CN213667913U - Superman aircraft capable of catapulting and flying - Google Patents

Superman aircraft capable of catapulting and flying Download PDF

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Publication number
CN213667913U
CN213667913U CN202022780908.2U CN202022780908U CN213667913U CN 213667913 U CN213667913 U CN 213667913U CN 202022780908 U CN202022780908 U CN 202022780908U CN 213667913 U CN213667913 U CN 213667913U
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China
Prior art keywords
mounting hole
superman
aircraft
limiting
fixedly mounted
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CN202022780908.2U
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Chinese (zh)
Inventor
李文艳
谭嘉伟
吴龙传
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Guangdong Lingzhirui Cultural Entertainment Co ltd
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Guangdong Lingzhirui Cultural Entertainment Co ltd
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Abstract

The utility model discloses a superman aircraft of ejectable flight, the on-line screen storage device comprises a base, the up end fixed mounting of base has the fixing base, the top of fixing base is provided with super human body, first mounting hole has been seted up to the bottom of super human body. This can launch super man-made aircraft of flight, first switch can promote the check lock lever and move left, the motion of check lock lever can drive spacing dish and move left, check lock lever and fourth mounting hole separation this moment, two first springs can promote first lift post upward movement, first lift post upward movement can be with power transmission to super man body on, and then realize launching of super man body, the second switch can be with power transmission to the shell fragment on, when shell fragment and limiting plate separation, the aircraft can be promoted to the spring three and expand, at the in-process of the motion of transfer line two, slider and spout can carry on spacingly to transfer line two, ensure that transfer line two can not take place the skew, and reasonable design, and easy operation.

