CN210503896U

CN210503896U - Aircraft head-shaped ribbon

Info

Publication number: CN210503896U
Application number: CN201920952282.3U
Authority: CN
Inventors: 赵百谦
Original assignee: Xuancheng Longhua Electron Co ltd
Current assignee: Xuancheng Longhua Electron Co ltd
Priority date: 2019-06-21
Filing date: 2019-06-21
Publication date: 2020-05-12
Anticipated expiration: 2029-06-21

Abstract

The utility model relates to an aircraft head form ribbon, include: the device comprises a head structure, a fixed seat, a first binding strip and a second binding strip, wherein one end of the fixed seat is connected with the head structure; the first ribbon strip and the second ribbon strip are fixed on the same surface and are symmetrically arranged; a plurality of first positioning holes are formed in the first ribbon strip, and a plurality of second positioning holes are formed in the second ribbon strip; a first through hole and a second through hole are symmetrically formed in the fixed seat, a first clamping block is arranged on one side wall of the first through hole, and a second clamping block is arranged on one side wall of the second through hole; the first strap bundling strip is connected with the first through hole, and the second strap bundling strip is connected with the second through hole; the first clamping block is clamped with the first positioning hole, and the second clamping block is clamped with the second positioning hole. The utility model discloses a set up two through-holes and join in marriage two and prick the tape and promote space use degree.

Description

Aircraft head-shaped ribbon

Technical Field

The utility model relates to a ribbon technical field specifically is aircraft head form ribbon.

Background

The wire harness binding belt is mainly used for binding objects and is widely applied to various fields. Aircraft headstraps are used more in applications where it is necessary to further secure or lift the bound object. The existing airplane head binding belt only has a single binding bundle, is not sufficient for space application, and is easy to omit when being placed singly.

SUMMERY OF THE UTILITY MODEL

The utility model discloses just to prior art exist not enough, provide aircraft head form ribbon.

In order to solve the above problems, the utility model adopts the following technical proposal:

an aircraft nose tie, comprising: the device comprises a head structure, a fixed seat, a first binding strip and a second binding strip, wherein one end of the fixed seat is connected with the head structure; the first ribbon strip and the second ribbon strip are fixed on the same surface and are symmetrically arranged; a plurality of first positioning holes are formed in the first ribbon strip, and a plurality of second positioning holes are formed in the second ribbon strip; a first through hole and a second through hole are symmetrically formed in the fixed seat, a first clamping block is arranged on one side wall of the first through hole, and a second clamping block is arranged on one side wall of the second through hole; the first strap bundling strip is connected with the first through hole, and the second strap bundling strip is connected with the second through hole; the first clamping block is clamped with the first positioning hole, and the second clamping block is clamped with the second positioning hole.

As an improvement of the above technical solution, the head structure includes: the airplane comprises an airplane head, side plates fixed on two sides of the airplane head, and a trunk, wherein one end of the trunk is arranged on a fixed seat; the aircraft head is fixed on the other end of the trunk; and the bottom surface of the side plate is provided with a positioning block.

As an improvement of the above technical solution, the head structure further includes: baffles arranged at two sides of the trunk; the baffle is positioned between the side plate and the fixed seat and is in an arc shape; two ends of the baffle are provided with abutting blocks.

As an improvement of the above technical scheme, a fixed block is arranged on the fixed seat, and the fixed block and the trunk are respectively arranged on two opposite side surfaces of the fixed seat; the first binding belt strip and the second binding belt strip are both arranged on the fixing block.

As an improvement of the technical scheme, first grooves are symmetrically arranged on the top surface and the bottom surface of the first binding strip, and the first grooves are positioned on the outer side of the first positioning hole; and second grooves are symmetrically arranged on the top surface and the bottom surface of the second binding strip and are positioned on the outer sides of the second positioning holes.

As an improvement of the technical scheme, the outer end of the first binding belt strip is provided with a joint, and the sectional area of the joint is smaller than that of the first binding belt strip.

