CN214796465U - Hand-throwing rotary airplane for teaching demonstration - Google Patents
Hand-throwing rotary airplane for teaching demonstration Download PDFInfo
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- CN214796465U CN214796465U CN202121149090.2U CN202121149090U CN214796465U CN 214796465 U CN214796465 U CN 214796465U CN 202121149090 U CN202121149090 U CN 202121149090U CN 214796465 U CN214796465 U CN 214796465U
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Abstract
The utility model discloses a teaching demonstration is with throwing formula of circling round aircraft, it includes fuselage, wing and fin, and its fuselage includes fuselage front bezel, regulating plate and fuselage back plate, and the regulating plate is connected between fuselage front bezel and fuselage back plate, and the regulating plate is the flexible structure, and the wing includes wing root and wing tip, and the both ends at wing root are connected to the wing tip, and the fin includes fin root and fin tip. The beneficial effects of the utility model are that: the angles of the front plate and the rear plate of the body can be adjusted through the wings and the empennage to realize different modes of flight, so that the interestingness is greatly improved; the user learns the influence of the angles of the wings, the empennage and the fuselage on the flight path and teaches through lively activities; simple structure, the equipment is convenient, and is with low costs.
Description
Technical Field
The utility model relates to a hand is thrown formula of circling round aircraft for teaching demonstration belongs to teaching aircraft model technical field.
Background
The hand throwing airplane is an airplane which can fly after being thrown out of hands, has simple structure and simple playing method, can be recycled, is popular with children, but has single playing method of the prior hand throwing airplane. The patent 2018211303478 entitled "a hand throwing aircraft" discloses a hand throwing aircraft which is connected at different positions through wings and empennages to achieve the purpose of different flight modes, but can only be switched among a limited number of fixed flight modes, and the aerodynamics principle of the hand throwing aircraft cannot be well understood by users in the using process.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model lies in providing a hand throwing convolution type aircraft for teaching demonstration, and the flight of different modes is realized to the angle of this aircraft accessible wing, fin, regulation fuselage front bezel and fuselage back plate, has improved the interest greatly, can make the user learn the influence of wing, fin, fuselage angle to the flight orbit simultaneously, and the lively education is in happy.
The utility model discloses a following scheme realizes: the utility model provides a teaching demonstration is with throwing formula of circling round aircraft, the wing with the fin passes respectively the fuselage, it includes fuselage, wing and fin, and its fuselage includes fuselage front bezel, regulating plate and fuselage back plate, the regulating plate is connected the fuselage front bezel with between the fuselage back plate, the regulating plate is flexible structure, the wing includes wing root and wing tip, the wing tip is connected the both ends of wing root, the wing tip is the structure of can kicking up, the fin includes fin root and fin tip, fin tip is connected the both ends of fin root, fin tip is the structure of kicking up.
The adjusting plate rotates left and right in the horizontal direction, and then drives the machine body rear plate to rotate left and right.
The angle of the adjusting plate rotating leftwards or rightwards is 0-90 degrees.
The angle of the adjusting plate rotating leftwards or rightwards is 0-60 degrees.
The angle of the adjusting plate rotating leftwards or rightwards is 0-30 degrees.
The angle of the adjusting plate rotating leftwards or rightwards is 0-15 degrees.
The angle of upward rotation of the wing tip of the wing and the wing tip of the tail wing is 0 to 90 degrees.
The upward rotating angle of the wing end of the wing and the wing end of the tail wing is 0-60 degrees.
The angle of upward rotation of the wing tip of the wing and the wing tip of the empennage is 0-30 degrees.
The upward rotating angle of the wing end of the wing and the wing end of the tail wing is 0-15 degrees.
The utility model has the advantages that:
1. the hand-thrown rotary type airplane for teaching demonstration can realize the flight in different modes by the angles of the wings, the empennage and the adjusting front plate and the back plate of the airplane body, thereby greatly improving the interestingness;
2. the utility model relates to a hand-thrown rotary aircraft for teaching demonstration, which enables a user to learn the influence of wings, empennage and fuselage angle on flight trajectory, and teaches through lively activities;
3. the utility model relates to a hand is thrown formula of circling round aircraft for teaching demonstration simple structure, and the equipment is convenient, and is with low costs.