Description

Superman aircraft capable of catapulting and flying
Technical Field
The utility model relates to a toy technical field specifically is a superman aircraft of ejectable flight.
Background
The doll products are derived from animation films, cartoon books and periodicals, and character images of online tours in the United states, Japan, Korea and the like, and are original cartoon animals, cartoon characters and physical images, the excellent toys are different from the toy concept in the traditional sense, and the toys have cultural connotation, are rich in story line, and are rich in individuality and humanization concept.
But the public young toy of present majority does not have the ejectable base, can not launch, and the object for appreciation nature is lower, and the public young toy of present majority also does not set up the aircraft that can expand, and the function is too single, and the object for appreciation nature is lower, and the design is unreasonable, is not convenient for use.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a can launch super man's aircraft of flight to it does not have the ejection base to provide the public young toy of present majority in solving above-mentioned background art, can not launch, and the object for appreciation nature is lower, and the public young aircraft that also does not set up and can launch of present majority toy, and the function is too single, and the object for appreciation nature is lower, and the design is unreasonable, the problem of being not convenient for use.
In order to achieve the above object, the utility model provides a following technical scheme: a superman aircraft capable of catapulting and flying comprises a base, wherein a fixed seat is fixedly mounted on the upper end face of the base, a superman body is arranged above the fixed seat, a first mounting hole is formed in the bottom of the superman body, four suckers are fixedly mounted at the bottom of the base, a second mounting hole is formed in the upper end face of the fixed seat, a first fixed plate is arranged inside the second mounting hole, a first lifting column is fixedly mounted on the upper end face of the first fixed plate, two first limiting columns and a second lifting column are fixedly mounted at the bottom of the first fixed plate, a first spring is arranged on the outer sides of the first limiting columns, a sliding groove is formed in the bottom of the second mounting hole, a limiting block is fixedly mounted at the bottom of the second lifting column, a third mounting hole is formed in the right side of the limiting block, and a limiting disc is arranged inside the third mounting hole, a second limiting column is fixedly mounted on the left side of the second limiting column, a second spring is arranged on the outer side of the second limiting column, a locking rod is fixedly mounted on the right side of the second limiting column, a fourth mounting hole is formed in the right side of the fixing seat, a first transmission rod is arranged in the fourth mounting hole, a first switch is fixedly mounted at one end, away from the locking rod, of the first transmission rod, a transmission disc is fixedly mounted at one end, close to the locking rod, of the first transmission rod, a fifth mounting hole is formed in the rear end face of the super-person body, a backpack is arranged on the rear end face of the super-person body, a fixed column is fixedly mounted at one side, close to the super-person body, of the backpack, a second switch is arranged at one side, away from the super-person body, of the backpack, a second fixing plate is fixedly mounted in the backpack, a second, two sixth mounting holes and chutes are formed in the outer side of the second fixing plate, a third spring is arranged at one end, close to the sixth mounting hole, of the second transmission rod, a sliding block is fixedly mounted on one side of the second transmission rod, an elastic sheet is fixedly mounted on the other side of the second transmission rod, and a limiting plate is fixedly mounted at one end, far away from the third spring, of the sixth mounting hole.
Preferably, the lower ends of the first fixing plate and the first lifting column are located inside the second mounting hole, the lower ends of the first fixing plate and the first lifting column are in sliding connection with the second mounting hole, and the outer diameter of the first lifting column is equal to the inner diameter of the first mounting hole.
Preferably, the first limiting column and the first spring are symmetrically distributed on the left side and the right side of the second lifting column, and the lower end of the second lifting column extends to the inside of the sliding groove.
Preferably, spacing dish, spacing post two and second spring all are located the inside of third mounting hole, spacing dish, spacing post two and second spring are sliding connection with the third mounting hole, the one end that spacing dish was kept away from to the check lock lever is the ball form.
Preferably, the outer diameter of the fixed column is equal to the inner diameter of the fifth mounting hole, the fixed column is in sliding connection with the fifth mounting hole, two transmission rods and two aircrafts are arranged, and the two transmission rods and the aircrafts are symmetrically distributed on the left side and the right side of the backpack.
