CN219072056U

CN219072056U - Novel pin-connected panel model aeroplane and model ship wing

Info

Publication number: CN219072056U
Application number: CN202223463861.2U
Authority: CN
Inventors: 杨锋; 葛炳来; 王泰; 杨梦真; 赵传龙
Original assignee: Shandong Chuangfei Aviation Technology Co ltd
Current assignee: Shandong Chuangfei Aviation Technology Co ltd
Priority date: 2022-12-25
Filing date: 2022-12-25
Publication date: 2023-05-26
Anticipated expiration: 2032-12-25

Abstract

The utility model discloses a novel assembled model airplane wing, which comprises a model airplane, wherein a notch is formed in the surface of the model airplane, the wing is clamped on the inner side surface of the notch, a fastening device is arranged on the lower end surface of the model airplane, the wing is clamped and fixed by the fastening device, the wing is installed by adopting a fastening positioning structure, the wing is fastened and fixed by the fastening device, the wing is installed conveniently, and the wing is detached and replaced conveniently.

Description

Novel pin-connected panel model aeroplane and model ship wing

Technical Field

The utility model relates to the field of aeromodelling, in particular to a novel assembled aeromodelling wing.

Background

Aero-models are a generic term for various aircraft models, including model aircraft and other model aircraft;

in the prior assembled model airplane, the wings and the model airplane main body are assembled, and are mostly fixed by screws, so that the wings are easy to damage during flying and inconvenient to replace.

Disclosure of Invention

Aiming at the problems in the prior art, the utility model aims to provide a novel assembled model airplane wing, which adopts a clamping positioning structure to install the wing, and the fastening device is fastened to fix the wing, so that the wing is convenient to install, and convenient to detach and replace.

In order to solve the problems, the utility model adopts the following technical scheme.

The utility model provides a novel pin-connected panel model aeroplane and model ship wing, includes the model aeroplane and model ship, the opening groove is seted up on the surface of model aeroplane and model ship, the inboard surface joint in opening groove has the wing, the lower extreme surface of model aeroplane and model ship is provided with fastening device, fastening device joint fixed wing adopts joint location structure to install the wing, and fastening device fastening fixed wing is convenient when installing the wing, and it is convenient when the split is changed.

Further, the buckling device comprises a convex groove, a spring and a convex clamping block, wherein the convex groove is formed in the lower end surface of the model airplane, the convex clamping block and the spring are arranged on the inner side surface of the convex groove, and the convex clamping block is clamped on the inner side surface of the wing, so that the wing can be conveniently clamped and fixed.

Further, the surface of the wing is provided with a positioning clamping hole, and the convex clamping block is clamped on the inner side surface of the positioning clamping hole, so that positioning clamping is facilitated.

Further, the jack has been seted up to the upper end surface of model aeroplane and model ship, jack and location card hole intercommunication, and during the change, usable screwdriver inserts along the jack, can impress the convex fixture block, is convenient for pull out the wing and dismantles the change, and it is convenient to change.

Further, the inner side surface of the lower end of the convex groove is connected with a screw through threads, so that the bottom is conveniently plugged.

Furthermore, the outer end of the wing is provided with a positioning groove, and the positioning groove is clamped into the inner side surface of the notch of the model airplane, so that the wing can be conveniently clamped into and positioned.

Furthermore, the convex fixture block adopts a convex round block structure, and is placed on the inner side surface of the convex groove together with the spring, so that the installation mechanism is convenient to assemble.

Compared with the prior art, the utility model has the advantages that:

(1) The wing is installed by adopting the clamping positioning structure, the fastening device is fastened and fixed on the wing, and the wing is convenient to install, and convenient to detach and replace.

(2) The fastening device comprises a convex groove, a spring and a convex clamping block, wherein the convex groove is formed in the lower end surface of the model airplane, the convex clamping block and the spring are arranged on the inner side surface of the convex groove, the convex clamping block is clamped on the inner side surface of the wing, the wing is conveniently clamped and fixed, the surface of the wing is provided with a positioning clamping hole, and the convex clamping block is clamped on the inner side surface of the positioning clamping hole, so that positioning clamping is facilitated.

(3) The jack is offered on the upper end surface of model aeroplane and model ship, jack and location card hole intercommunication, and during the change, usable screwdriver inserts along the jack, can push in the convex fixture block, is convenient for pull out the wing and dismantles the change, and it is convenient to change.