Compared with the prior art, the utility model discloses an implement the effect as follows:

the utility model discloses a set up two through-holes and join in marriage two ribbon strips and promote space use degree, bind the mechanism through setting up whole ribbon including the head structure of aircraft head fixes, promote the rigidity of fixing base through setting up the fixed block, realize fast alignment through setting up recess and joint and insert. The device fully utilizes the binding space by arranging the double holes and the double binding strips, improves the relevance of binding objects and avoids omission.

Drawings

Fig. 1 is a front view of a tie of the present invention;

fig. 2 is a left side view of the binding band of the present invention.

In the figure: the aircraft nose comprises a head structure 1, an aircraft nose 11, a trunk 111, a side plate 12, a positioning block 121, a baffle 13, a support block 131, a fixing seat 2, a first through hole 21, a first clamping block 211, a second through hole 22, a second clamping block 221, a fixing block 23, a first binding strip 3, a first positioning hole 31, a first groove 32, a joint 33, a second binding strip 4, a second positioning hole 41, and a second groove 42.

Detailed Description

The present invention will be described with reference to specific embodiments.

Fig. 1 is a front view of the binding band of the present invention, and fig. 2 is a left side view of the binding band of the present invention, as shown in fig. 1 and fig. 2. The ribbon includes: the head structure comprises a head structure 1, a fixed seat 2 with one end connected with the head structure 1, a first binding strip 3 installed at the other end of the fixed seat 2, and a second binding strip 4 installed on the fixed seat 2. The first band tie 3 and the second band tie 4 are fixed on the same surface and are symmetrically arranged. The first tape 3 is provided with a plurality of first positioning holes 31, and the second tape 4 is provided with a plurality of second positioning holes 41.

The fixing base 2 is symmetrically provided with a first through hole 21 and a second through hole 22, one side wall of the first through hole 21 is provided with a first clamping block 211, and one side wall of the second through hole 22 is provided with a second clamping block 221. The first strap 3 is connected to the first through-hole 21, and the second strap 4 is connected to the second through-hole 22. The first latch 211 is connected to the first positioning hole 31 in a snap-fit manner, and the second latch 221 is connected to the second positioning hole 41 in a snap-fit manner.

The original airplane head tying belts are all arranged in a single hole, and double through holes are arranged to match with double tying belts. The object is fixed by the binding strip, the first binding strip 3 and the second binding strip 4 are respectively folded towards two sides, are respectively connected with the first through hole 21 and the second through hole 22, and are adjusted to be in proper positions through clamping of the clamping blocks and the positioning holes. The head structure 1 is fixed, so that a plurality of objects can be bound and placed at the same time, the space is effectively utilized, and related objects are bound and placed together by the structure, so that omission is avoided.

The head structure 1 comprises: the aircraft comprises an aircraft head 11, side plates 12 fixed on two sides of the aircraft head 11, and a trunk 111 with one end arranged on a fixed seat 2. The aircraft head 11 is fixed to the other end of the trunk 111. A positioning block 121 is arranged on the bottom surface of the side plate 12. The side plates 12 can be retracted, the aircraft head 11 penetrates through the fixing holes, the side plates 12 are retracted when penetrating, the side plates penetrate through the rear side plates 12 to be expanded, and the positioning blocks 121 are in contact with the end faces of the plates to play a positioning role. The fixing mode is simple and convenient and easy to disassemble.

The head structure 1 further comprises: baffles 13 are provided on both sides of the trunk 111. The baffle 13 is positioned between the side plate 12 and the fixed seat 2 and is in a circular arc shape. Two ends of the baffle 13 are provided with abutting blocks 131. After the side plate 12 passes through the fixed orifices, the baffle 13 is stressed and bent, and is matched with the side plate 12 to be abutted against two sides of the fixed plate, so that the trunk 111 is prevented from shaking and running, the positioning fixed seat 2 is used, and the position of the aircraft head 11 is stabilized. The abutting block 131 contacts with the end face before penetrating, and plays a role of protecting the baffle 13.