Preferably, the lower end of the sliding block is located inside the sliding groove, the sliding block is in sliding connection with the sliding groove, the elastic sheet is clamped with the limiting plate, and the lower end of the second switch is in contact connection with the elastic sheet.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the superman aircraft capable of catapulting and flying comprises a superman body, a first fixing plate, a first lifting column, a first spring, a second lifting column, a limiting block, a third mounting hole, a limiting disc, a second limiting column, a second spring, a first transmission rod, a first switch, a transmission disc and a locking rod, wherein the first switch can transmit power to the first transmission rod through the mutual matching of the superman body, the first transmission rod can transmit the power to the transmission disc, the transmission disc can push the locking rod to move leftwards, the limiting disc can be driven to move leftwards through the movement of the locking rod leftwards, the locking rod is separated from a fourth mounting hole at the moment, when the locking rod is separated from the fourth mounting hole, the two first springs can push the first fixing plate to move upwards through the fixing plate, the first fixing plate can drive the first lifting column to move upwards, the first lifting column can transmit the power to the superman body through the upward movement of the first lifting column, the ejection of the superman body is realized, the operation is simple, the design is reasonable, and the playability is high;
2. this can launch super-human aircraft of flight, in the use device's in-process, through the second switch, transfer line two, the sixth mounting hole, the spout, the slider, the shell fragment, spring three, mutually support of aircraft and limiting plate, the second switch can be with power transmission to the shell fragment, shell fragment and limiting plate separation this moment, when shell fragment and limiting plate separation, spring three can promote transfer line two and move, the motion that utilizes transfer line two can drive the aircraft and expand, at the in-process of transfer line two motions, slider and spout can carry on spacingly to transfer line two, ensure that transfer line two can not take place the skew, and reasonable design, and easy operation.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the back structure of the superman body of the present invention;
FIG. 3 is a schematic view of the front structure of the superman body of the present invention;
FIG. 4 is a schematic view of the sectional structure of the fixing base of the present invention;
FIG. 5 is a schematic top view of the backpack of the present invention;
FIG. 6 is a schematic view of the cross-sectional structure of the backpack of the present invention;
FIG. 7 is an enlarged schematic view of the structure at A in FIG. 4 according to the present invention;
fig. 8 is an enlarged schematic view of the structure at B in fig. 6 according to the present invention.
In the figure: 1. a base; 2. a fixed seat; 3. a superman body; 4. a first mounting hole; 5. a suction cup; 6. a second mounting hole; 7. a first fixing plate; 8. a first lifting column; 9. a first limiting column; 10. a first spring; 11. a second lifting column; 12. a sliding groove; 13. a limiting block; 14. a third mounting hole; 15. a limiting disc; 16. a second limiting column; 17. a second spring; 18. a first transmission rod; 19. a first switch; 20. a drive plate; 21. a fourth mounting hole; 22. a fifth mounting hole; 23. a backpack; 24. fixing a column; 25. a second switch; 26. a second fixing plate; 27. a second transmission rod; 28. a sixth mounting hole; 29. a chute; 30. a slider; 31. a spring plate; 32. a third spring; 33. an aircraft; 34. a limiting plate; 35. a locking lever.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-8, the present invention provides a technical solution: a superman aircraft capable of catapulting and flying comprises a base 1, wherein a fixed seat 2 is fixedly installed on the upper end face of the base 1, a superman body 3 is arranged above the fixed seat 2, a first installation hole 4 is formed in the bottom of the superman body 3, four suckers 5 are fixedly installed at the bottom of the base 1, a second installation hole 6 is formed in the upper end face of the fixed seat 2, a first fixing plate 7 is arranged inside the second installation hole 6, a first lifting column 8 is fixedly installed on the upper end face of the first fixing plate 7, two first limiting columns 9 and a second lifting column 11 are fixedly installed at the bottom of the first fixing plate 7, a first spring 10 is arranged on the outer side of each first limiting column 9, a sliding groove 12 is formed in the bottom of the second installation hole 6, a limiting block 13 is fixedly installed at the bottom of each second lifting column 11, a third installation hole 14 is formed in the right side of each limiting block 13, a limiting disc 15 is arranged inside, a second limiting column 16 is fixedly installed on the left side of the limiting disc 15, a second spring 17 is arranged on the outer side of the second limiting column 16, a locking rod 35 is fixedly installed on the right side of the limiting disc 15, a fourth installation hole 21 is formed in the right side of the fixing seat 2, a first transmission rod 18 is arranged inside the fourth installation hole 21, a first switch 19 is fixedly installed at one end, away from the locking rod 35, of the first transmission rod 18, a transmission disc 20 is fixedly installed at one end, close to the locking rod 35, of the first transmission rod 18, a fifth installation hole 22 is formed in the rear end face of the super-person body 3, a backpack 23 is arranged on the rear end face of the super-person body 3, a fixing column 24 is fixedly installed at one face, close to the super-person body 3, of the backpack 23, a second switch 25 is arranged at one face, away from the super-person body 3, a second fixing plate 26 is fixedly installed inside the backpack 23, two sixth mounting holes 28 and a sliding groove 29 are formed in the outer side of the second fixing plate 26, a third spring 32 is arranged at one end, close to the sixth mounting hole 28, of the second transmission rod 27, a sliding block 30 is fixedly mounted on one surface of the second transmission rod 27, an elastic sheet 31 is fixedly mounted on the other surface of the second transmission rod 27, and a limiting plate 34 is fixedly mounted at one end, far away from the third spring 32, of the sixth mounting hole 28.
