wing frame 60 minimize, and only need the propulsion element 62 of less intensity just can launch annular wing 200 well, this is especially favourable for children.
In the present embodiment, complete under the state of launching and prepare percussion, described handle 34 is separated with described wing frame 60.Pull pulling plug 88 to make wing frame 60 move to primary importance from the second place, then, described return spring 98 pulls handle 34 to make handle 34 get back to original position, realizes handle 34 and is separated with wing frame 60.Such design can frictional resistance well suffered by reduce engine wing support 60, and make annular wing 200 have larger initial velocity, flying distance is farther.
In the present embodiment, described parts 58 part is between the first position and the second position roughly cylindrical, described wing frame 60 has the through hole receiving described parts 58, and described wing frame 60 is arranged between primary importance on described parts 58 and the second place movably.Described parts 58 also comprise knob 82 for being attached propulsion element 62 and flange 66.The flange 66 of described parts 58 extends along a part for parts 58 length respectively to the top side T of toy 20 and bottom side B.Parts 58 are attached on shell by the connecting hole of 6 in flange 66 67.
In the present embodiment, the passage 68 that described parts 58 are also provided with the part along its length and arrange, described passage helically extends around described parts 58.Described passage 68 makes wing frame 60 be moved to the second place by primary importance and rotate, and drives annular wing 200 to rotate.
In the present embodiment, also comprise a pin 78 through the hole 80 of described wing frame 60, described passage 68 and described propulsion element 62 one end, one end of the spring of described propulsion element 62 is attached on the knob 82 of described parts 58 inside, the other end of described spring is attached on described pin 78, described spring, described wing frame 60 remains on described parts 58 by described pin 78 and described passage 68, and, when described propulsion element 62 pulls described wing frame 60 to move, described annular wing 200 moves along with described wing frame 60 and rotates under the effect of passage 68, when described wing frame 60 slows down in the second place, described annular wing 200 overcomes the contact with described wing frame 60, be launched when forward travel and rotary motion.
In the present embodiment, also comprise the safety element that unscheduled annular wing 200 is launched in a restriction, described safety element; Described safety element is capping 134, described capping 134 is provided with safety vent 132, capping 134 is curling and folding with it to engage with unscheduled annular wing 200 at oneself towards safety vent 132, described safety vent 132 is for limiting the size of annular wing 200, and then prevent unscheduled annular wing 200 to be loaded, safe and reliable.
embodiment 2
The difference of the present embodiment and embodiment 1 is: the first wing frame 360 is similar to wing frame 60, have roughly cylindrical shape, it comprises: the first tab 370 engaged with trigger 28, for supporting outward extending first rib 372 of annular wing 200 and the first hole 380 for acceptance pin 78.In addition, the first rib 372 has the first leading edge 374 of inclination so that load annular wing 200, as the rib 72 in wing frame 60.Described first wing frame 360 also comprises is located at brace projections thing 379 adjacent with the first hole 380 on the first inner surface 381.In addition, the first wing frame 360 has the second rib 372a that 1 the outward extending helical form adjacent with the first tab 370 is arranged, and described second rib 372a spirality is arranged.Described second supporting structure also comprises the first holdback 376, the second holdback 376a be located on the first rib 372, second rib 372a.
embodiment 3
The difference of the present embodiment and embodiment 2 is: the quantity of the second rib 372a is 3.
Above-described embodiment is the utility model preferably implementation, and in addition, the utility model can also realize by alternate manner, and any apparent replacement is all within protection domain of the present utility model without departing from the concept of the premise utility.
Claims (9)
1., for launching a toy for annular wing, it is characterized in that: comprising:
One parts;
One annular wing, described annular wing is annular, and described annular wing is flexible, and the cross sectional shape of described annular wing is close with the cross sectional shape of aircraft wing;
One wing frame, described wing frame to be arranged in described parts and to contact the inner surface of described annular wing;
One propulsion element, described propulsion element makes described wing frame accelerate to move to the second place along the primary importance of described parts;
One return element, described return element makes described wing frame move to the primary importance prepared when pulling the trigger along described parts from second place when completing transmitting;
One trigger, described wing frame is remained on primary importance by described trigger, and can discharge described wing frame to allow its primary importance along described parts to move to the second place.
2. a kind of toy for launching annular wing according to claim 1, it is characterized in that: described toy also comprises shell, described shell encloses described parts and wing frame between the first position and the second position, a part for described shell can move relative to described parts, so that be loaded on described wing frame by described annular wing, described shell allows wing frame described in visual determination whether to be in selected primary importance or the second place.
3. a kind of toy for launching annular wing according to claim 1, is characterized in that: described wing frame comprises tab, for contacting the first supporting structure and second supporting structure of the inner surface of described annular wing; When the inner surface of described annular wing contacts with described first supporting structure, described first supporting structure contact is maintained roughly symmetrical shape, described second supporting structure contacts the trailing edge of described annular wing, slips away from described wing frame to prevent described annular wing during launching.
