Multi-section aircraft model

Abstract

The utility model discloses a multi-segment aircraft model, which comprises an aircraft model body and a support, the outer side wall of the aircraft model body is fixedly sleeved with a positioning sleeve, the two sides of the positioning sleeve are fixedly connected with transverse plates, the bottom of each transverse plate is fixedly connected with a bearing plate, the inner walls of the two sides of the support are both provided with grooves, and the inner walls of the two sides of the support are fixedly connected with the bearing plate. A sliding rod is fixedly connected into the groove, the sliding rod is slidably sleeved with a sliding block, an inserting groove is formed in the top of the sliding block, the bottom end of the bearing plate is slidably inserted into the inserting groove, the sliding rod is sleeved with a spring, and the two ends of the spring are fixedly connected with the bottom of the sliding block and the inner wall of the groove correspondingly; according to the aircraft model, the springback assembly is adopted, the launching state can be simulated, then the interestingness of the aircraft model is improved, and the aircraft model can be locked to form an ornament.

Description

Technical Field

[0001] The utility model relates to the field of aircraft model-related products, in particular to a multi-section aircraft model. Background Art

[0002] Aviation refers to the navigation of manned or unmanned aircraft in the Earth's atmosphere; aerospace refers to the navigation of manned or unmanned spacecraft outside the Earth's atmosphere, also known as space flight or space navigation. In order to expand social production, humans must open up new spaces for activities. From land to sea, from sea to atmosphere, and then to outer space, this is the process of humans gradually expanding their scope of activities. The production of aircraft models can be used to popularize aviation knowledge and cultivate aviation science and technology talents. Aircraft models have developed into a very attractive entertainment toy;

[0003] However, the existing aircraft models are only for viewing purposes, have single functions, are less interesting, and cannot satisfy children's interactive operations, thus having defects. Utility Model Content

[0004] The purpose of the utility model is to provide a multi-section aircraft model to solve the problems raised in the above background technology.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a multi-section aircraft model, comprising an aircraft model body and a bracket, a positioning sleeve fixedly sleeved on the outer side wall of the aircraft model body, both sides of the positioning sleeve are fixedly connected with cross plates, the bottom of the cross plate is fixedly connected with a carrying plate, grooves are provided on the inner walls of both sides of the bracket, sliding rods are fixedly connected in the grooves, a sliding block is slidably sleeved on the sliding rod, a slot is provided at the top of the sliding block, the bottom end of the carrying plate is slidably inserted in the slot, a spring is sleeved on the sliding rod, the two ends of the spring are respectively fixedly connected to the bottom of the sliding block and the inner wall of the groove, the top of both ends of the bracket are fixedly connected with support blocks, a screw mouth is provided on the support block, a threaded rod is inserted into the inner thread of the screw mouth, one end of the threaded rod is fixedly connected with a clamping block, and a clamping groove corresponding to the clamping block is provided on the outer side wall of the carrying plate.

[0006] Preferably, a mounting groove is provided at the bottom of the bracket, and a counterweight block is fixedly connected in the mounting groove.

[0007] Preferably, one end of the threaded rod away from the clamping block is fixedly connected to a rotating block, and an outer side wall of the rotating block is provided with anti-slip grooves.

[0008] Preferably, a buffer sleeve is fixedly sleeved on the top of the aircraft model body, and the buffer sleeve is made of sponge.

[0009] Preferably, the positioning sleeve is arranged in a ring-shaped structure.

[0010] Preferably, the bracket is arranged in a "concave" structure.

[0011] Compared with the prior art, the beneficial effects of the utility model are:

[0012] The multi-section aircraft model is implemented by inserting the bearing plate on the bottom of the cross plate into the slot on the slider, and by rotating the threaded rod on the support block to push the card block to be inserted into the card slot on the bearing plate to fix the aircraft model body. The aircraft model body is supported by a bracket, and the card block can be removed from the card slot and then the aircraft model body can be pressed to cause the bearing plate to push the slider to slide on the slide rod. At this time, the slider will press the spring to compress it, and the aircraft model body is released. At this time, the spring in the compressed state automatically rebounds under the action of its own rebound force to push the slider back to the initial position. At the same time, the bearing plate is separated from the aircraft model body from the slot and bounces upward. The utility model adopts the setting of the rebound component to simulate the launching state, thereby increasing the interest of the aircraft model, and can be locked to form a pendant. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a structural schematic diagram of a multi-section aircraft model of the utility model;

[0014] Figure 2 It is an enlarged view of point A of a multi-section aircraft model of the present utility model.

