CN218280546U

CN218280546U - Airplane model with adjustable wing angle

Info

Publication number: CN218280546U
Application number: CN202222520074.0U
Authority: CN
Inventors: 肖谦
Original assignee: Xi'an Hanchangyu Construction Engineering Co ltd
Current assignee: Xi'an Hanchangyu Construction Engineering Co ltd
Priority date: 2022-09-22
Filing date: 2022-09-22
Publication date: 2023-01-13
Anticipated expiration: 2032-09-22

Abstract

The utility model discloses an aircraft model with adjustable wing angle, include: fuselage, wing, pulley and fixed block, the fuselage both sides are provided with the wing, the fuselage all is connected with the pulley with the bottom of wing, this aircraft model with adjustable wing angle, the aircraft model demonstrates to outer through the show area usually, and the aircraft model is a whole, can't dismantle the aircraft model, thereby lead to unable angle modulation to the wing, can rotate the threaded rod this moment, can carry out the thread slipping with the slider when the threaded rod rotates, can drive the connecting block during slider thread slipping and remove, can lift up or push down the removal to the wing when the connecting block removes the assigned position, can hoist the show with the wing this moment, thereby avoid visitor's touching the aircraft model, the condition that the aircraft model dropped takes place, the aircraft model of being convenient for can hoist the show and the condition that can not appear dropping.

Description

Airplane model with adjustable wing angle

Technical Field

The utility model relates to an aircraft model technical field specifically is an aircraft model with adjustable wing angle.

Background

Airplane models are generally divided into two categories, dynamic and static: the model is static for collection, display and the like, can not fly, and is a model which takes an airplane as an image and is reduced according to a certain proportion; the dynamic state is that the aircraft can fly and can be controlled by remote control and other modes, people can know more aircraft knowledge through an aircraft model, and the existing blood sampling auxiliary equipment has certain defects when in use;

static aircraft models are usually used for displaying, and the aircraft models are integrally connected together and cannot be detached, so that the angles of the wings of the aircraft models cannot be adjusted as required, and the diversity of the aircraft models cannot be displayed.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an aircraft model with adjustable wing angle to solve the unable angle regulation's of wing on the aircraft model in the existing market that above-mentioned background art provided problem.

In order to achieve the above object, the utility model provides a following technical scheme: an aircraft model with adjustable wing angle, comprising: fuselage, wing, pulley and fixed block, the fuselage both sides are provided with the wing, the fuselage all is connected with the pulley with the bottom of wing, and the fixed block is installed the both sides of fuselage, the inside spout of having seted up of fixed block, the inside threaded rod that has run through the bearing that passes through of spout, the threaded rod outside is connected with the slider, the slider outside is connected with the connecting block, is close to the connecting block the mounting groove has been seted up to the inside of wing, mounting groove internally mounted has the damping pivot, damping pivot through connection block's inside.

Preferably, the sliding block and the connecting block are of an integral structure.

Preferably, a rotating structure is formed between the connecting block and the damping rotating shaft through a mounting groove.

Preferably, the wing is further provided with a storage groove, a limiting groove, a moving block, a limiting block and a hanging ring, and the storage groove is formed in the surface of the top of the wing.

Preferably, the inner wall of the accommodating groove is provided with a limiting groove, a moving block is connected inside the accommodating groove, and two sides of the moving block close to the limiting groove are connected with limiting blocks.

Preferably, a lifting ring is installed at the top of the moving block.

Compared with the prior art, the beneficial effects of the utility model are that: this aircraft model with adjustable wing angle, aircraft model demonstrates to the outside through the show area usually, and aircraft model is a whole, can't dismantle aircraft model, thereby lead to unable angle modulation to the wing, can rotate the threaded rod this moment, can carry out the screw thread slip with the slider when the threaded rod rotates, can drive the connecting block during slider screw thread slip and remove, can lift up or push down the removal to the wing when the connecting block removes the assigned position, can hoist the show with the wing this moment, thereby avoid visitor's touching aircraft model, the condition that the aircraft model dropped takes place, be convenient for aircraft model can hoist the show and can not appear the condition that drops.

1. The aircraft model demonstrates outside through the show area usually, and the aircraft model is a whole, can't dismantle the aircraft model, thereby lead to can't carrying out angle modulation to the wing, can rotate the threaded rod this moment, can carry out the screw thread slip with the slider when the threaded rod rotates, can drive the connecting block during slider screw thread slip and remove, can lift or push down the removal to the wing when the connecting block removes the assigned position, can rotate through damping pivot and connecting block when the wing removes, the aircraft model of being convenient for can adjust the angle of wing according to the demand.

2. The easy condition that takes place to drop when visitor handheld aircraft model, can stimulate rings this moment and remove, rings can drive the movable block when removing and remove, the movable block can drive the stopper when sliding and remove, can slide with the spacing groove when the stopper removes, can dock lifting rope and rings when rings remove the assigned position, can hoist fuselage and wing show this moment, thereby avoid visitor touching aircraft model, the condition that the aircraft model dropped takes place, the aircraft model of being convenient for can hoist the show and can not appear the condition that drops.

Drawings

FIG. 1 is a front view of the cutting structure of the present invention;

FIG. 2 is a schematic top view of the present invention;

FIG. 3 is a front view of the fixing block of the present invention;

fig. 4 is the view of the hanging ring of the present invention.