Furthermore, the lower ends of the first fixing plate 7 and the first lifting column 8 are located inside the second mounting hole 6, the lower ends of the first fixing plate 7 and the first lifting column 8 are slidably connected with the second mounting hole 6, the outer diameter of the first lifting column 8 is equal to the inner diameter of the first mounting hole 4, in the process of using the device, a worker inserts the first mounting hole 4 below the superman body 3 into the upper end face of the first lifting column 8, at the moment, the worker can press the first switch 19, the first switch 19 can transmit power to the first transmission rod 18, the first transmission rod 18 can transmit the power to the transmission disc 20, the transmission disc 20 can push the locking rod 35 to move leftwards, the limiting disc 15 can be driven to move leftwards by the movement of the leftward locking rod 35, at the moment, the locking rod 35 is separated from the fourth mounting hole 21, when the locking rod 35 is separated from the fourth mounting hole 21, the two first springs 10 can push the first fixing plate 7 to move upwards, utilize fixed plate 7 upward movement, fixed plate 7 can drive first lift post 8 upward movement, utilizes first lift post 8 upward movement can be with power transmission to superman body 3 on, and then realizes superman body 3's ejection.
Furthermore, the first limiting column 9 and the first spring 10 are symmetrically distributed on the left side and the right side of the second lifting column 11, the lower end of the second lifting column 11 extends to the inside of the sliding groove 12, and in the process of using the device, the power can be transmitted to the first fixing plate 7 through the two first springs 10, so that ejection of the device is achieved.
Further, spacing dish 15, spacing post two 16 and second spring 17 all are located the inside of third mounting hole 14, spacing dish 15, spacing post two 16 and second spring 17 are sliding connection with third mounting hole 14, the one end that spacing dish 15 was kept away from to check lock lever 35 is the ball form, at the in-process of user equipment, utilize spacing dish 15 to carry on spacingly to spacing post two 16, effectively avoid second spring 17 to take place to break away from, the frictional force of check lock lever 35 and sliding tray 12 is reduced greatly to the check lock lever 35 that utilizes the ball form, and reasonable design is convenient for use.
Further, the outer diameter of the fixing column 24 is equal to the inner diameter of the fifth mounting hole 22, the fixing column 24 is in sliding connection with the fifth mounting hole 22, the number of the transmission rods 27 and the number of the aircraft 33 are two, the transmission rods 27 and the aircraft 33 are symmetrically distributed on the left side and the right side of the backpack 23, and in the using process of the device, a worker can insert the fixing column 24 into the fifth mounting hole 22, so that the fixing and limiting of the superman body 3 on the backpack 23 are achieved.
Further, the lower extreme of slider 30 is located the inside of spout 29, slider 30 is sliding connection with spout 29, shell fragment 31 and the mutual block of limiting plate 34, the lower extreme and the shell fragment 31 of second switch 25 are connected for the contact, in the in-process of user equipment, the staff can press second switch 25, second switch 25 downstream this moment, utilize second switch 25 downstream to press shell fragment 31, the left end and the limiting plate 34 of shell fragment 31 break away from completely this moment, spring three 32 can be with power transmission to transfer line two 27 this moment, the motion that utilizes two transfer lines two 27 can drive two aircraft 33 and outwards move, and then realize the expansion of aircraft 33, and is easy to operate, and reasonable design, and convenient to use.
The working principle is as follows: firstly, in the process of using the device, a worker inserts the first mounting hole 4 under the superman body 3 into the upper end face of the first lifting column 8, at the moment, the worker can press the first switch 19, the first switch 19 can transmit power to the first transmission rod 18, the first transmission rod 18 can transmit power to the transmission disc 20, the transmission disc 20 can push the locking rod 35 to move leftwards, the limiting disc 15 can be driven to move leftwards by the movement of the leftward locking rod 35, the locking rod 35 is separated from the fourth mounting hole 21, when the locking rod 35 is separated from the fourth mounting hole 21, the two first springs 10 can push the first fixing plate 7 to move upwards, the first fixing plate 7 can drive the first lifting column 8 to move upwards by the movement of the first fixing plate 7, the power can be transmitted to the superman body 3 by the upward movement of the first lifting column 8, and then the superman ejection of the superman body 3 is realized, the staff can press second switch 25, and second switch 25 downstream this moment utilizes second switch 25 downstream to press shell fragment 31, and the left end and the limiting plate 34 of shell fragment 31 break away from completely, and three 32 springs can drive power transmission to transfer line two 27 on, and the motion that utilizes two transfer lines two 27 can drive two aircraft 33 outward movements, and then realizes the expansion of aircraft 33, easy operation, and reasonable in design, convenient to use.
It should be finally noted that the above only serves to illustrate the technical solution of the present invention, and not to limit the scope of the present invention, and that simple modifications or equivalent replacements performed by those skilled in the art to the technical solution of the present invention do not depart from the spirit and scope of the technical solution of the present invention.