Drawings
Fig. 1 is the utility model discloses a teaching demonstration is with overlooking the structural schematic diagram of formula aircraft of throwing circle with hand.
Fig. 2 is the utility model relates to a teaching demonstration is with fuselage of throwing formula of circling round aircraft and is looked sideways at structural schematic.
In the figure: the airplane comprises a fuselage 1, wings 2, empennages 3, a fuselage front plate 4, an adjusting plate 5, a fuselage rear plate 6, wing roots 7, wing tips 8, empennage roots 9 and empennage tips 10.
Detailed Description
The present invention will be further described with reference to fig. 1, but the scope of the present invention is not limited to the description.
In which like parts are designated by like reference numerals. It is noted that the terms "front," "back," "left," "right," "upper" and "lower" used in the following description refer to directions in the drawings, the terms "inner" and "outer" refer to directions toward and away from, respectively, the geometric center of a particular component, and the drawings are in greatly simplified form and employ non-precise ratios, merely for the purpose of facilitating and distinctly aiding in the description of the embodiments of the present invention.
In the following description, for purposes of clarity, not all features of an actual implementation are described, well-known functions or constructions are not described in detail since they would obscure the invention with unnecessary detail, it being understood that in the development of any actual embodiment, numerous implementation details must be set forth in order to achieve the developer's specific goals, such as compliance with system-related and business-related constraints, changing from one implementation to another, and it being recognized that such development efforts may be complex and time consuming, but would nevertheless be a routine undertaking for those of ordinary skill in the art.
Example 1: a hand-thrown rotary type airplane for teaching demonstration, which comprises a fuselage 1, wings 2 and a tail 3, wherein the wings 2 and the tail 3 respectively penetrate through the fuselage 1, the fuselage 1 comprises a fuselage front plate 4, an adjusting plate 5 and a fuselage rear plate 6, the adjusting plate 5 is connected between the fuselage front plate 4 and the fuselage rear plate 6, the adjusting plate 5 is of a bendable structure, the wing 2 comprises a wing root 7 and a wing tip 8, the wing tip 8 is connected at two ends of the wing root 7, the wing tip 8 is of an upwardly bendable structure, the tail 3 comprises a tail root 9 and a tail tip 10, the tail tip 10 is connected at two ends of the tail root 9, the tail tip 10 is of an upwardly bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction, and then the rear plate 6 of the motor body is driven to rotate left and right, the angle of leftward rotation of the adjusting plate 5 is 90 degrees, and the angle of upward rotation of the wing tip 8 and the tail wing tip 10 is 90 degrees.
Example 2: a hand-thrown rotary type airplane for teaching demonstration, which comprises a fuselage 1, wings 2 and a tail 3, wherein the wings 2 and the tail 3 respectively penetrate through the fuselage 1, the fuselage 1 comprises a fuselage front plate 4, an adjusting plate 5 and a fuselage rear plate 6, the adjusting plate 5 is connected between the fuselage front plate 4 and the fuselage rear plate 6, the adjusting plate 5 is of a bendable structure, the wing 2 comprises a wing root 7 and a wing tip 8, the wing tip 8 is connected at two ends of the wing root 7, the wing tip 8 is of an upwardly bendable structure, the tail 3 comprises a tail root 9 and a tail tip 10, the tail tip 10 is connected at two ends of the tail root 9, the tail tip 10 is of an upwardly bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction, further, the rear plate 6 of the body is rotated left and right, the angle of rotation of the adjusting plate 5 to the right is 90 degrees, and the angle of rotation of the wing tip 8 and the tail wing tip 10 to the up is 90 degrees.