The fixing seat 2 is provided with a fixing block 23, and the fixing block 23 and the trunk 111 are respectively arranged on two opposite side faces of the fixing seat 2. The first and

second tape ties

3 and 4 are mounted on the fixing block 23. The fixing block 23 is used for improving the structural rigidity of the fixing base 2, and the first positioning hole 31 and the second positioning hole 41 are far away from the fixing base 2, so that the two strapping strips can be conveniently folded and fixed.

First grooves 32 are symmetrically formed in the top surface and the bottom surface of the first strap 3, and the first grooves 32 are located on the outer side of the first positioning hole 31. And second grooves 42 are symmetrically arranged on the top surface and the bottom surface of the second band bundling strip 4, and the second grooves 42 are positioned at the outer sides of the second positioning holes 41. The contact area of the section passing through the through hole is reduced, so that the contact resistance is reduced, the band is helped to be exposed at the other side of the through hole quickly, and the band is convenient to pull.

The outer end of the first band tie 3 is provided with a joint 33, and the sectional area of the joint 33 is smaller than that of the first band tie 3. This arrangement can help align the first strap 3 with the first through hole 21.

It is noted that it is not necessary that the first strap 3 is connected to the first through hole 21 and the second strap 4 is connected to the second through hole 22. This connection relationship may also be reversed and does not affect the utility model.

It will be apparent to those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims and their equivalents, the present invention is also intended to include such modifications and variations.

Claims

1. Aircraft nose form ribbon, its characterized in that includes: the device comprises a head structure (1), a fixed seat (2) with one end connected with the head structure (1), a first binding strip (3) arranged at the other end of the fixed seat (2), and a second binding strip (4) arranged on the fixed seat (2); the first binding belt strip (3) and the second binding belt strip (4) are fixed on the same surface and are symmetrically arranged; a plurality of first positioning holes (31) are formed in the first tape (3), and a plurality of second positioning holes (41) are formed in the second tape (4);

a first through hole (21) and a second through hole (22) are symmetrically arranged on the fixed seat (2), a first clamping block (211) is arranged on one side wall of the first through hole (21), and a second clamping block (221) is arranged on one side wall of the second through hole (22); the first strap (3) is connected with the first through hole (21), and the second strap (4) is connected with the second through hole (22); the first clamping block (211) is clamped with the first positioning hole (31), and the second clamping block (221) is clamped with the second positioning hole (41).

2. Aircraft nose tie according to claim 1, characterised in that the head structure (1) comprises: the aircraft comprises an aircraft head (11), side plates (12) fixed on two sides of the aircraft head (11), and a trunk (111) with one end arranged on a fixed seat (2); the aircraft head (11) is fixed on the other end of the trunk (111); and a positioning block (121) is arranged on the bottom surface of the side plate (12).

3. Aircraft nose tie according to claim 2, characterized in that said head structure (1) further comprises: baffles (13) arranged at two sides of the trunk (111); the baffle (13) is positioned between the side plate (12) and the fixed seat (2) and is arc-shaped; two ends of the baffle (13) are provided with abutting blocks (131).

4. An aircraft nose-shaped ribbon according to claim 2, characterized in that the fixing seat (2) is provided with a fixing block (23), and the fixing block (23) and the trunk (111) are respectively arranged on two opposite side surfaces of the fixing seat (2); the first binding belt strip (3) and the second binding belt strip (4) are both arranged on the fixing block (23).

5. Aircraft nose tie according to claim 1, characterised in that the first tie strip (3) is provided with first grooves (32) symmetrically on the top and bottom, the first grooves (32) being located outside the first positioning hole (31); and second grooves (42) are symmetrically formed in the top surface and the bottom surface of the second binding strip (4), and the second grooves (42) are located on the outer sides of the second positioning holes (41).

6. Aircraft nose tie according to claim 1, characterised in that the outer end of the first tie strip (3) is provided with a joint (33), the cross-sectional area of the joint (33) being smaller than the cross-sectional area of the first tie strip (3).