Drawings

FIG. 1 is a schematic cross-sectional view of the overall structure of the present utility model;

FIG. 2 is a top view of the overall structure of the present utility model;

figure 3 is a top view of a wing of the present utility model.

The reference numerals in the figures illustrate:

1 model airplane, 2 notch, 3 wings, 4 fastening device, 40 convex groove, 41 spring, 42 convex fixture block, 31 positioning fixture hole, 100 jack, 30 positioning groove, 43 screw.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Example 1

Referring to fig. 1-3, a novel assembled model airplane wing comprises a model airplane 1, wherein a notch 2 is formed in the surface of the model airplane 1, a wing 3 is clamped on the inner side surface of the notch 2, a fastening device 4 is arranged on the lower end surface of the model airplane 1, and the fastening device 4 is clamped on the fixed wing 3;

the outer end of the wing 3 is provided with a positioning groove 30, when in installation, the positioning groove 30 of the wing 3 is clamped into the inner side surface of the notch 2 of the model airplane 1, the positioning groove can be mutually inserted and positioned, the fastening device 4 comprises a convex groove 40, a spring 41 and a convex clamping block 42, the convex groove 40 is arranged on the lower end surface of the model airplane 1, after the wing 3 is clamped, the convex clamping block 42 can be sprung up by the spring 41, the convex clamping block 42 can be clamped on the inner side surface of the wing 3, the surface of the wing 3 is provided with a positioning clamping hole 31, and the convex clamping block 42 is clamped on the inner side surface of the positioning clamping hole 31, so that the fastening device is convenient to clamp and fix, and the installation is convenient and stable;

the jack 100 is arranged on the upper end surface of the model airplane 1, the jack 100 is communicated with the positioning clamping hole 31, a screwdriver can be used for inserting along the jack 100 during replacement, and the convex clamping block 42 can be pressed in, so that the wing 3 can be conveniently pulled out, detached and replaced, and the replacement is convenient.

Example 2

the convex clamping block 42 and the spring 41 are arranged on the inner side surface of the convex groove 40, the convex clamping block 42 adopts a convex round block structure, and is placed on the inner side surface of the convex groove 41 together with the spring 41, so that the convex clamping block 42 and the spring 41 are convenient to assemble, and the inner side surface of the lower end of the convex groove 40 is connected with the screw 43 through threads, so that the bottom of the convex groove 41 can be plugged, and the assembly is convenient.

The above description is only of the preferred embodiments of the present utility model; the scope of the utility model is not limited in this respect. Any person skilled in the art, within the technical scope of the present disclosure, may apply to the present utility model, and the technical solution and the improvement thereof are all covered by the protection scope of the present utility model.

Claims

1. Novel pin-connected panel model aeroplane and model ship wing, including model aeroplane and model ship (1), its characterized in that: the surface of model aeroplane and model ship (1) is offered notch (2), the inboard surface joint in notch (2) has wing (3), the lower extreme surface of model aeroplane and model ship (1) is provided with fastening device (4), fastening device (4) joint fixed wing (3).

2. A novel modular aeromodelling wing as claimed in claim 1, wherein: the buckling device (4) comprises a convex groove (40), a spring (41) and a convex clamping block (42), wherein the convex groove (40) is formed in the lower end surface of the model airplane (1), the convex clamping block (42) and the spring (41) are arranged on the inner side surface of the convex groove (40), and the convex clamping block (42) is clamped on the inner side surface of the wing (3).

3. A novel modular aeromodelling wing as claimed in claim 1, wherein: the surface of the wing (3) is provided with a positioning clamping hole (31), and the convex clamping block (42) is clamped on the inner side surface of the positioning clamping hole (31).

4. A novel modular aeromodelling wing as claimed in claim 3, wherein: the upper end surface of the model airplane (1) is provided with a jack (100), and the jack (100) is communicated with the positioning clamping hole (31).

5. A novel modular aeromodelling wing as claimed in claim 2, wherein: the inner side surface of the lower end of the convex groove (40) is connected with a screw (43) through threads.

6. A novel modular aeromodelling wing as claimed in claim 1, wherein: the outer end of the wing (3) is provided with a positioning groove (30), and the positioning groove (30) is clamped into the inner side surface of the notch (2) of the model airplane (1).

7. A novel modular aeromodelling wing as claimed in claim 2, wherein: the convex clamping block (42) adopts a convex round block structure and is placed on the inner side surface of the convex groove (40) together with the spring (41).