Example 3: a hand-thrown rotary type airplane for teaching demonstration, which comprises a fuselage 1, wings 2 and a tail 3, wherein the wings 2 and the tail 3 respectively penetrate through the fuselage 1, the fuselage 1 comprises a fuselage front plate 4, an adjusting plate 5 and a fuselage rear plate 6, the adjusting plate 5 is connected between the fuselage front plate 4 and the fuselage rear plate 6, the adjusting plate 5 is of a bendable structure, the wing 2 comprises a wing root 7 and a wing tip 8, the wing tip 8 is connected at two ends of the wing root 7, the wing tip 8 is of an upwardly bendable structure, the tail 3 comprises a tail root 9 and a tail tip 10, the tail tip 10 is connected at two ends of the tail root 9, the tail tip 10 is of an upwardly bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction, and then the rear plate 6 of the motor body is driven to rotate left and right, the angle of leftward rotation of the adjusting plate 5 is 60 degrees, and the angle of upward rotation of the wing tip 8 and the tail wing tip 10 is 60 degrees.
Example 4: a hand-thrown rotary type airplane for teaching demonstration, which comprises a fuselage 1, wings 2 and a tail 3, wherein the wings 2 and the tail 3 respectively penetrate through the fuselage 1, the fuselage 1 comprises a fuselage front plate 4, an adjusting plate 5 and a fuselage rear plate 6, the adjusting plate 5 is connected between the fuselage front plate 4 and the fuselage rear plate 6, the adjusting plate 5 is of a bendable structure, the wing 2 comprises a wing root 7 and a wing tip 8, the wing tip 8 is connected at two ends of the wing root 7, the wing tip 8 is of an upwardly bendable structure, the tail 3 comprises a tail root 9 and a tail tip 10, the tail tip 10 is connected at two ends of the tail root 9, the tail tip 10 is of an upwardly bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction, further, the rear plate 6 with the fuselage is rotated left and right, the angle of rotation of the adjusting plate 5 to the right is 60 degrees, and the angle of rotation of the wing tip 8 and the tail wing tip 10 to the up is 60 degrees.
Example 5: a hand-thrown rotary type airplane for teaching demonstration, which comprises a fuselage 1, wings 2 and a tail 3, wherein the wings 2 and the tail 3 respectively penetrate through the fuselage 1, the fuselage 1 comprises a fuselage front plate 4, an adjusting plate 5 and a fuselage rear plate 6, the adjusting plate 5 is connected between the fuselage front plate 4 and the fuselage rear plate 6, the adjusting plate 5 is of a bendable structure, the wing 2 comprises a wing root 7 and a wing tip 8, the wing tip 8 is connected at two ends of the wing root 7, the wing tip 8 is of an upwardly bendable structure, the tail 3 comprises a tail root 9 and a tail tip 10, the tail tip 10 is connected at two ends of the tail root 9, the tail tip 10 is of an upwardly bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction, and then the rear plate 6 of the motor body is driven to rotate left and right, the angle of the left rotation of the adjusting plate 5 is 30 degrees, and the angle of the upward rotation of the wing end 8 and the tail wing end 10 is 30 degrees.
Example 6: a hand-thrown rotary type airplane for teaching demonstration, which comprises a fuselage 1, wings 2 and a tail 3, wherein the wings 2 and the tail 3 respectively penetrate through the fuselage 1, the fuselage 1 comprises a fuselage front plate 4, an adjusting plate 5 and a fuselage rear plate 6, the adjusting plate 5 is connected between the fuselage front plate 4 and the fuselage rear plate 6, the adjusting plate 5 is of a bendable structure, the wing 2 comprises a wing root 7 and a wing tip 8, the wing tip 8 is connected at two ends of the wing root 7, the wing tip 8 is of an upwardly bendable structure, the tail 3 comprises a tail root 9 and a tail tip 10, the tail tip 10 is connected at two ends of the tail root 9, the tail tip 10 is of an upwardly bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction, further, the rear plate 6 with the fuselage is rotated left and right, the angle of rotation of the adjusting plate 5 to the right is 30 degrees, and the angle of rotation of the wing tip 8 and the tail wing tip 10 to the up is 30 degrees.