4. a kind of toy for launching annular wing according to claim 2, is characterized in that: described first supporting structure comprises multiple rib, and multiple rib stretches out along the axis connecting primary importance and the second place.
5. a kind of toy for launching annular wing according to claim 1, is characterized in that: complete under the state of launching and prepare percussion, described return element is separated with described wing frame.
6. a kind of toy for launching annular wing according to claim 1, it is characterized in that: described parts part is between the first position and the second position cylindrical, described wing frame has the through hole receiving described parts, and described wing frame is arranged between primary importance on described parts and the second place movably.
7. a kind of toy for launching annular wing according to claim 1, is characterized in that: the passage that described parts are provided with the part along its length and arrange, and described passage helically extends around described parts.
8. a kind of toy for launching annular wing according to claim 6, is characterized in that: described toy also comprises a pin through one end of described wing frame, described passage and described propulsion element, described propulsion element comprises spring, one end of described spring is attached on described parts, the other end of described spring is attached on described pin, described spring, described wing frame keeps on the part by described pin and described passage, and, when described propulsion element pulls described wing frame to move, described annular wing moves along with described wing frame and rotates under the effect of passage, when described wing frame slows down in the second place, described annular wing overcomes the contact with described wing frame, be launched when forward travel and rotary motion.
9. a kind of toy for launching annular wing according to claim 1, is characterized in that: described toy also comprises the safety element that unscheduled annular wing is launched in a restriction; Described safety element comprises the capping being provided with safety vent, and safety vent is for limiting the size of described annular wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520263470.7U CN204619384U (en) | 2015-04-28 | 2015-04-28 | A kind of toy for launching annular wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520263470.7U CN204619384U (en) | 2015-04-28 | 2015-04-28 | A kind of toy for launching annular wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204619384U true CN204619384U (en) | 2015-09-09 |
Family
ID=54038448
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520263470.7U Active CN204619384U (en) | 2015-04-28 | 2015-04-28 | A kind of toy for launching annular wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204619384U (en) |
-
2015
- 2015-04-28 CN CN201520263470.7U patent/CN204619384U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US7811151B2 (en) | Toy airplane with foldable wings and a switch to activate a plane propeller | |
| US5129852A (en) | Toy airplane launcher and winder | |
| US2593979A (en) | Tethered toy airplane | |
| US4159087A (en) | Glider kite | |
| CN204619384U (en) | A kind of toy for launching annular wing | |
| CN204619386U (en) | A kind of toy for launching projectile | |
| US2780422A (en) | Flying aircraft carrier | |
| US2765582A (en) | Toy folding wing glider and launcher | |
| US8764506B2 (en) | Manually pivoting wings on a toy airplane | |
| US2145972A (en) | Aerial toy | |
| US4997401A (en) | Aerial toy | |
| US2879999A (en) | Aerial tow target | |
| US8382547B2 (en) | Toy projectile and launcher | |
| US1647619A (en) | Airplane | |
| CN102961878A (en) | Reconfigurable toy vehicle | |
| CN204535550U (en) | A kind of heavy integral type laser catapult | |
| US3430562A (en) | Aircraft bomb | |
| US1541579A (en) | Toy aeroplane and launching device therefor | |
| KR200281724Y1 (en) | Launcher with Air Craft | |
| CN204085335U (en) | A kind of folding guided missile shackle structure | |
| CN205425967U (en) | Air gun feeding firing mechanism | |
| US5364298A (en) | Toy airplane launcher and winder | |
| US1280803A (en) | Combined sky-rocket and aeroplane. | |
| KR20220000178U (en) | Toy of Projectile Launcher for Education | |
| CN105346726A (en) | Space sharing scheme of fuel tanks and built-in bomb bay |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170804 Address after: 523000 A, block 34, Golden River Road, Jinhe community, Zhangmutou town, Dongguan, Guangdong, 401 Patentee after: Surfing Dragon Sports Technology (Dongguan) Co., Ltd. Address before: 523000 Guangdong Province, Dongguan City Zhangmutou Jinhe community Jinhe Road No. 34 Co-patentee before: Grammeter Ah Co., Ltd Patentee before: Dongguan City Nuo Feng Industrial Co., Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210813 Address after: 523000 No. 34, Jinhe Road, Zhangmutou town, Dongguan City, Guangdong Province Patentee after: Guangdong Nuofeng Technology Co.,Ltd. Address before: 401, block a, 34 Jinhe Road, Jinhe community, Zhangmutou town, Dongguan City, Guangdong Province 523000 Patentee before: SURF DRAGONS SPORTS TECHNOLOGY (DONGGUAN) Co.,Ltd. |