Claims (6)

1. The utility model provides a superman aircraft that can launch flight, includes base (1), its characterized in that: a fixing seat (2) is fixedly mounted on the upper end face of the base (1), a superman body (3) is arranged above the fixing seat (2), a first mounting hole (4) is formed in the bottom of the superman body (3), four suckers (5) are fixedly mounted on the bottom of the base (1), a second mounting hole (6) is formed in the upper end face of the fixing seat (2), a first fixing plate (7) is arranged inside the second mounting hole (6), a first lifting column (8) is fixedly mounted on the upper end face of the first fixing plate (7), two first limiting columns (9) and a second lifting column (11) are fixedly mounted at the bottom of the first fixing plate (7), a first spring (10) is arranged on the outer side of the first limiting column (9), a sliding groove (12) is formed in the bottom of the second mounting hole (6), a limiting block (13) is fixedly mounted at the bottom of the second lifting column (11), a third mounting hole (14) is formed in the right side of the limiting block (13), a limiting disc (15) is arranged inside the third mounting hole (14), a limiting column II (16) is fixedly mounted on the left side of the limiting disc (15), a second spring (17) is arranged on the outer side of the limiting column II (16), a locking rod (35) is fixedly mounted on the right side of the limiting disc (15), a fourth mounting hole (21) is formed in the right side of the fixing seat (2), a first transmission rod (18) is arranged inside the fourth mounting hole (21), a first switch (19) is fixedly mounted at one end, away from the locking rod (35), of the first transmission rod (18), a transmission disc (20) is fixedly mounted at one end, close to the locking rod (35), of the first transmission rod (18), a fifth mounting hole (22) is formed in the rear end face of the superman body (3), and a backpack (23) is arranged on the rear end face of the superman, a fixed column (24) is fixedly arranged on one side of the backpack (23) close to the superman body (3), a second switch (25) is arranged on one side of the backpack (23) far away from the superman body (3), a second fixing plate (26) is fixedly arranged in the backpack (23), a second transmission rod (27) is arranged on the outer side of the second fixing plate (26), an aircraft (33) is fixedly arranged at one end of the second transmission rod (27) far away from the backpack (23), two sixth mounting holes (28) and sliding grooves (29) are formed in the outer side of the second fixing plate (26), a third spring (32) is arranged at one end of the second transmission rod (27) close to the sixth mounting hole (28), one surface of the second transmission rod (27) is fixedly provided with a sliding block (30), the other surface of the second transmission rod (27) is fixedly provided with an elastic sheet (31), and a limiting plate (34) is fixedly mounted at one end, far away from the third spring (32), of the sixth mounting hole (28).
2. The catapult-assisted flying superman aircraft as claimed in claim 1, wherein: the lower extreme of fixed plate (7) and first lift post (8) all is located the inside of second mounting hole (6), the lower extreme and second mounting hole (6) of fixed plate (7) and first lift post (8) are sliding connection, the external diameter of first lift post (8) equals the internal diameter of first mounting hole (4).
3. The catapult-assisted flying superman aircraft as claimed in claim 1, wherein: spacing post (9) and first spring (10) equal symmetric distribution are in the left and right sides of second lift post (11), the lower extreme of second lift post (11) extends to the inside that has sliding tray (12).
4. The catapult-assisted flying superman aircraft as claimed in claim 1, wherein: spacing dish (15), spacing post two (16) and second spring (17) all are located the inside of third mounting hole (14), spacing dish (15), spacing post two (16) and second spring (17) are sliding connection with third mounting hole (14), the one end that spacing dish (15) were kept away from in check lock lever (35) is the orbed.
5. The catapult-assisted flying superman aircraft as claimed in claim 1, wherein: the outer diameter of the fixed column (24) is equal to the inner diameter of the fifth mounting hole (22), the fixed column (24) is in sliding connection with the fifth mounting hole (22), two transmission rods (27) and two aircrafts (33) are arranged, and the two transmission rods (27) and the aircrafts (33) are symmetrically distributed on the left side and the right side of the backpack (23).
6. The catapult-assisted flying superman aircraft as claimed in claim 1, wherein: the lower end of the sliding block (30) is located inside the sliding groove (29), the sliding block (30) is in sliding connection with the sliding groove (29), the elastic sheet (31) is clamped with the limiting plate (34), and the lower end of the second switch (25) is in contact connection with the elastic sheet (31).
CN202022780908.2U 2020-11-26 2020-11-26 Superman aircraft capable of catapulting and flying Active CN213667913U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202022780908.2U CN213667913U (en) 2020-11-26 2020-11-26 Superman aircraft capable of catapulting and flying

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202022780908.2U CN213667913U (en) 2020-11-26 2020-11-26 Superman aircraft capable of catapulting and flying

Publications (1)

Publication Number Publication Date
CN213667913U true CN213667913U (en) 2021-07-13

Family

ID=76736104

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202022780908.2U Active CN213667913U (en) 2020-11-26 2020-11-26 Superman aircraft capable of catapulting and flying

Country Status (1)

Country Link
CN (1) CN213667913U (en)

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