Example 7: a hand-thrown rotary type airplane for teaching demonstration, which comprises a fuselage 1, wings 2 and a tail 3, wherein the wings 2 and the tail 3 respectively penetrate through the fuselage 1, the fuselage 1 comprises a fuselage front plate 4, an adjusting plate 5 and a fuselage rear plate 6, the adjusting plate 5 is connected between the fuselage front plate 4 and the fuselage rear plate 6, the adjusting plate 5 is of a bendable structure, the wing 2 comprises a wing root 7 and a wing tip 8, the wing tip 8 is connected at two ends of the wing root 7, the wing tip 8 is of an upwardly bendable structure, the tail 3 comprises a tail root 9 and a tail tip 10, the tail tip 10 is connected at two ends of the tail root 9, the tail tip 10 is of an upwardly bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction, and then the rear plate 6 of the motor body is driven to rotate left and right, the angle of leftward rotation of the adjusting plate 5 is 15 degrees, and the angle of upward rotation of the wing tip 8 and the tail wing tip 10 is 15 degrees.
Example 8: a hand-thrown rotary type airplane for teaching demonstration, which comprises a fuselage 1, wings 2 and a tail 3, wherein the wings 2 and the tail 3 respectively penetrate through the fuselage 1, the fuselage 1 comprises a fuselage front plate 4, an adjusting plate 5 and a fuselage rear plate 6, the adjusting plate 5 is connected between the fuselage front plate 4 and the fuselage rear plate 6, the adjusting plate 5 is of a bendable structure, the wing 2 comprises a wing root 7 and a wing tip 8, the wing tip 8 is connected at two ends of the wing root 7, the wing tip 8 is of an upwardly bendable structure, the tail 3 comprises a tail root 9 and a tail tip 10, the tail tip 10 is connected at two ends of the tail root 9, the tail tip 10 is of an upwardly bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction, further, the rear plate 6 of the belt body rotates left and right, the angle of the rightward rotation of the adjusting plate 5 is 15 degrees, and the angle of the upward rotation of the wing tip 8 and the empennage tip 10 is 15 degrees.
Example 9: a hand-thrown rotary aircraft for teaching demonstration comprises an aircraft body 1, wings 2 and an empennage 3, wherein the wings 2 and the empennage 3 respectively penetrate through the aircraft body 1, the aircraft body 1 comprises an aircraft body front plate 4, an adjusting plate 5 and an aircraft body rear plate 6, the adjusting plate 5 is connected between the aircraft body front plate 4 and the aircraft body rear plate 6, the adjusting plate 5 is of a bendable structure, the wings 2 comprise wing roots 7 and wing tips 8, the wing tips 8 are connected to two ends of the wing roots 7, the wing tips 8 are of an upward bendable structure, the empennage 3 comprises an empennage root 9 and an empennage tip 10, the empennage tips 10 are connected to two ends of the empennage root 9, the empennage tips 10 are of an upward bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction and further rotates left and right with the aircraft body rear plate 6, the leftward rotation angle of the adjusting plate 5 is 60 degrees, and the wing tips 8 and the empennage tips 10 are kept still.
Example 10: a hand-thrown rotary aircraft for teaching demonstration comprises an aircraft body 1, wings 2 and an empennage 3, wherein the wings 2 and the empennage 3 respectively penetrate through the aircraft body 1, the aircraft body 1 comprises an aircraft body front plate 4, an adjusting plate 5 and an aircraft body rear plate 6, the adjusting plate 5 is connected between the aircraft body front plate 4 and the aircraft body rear plate 6, the adjusting plate 5 is of a bendable structure, the wings 2 comprise wing roots 7 and wing tips 8, the wing tips 8 are connected to two ends of the wing roots 7, the wing tips 8 are of an upward bendable structure, the empennage 3 comprises an empennage wing root 9 and an empennage tip 10, the empennage tips 10 are connected to two ends of the empennage wing roots 9, the empennage tips 10 are of an upward bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction and further rotates left and right with the aircraft body rear plate 6, the adjusting plate 5 and the empennage tips 10 are kept stationary, and the upward rotation angle of the wing tips 8 is 15 degrees.