[0015] In the figure: 1. Aircraft model body; 2. Bracket; 3. Positioning sleeve; 4. Cross plate; 5. Load-bearing plate; 6. Sliding rod; 7. Sliding block; 8. Spring; 9. Support block; 10. Threaded rod; 11. Block; 12. Counterweight block; 13. Rotating block; 14. Buffer sleeve. DETAILED DESCRIPTION

[0016] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0017] See also Figure 1-2The utility model provides an embodiment: a multi-section aircraft model, including an aircraft model body 1 and a bracket 2, a positioning sleeve 3 is fixedly sleeved on the outer wall of the aircraft model body 1, and both sides of the positioning sleeve 3 are fixedly connected with a cross plate 4, and the bottom of the cross plate 4 is fixedly connected with a bearing plate 5, and grooves are provided on the inner walls of both sides of the bracket 2, and a slide bar 6 is fixedly connected in the groove, and a slider 7 is slidably sleeved on the slide bar 6, and a slot is provided on the top of the slider 7, and the bottom end of the bearing plate 5 is slidably inserted in the slot, and a spring 8 is sleeved on the slide bar 6, and the two ends of the spring 8 are respectively fixedly connected to the bottom of the slider 7 and the inner wall of the groove. Specifically, pressing the aircraft model body 1 causes the bearing plate 5 to push the slider 7 to slide on the slide bar 6, and at this time the slider 7 will press the spring 8 to make it In a compressed state, the aircraft model body 1 is released, and the spring 8 in a compressed state automatically rebounds under the action of its own resilience to push the slider 7 back to its initial position. At the same time, the supporting plate 5 is separated from the aircraft model body 1 in the slot and bounces upward; the tops of both ends of the bracket 2 are fixedly connected with support blocks 9, and a screw hole is provided on the support block 9. A threaded rod 10 is inserted into the inner thread of the screw hole, and a clamping block 11 is fixedly connected to one end of the threaded rod 10. A clamping groove corresponding to the clamping block 11 is provided on the outer wall of the supporting plate 5. Specifically, the threaded rod 10 is rotated on the support block 9 to push the clamping block 11 to be inserted into the clamping groove on the supporting plate 5, thereby realizing the fixation of the aircraft model body 1, and the aircraft model body 1 is supported by the bracket 2 as a decorative piece.

[0018] In this embodiment, an installation groove is provided at the bottom of the bracket 2, and a counterweight block 12 is fixedly connected in the installation groove to improve the supporting stability of the bracket 2; a rotating block 13 is fixedly connected to the end of the threaded rod 10 away from the clamping block 11, and anti-slip grooves are provided on the outer wall of the rotating block 13 to facilitate the rotation of the threaded rod 10; a buffer sleeve 14 is fixedly sleeved on the top of the aircraft model body 1, and the buffer sleeve 14 is made of sponge to increase the buffering effect of the top of the aircraft model body 1 to avoid impact on the face; the positioning sleeve 3 is a ring-shaped mechanism; the bracket 2 is a "concave" structure.

[0019] Working principle: First, insert the carrier plate 5 on the bottom of the horizontal plate 4 into the slot on the slider 7, and then push the card block 11 into the card slot on the carrier plate 5 by rotating the threaded rod 10 on the support block 9 to fix the aircraft model body 1. Use the bracket 2 to support the aircraft model body 1 as a decoration.

[0020] The card block 11 can be removed from the card slot and then the aircraft model body 1 can be pressed to cause the supporting plate 5 to push the slider 7 to slide on the slide rod 6. At this time, the slider 7 will press the spring 8 to compress it. The aircraft model body 1 is released. At this time, the spring 8 in the compressed state automatically rebounds under the action of its own resilience and pushes the slider 7 back to its initial position. At the same time, the supporting plate 5 is separated from the aircraft model body 1 in the slot and bounces upward.

[0021] It is obvious to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be regarded as exemplary and non-restrictive from any point of view, and the scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present invention. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.

Claims

1. A multi-section aircraft model, comprising an aircraft model body (1) and a bracket (2), characterized in that: A positioning sleeve (3) is fixedly sleeved on the outer wall of the aircraft model body (1), and both sides of the positioning sleeve (3) are fixedly connected with a cross plate (4), and the bottom of the cross plate (4) is fixedly connected with a bearing plate (5), and grooves are provided on the inner walls of both sides of the bracket (2), and a sliding rod (6) is fixedly connected in the groove, and a slider (7) is slidably sleeved on the sliding rod (6), and a slot is provided at the top of the slider (7), and the bottom end of the bearing plate (5) is slidably inserted in the slot, and a spring (8) is sleeved on the sliding rod (6), and the two ends of the spring (8) are respectively fixedly connected to the bottom of the slider (7) and the inner wall of the groove, and the tops of both ends of the bracket (2) are fixedly connected with support blocks (9), and the support block (9) is provided with a screw hole, and a threaded rod (10) is inserted into the inner thread of the screw hole, and one end of the threaded rod (10) is fixedly connected with a clamping block (11), and a clamping groove corresponding to the clamping block (11) is provided on the outer wall of the bearing plate (5).

2. A multi-section aircraft model according to claim 1, characterized in that: A mounting groove is provided at the bottom of the bracket (2), and a counterweight block (12) is fixedly connected in the mounting groove.

3. A multi-section aircraft model according to claim 1, characterized in that: One end of the threaded rod (10) away from the clamping block (11) is fixedly connected to a rotating block (13), and an outer side wall of the rotating block (13) is provided with anti-slip grooves.

4. A multi-section aircraft model according to claim 1, characterized in that: A buffer sleeve (14) is fixedly sleeved on the top of the aircraft model body (1), and the buffer sleeve (14) is made of sponge.

5. A multi-section aircraft model according to claim 1, characterized in that: The positioning sleeve (3) is arranged as an annular structure.

6. A multi-section aircraft model according to claim 1, characterized in that: The support (2) is arranged in a "concave" type structure.

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