In the figure: 1. a body; 2. an airfoil; 3. a pulley; 4. a fixed block; 5. a chute; 6. a threaded rod; 7. a slider; 8. connecting blocks; 9. mounting grooves; 10. a damping rotating shaft; 11. a storage groove; 12. a limiting groove; 13. a moving block; 14. a limiting block; 15. a lifting ring.

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. 1-4, the present invention provides a technical solution: an aircraft model with adjustable wing angle, comprising: fuselage 1, wing 2, pulley 3 and

fixed block

4, 1 both sides of fuselage are provided with wing 2, fuselage 1 all is connected with pulley 3 with wing 2's bottom, fixed block 4, install the both sides at fuselage 1, fixed block 4 has inside spout 5 of having seted up, spout 5 is inside to have threaded rod 6 through bearing through connection, threaded rod 6 outside is connected with slider 7, slider 7 outside is connected with connecting block 8, mounting groove 9 has been seted up to the inside of wing 2 that is close to connecting block 8, mounting groove 9 internally mounted has damping

pivot

10, 10 inside through connection piece 8 of damping pivot, slider 7 and connecting block 8 structure as an organic whole, constitute revolution mechanic through mounting groove 9 between connecting block 8 and the damping pivot 10.

During the concrete implementation, the model demonstrates outside through the show area usually, and the aircraft model is a whole, can't dismantle the aircraft model, thereby lead to unable angle modulation to wing 2, can't show the characteristic of aircraft model, can rotate threaded rod 6 this moment, can carry out the screw thread slip with slider 7 when threaded rod 6 rotates, slider 7 can drive connecting block 8 during the screw thread slip and remove, can lift up or push down the removal to wing 2 when connecting block 8 removes the assigned position, can rotate through damping pivot 10 and connecting block 8 when wing 2 removes, can adjust the angle that wing 2 and fuselage 1 formed during wing 2 is rotatory.

Referring to fig. 1,2 and 3, the model can adjust the angle of the wing 2 according to the requirement.

Referring to fig. 1,2 and 4, the wing 2 is further provided with a storage groove 11, a limiting groove 12, a moving block 13, a limiting block 14 and a hanging ring 15, the storage groove 11 is formed in the top surface of the wing 2, the limiting groove 12 is formed in the inner wall of the storage groove 11, the moving block 13 is connected inside the storage groove 11, the limiting block 14 is connected to two sides of the moving block 13 close to the limiting groove 12, the hanging ring 15 is installed at the top of the moving block 13, and the hanging rings 15 are symmetrically provided with two groups about the center of the body 1.

When the airplane model is displayed externally, the airplane model is usually fixed on a display frame when the airplane model is displayed externally, a visitor can easily fall the airplane model when holding the airplane model, the surface of the airplane model is usually smooth and does not have the function of lifting display, the lifting ring 15 can be pulled to move at the moment, the lifting ring 15 can drive the moving block 13 to move when moving, the moving block 13 can slide with the accommodating groove 11 when moving, the moving block 13 can drive the limiting block 14 to move when sliding, the limiting block 14 can slide with the limiting groove 12 when moving, the lifting rope can be butted with the lifting ring 15 when the lifting ring 15 moves to a specified position, the airplane body 1 and the wing 2 can be lifted to be displayed at the moment, and therefore the visitor is prevented from touching the airplane model and the airplane model falls.

Referring to fig. 1,2 and 4, the airplane model can be lifted and displayed without falling.

In summary, when the airplane model with adjustable wing angles is used, the height of the sliding block 7 is adjusted through the threaded rod 6, so that the angles of the wings 2 can be adjusted, the airplane model can be conveniently displayed in different postures, the airplane model can be hung and displayed in order to avoid direct contact of personnel with the airplane model, and the airplane model cannot be damaged, and the content which is not described in detail in the description belongs to the prior art known by the person skilled in the art.

Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.

Claims

1. An aircraft model with adjustable wing angle, comprising: the airplane comprises a fuselage (1), wings (2), pulleys (3) and fixed blocks (4), and is characterized in that the fuselage is fixed on the wing;

wings (2) are arranged on two sides of the fuselage (1), and pulleys (3) are connected to the bottoms of the fuselage (1) and the wings (2);

fixed block (4), install the both sides of fuselage (1), fixed block (4) inside spout (5) have been seted up, spout (5) are inside to have threaded rod (6) through bearing through connection, threaded rod (6) outside is connected with slider (7), slider (7) outside is connected with connecting block (8), is close to connecting block (8) mounting groove (9) have been seted up to the inside of wing (2), mounting groove (9) internally mounted has damping pivot (10), the inside of damping pivot (10) through connection piece (8).

2. An aircraft model with adjustable wing angle as defined in claim 1, wherein: the sliding block (7) and the connecting block (8) are of an integral structure.

3. An aircraft model with adjustable wing angle as defined in claim 2, wherein: and a rotating structure is formed between the connecting block (8) and the damping rotating shaft (10) through a mounting groove (9).

4. An aircraft model with adjustable wing angle as defined in claim 1, wherein: the wing (2) is further provided with a storage groove (11), a limiting groove (12), a moving block (13), a limiting block (14) and a hanging ring (15), and the storage groove (11) is formed in the top surface of the wing (2).

5. An aircraft model with adjustable wing angle as defined in claim 4, wherein: the inner wall of the accommodating groove (11) is provided with a limiting groove (12), a moving block (13) is connected inside the accommodating groove (11), and limiting blocks (14) are connected to two sides of the moving block (13) close to the limiting groove (12).

6. An aircraft model with adjustable wing angle as defined in claim 5, wherein: and a hanging ring (15) is arranged at the top of the moving block (13).