Example 11: a hand-thrown rotary aircraft for teaching demonstration comprises an aircraft body 1, wings 2 and an empennage 3, wherein the wings 2 and the empennage 3 respectively penetrate through the aircraft body 1, the aircraft body 1 comprises an aircraft body front plate 4, an adjusting plate 5 and an aircraft body rear plate 6, the adjusting plate 5 is connected between the aircraft body front plate 4 and the aircraft body rear plate 6, the adjusting plate 5 is of a bendable structure, the wings 2 comprise wing roots 7 and wing tips 8, the wing tips 8 are connected to two ends of the wing roots 7, the wing tips 8 are of an upward bendable structure, the empennage 3 comprises an empennage root 9 and an empennage tip 10, the empennage tips 10 are connected to two ends of the empennage root 9, the empennage tips 10 are of an upward bendable structure, the adjusting plate 5 rotates left and right in the horizontal direction and further rotates left and right with the aircraft body rear plate 6, the adjusting plate 5 and the wing tips 8 are kept stationary, and the angle of upward rotation of the empennage tips 10 is 20 degrees.
Although the invention has been shown and described in detail with respect to the preferred embodiments thereof, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (10)
1. The utility model provides a hand throwing formula of circling round aircraft for teaching demonstration, its includes fuselage (1), wing (2) and fin (3), wing (2) with fin (3) pass respectively fuselage (1), its characterized in that: its fuselage (1) includes fuselage front bezel (4), regulating plate (5) and fuselage back plate (6), regulating plate (5) are connected fuselage front bezel (4) with between fuselage back plate (6), regulating plate (5) are flexible structure, wing (2) are including wing root (7) and wing tip (8), wing tip (8) are connected the both ends of wing root (7), wing tip (8) are the structure of kickup, fin (3) are including fin root (9) and fin tip (10), fin tip (10) are connected the both ends of fin root (9), fin tip (10) are the structure of kickup.
2. A hand-thrown rotary aircraft for educational demonstration according to claim 1, wherein: the adjusting plate (5) rotates left and right in the horizontal direction, and then drives the body rear plate (6) to rotate left and right.
3. A hand-thrown rotary aircraft for educational demonstration according to claim 2, wherein: the angle of the adjusting plate (5) rotating leftwards or rightwards is 0-90 degrees.
4. A hand-thrown rotary aircraft for educational demonstration according to claim 2, wherein: the angle of the adjusting plate (5) rotating leftwards or rightwards is 0-60 degrees.
5. A hand-thrown rotary aircraft for educational demonstration according to claim 2, wherein: the angle of the adjusting plate (5) rotating leftwards or rightwards is 0-30 degrees.
6. A hand-thrown rotary aircraft for educational demonstration according to claim 2, wherein: the angle of the adjusting plate (5) rotating leftwards or rightwards is 0-15 degrees.
7. A hand-thrown rotary aircraft for educational demonstration according to claim 1, wherein: the angle of upward rotation of the wing tip (8) and the empennage tip (10) is 0-90 degrees.
8. A hand-thrown rotary aircraft for educational demonstration according to claim 1, wherein: the angle of upward rotation of the wing tip (8) and the empennage tip (10) is 0-60 degrees.
9. A hand-thrown rotary aircraft for educational demonstration according to claim 1, wherein: the angle of upward rotation of the wing tip (8) and the empennage tip (10) is 0-30 degrees.
10. A hand-thrown rotary aircraft for educational demonstration according to claim 1, wherein: the angle of upward rotation of the wing tip (8) and the empennage tip (10) is 0-15 degrees.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121149090.2U CN214796465U (en) | 2021-05-27 | 2021-05-27 | Hand-throwing rotary airplane for teaching demonstration |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121149090.2U CN214796465U (en) | 2021-05-27 | 2021-05-27 | Hand-throwing rotary airplane for teaching demonstration |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214796465U true CN214796465U (en) | 2021-11-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121149090.2U Active CN214796465U (en) | 2021-05-27 | 2021-05-27 | Hand-throwing rotary airplane for teaching demonstration |
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| Country | Link |
|---|---|
| CN (1) | CN214796465U (en) |
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2021
- 2021-05-27 CN CN202121149090.2U patent/CN214796465U/en active Active
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