CN110510136A - A kind of unmanned plane wing protective device - Google Patents
A kind of unmanned plane wing protective device Download PDFInfo
- Publication number
- CN110510136A CN110510136A CN201810488036.7A CN201810488036A CN110510136A CN 110510136 A CN110510136 A CN 110510136A CN 201810488036 A CN201810488036 A CN 201810488036A CN 110510136 A CN110510136 A CN 110510136A
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- CN
- China
- Prior art keywords
- protective frame
- wing
- unmanned plane
- protective
- fixing bolt
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 230000001681 protective effect Effects 0.000 title claims abstract description 93
- 238000003466 welding Methods 0.000 claims description 6
- 238000009434 installation Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of unmanned plane wing protective devices, including wing, the two sides of the wing are respectively connected with the first protective frame, the inside of first protective frame, which corresponds to, is provided with sliding slot at the position of wing, the inside of the sliding slot is provided with rubber block at a side position of wing, spring is connected on the inside of the rubber block, triangular prism is connected on the outside of first protective frame, and first one end of protective frame be provided with card slot, the top of first protective frame is connected with the first fixing bolt above card slot, and first protective frame top far from being connected with the second fixing bolt at a side position of the first fixing bolt.The present invention can protect the edge of wing, reduce the probability for causing brokenly ring when colliding to wing, the impact force to wing can be also buffered when unmanned plane collides, while reduce influence of the protective frame installation to unmanned plane speed.
Description
Technical field
The present invention relates to unmanned plane field, specially a kind of unmanned plane wing protective device.
Background technique
With being constantly progressive for modern society, unmanned air vehicle technique level is also higher and higher, since unmanned plane is driven without personnel
It sails, and easy to operate flexible, is all widely used in a variety of applications in every field, but unmanned plane works in some rugged environments
When easily there is failure unmanned plane caused to damage, in order to reduce the loss of unmanned plane, it is therefore desirable to design a kind of unmanned plane wing and protect
Protection unit.
But it is poor to the edge safeguard measure of wing for the protective device of unmanned plane wing currently on the market, in nothing
It is man-machine to cause brokenly ring larger on wing when colliding, impact force when unmanned plane collides to wing can not be buffered in.
Summary of the invention
The present invention provides a kind of unmanned plane wing protective device, can effectively solve mentioned above in the background art ask
Topic.
To achieve the above object, the invention provides the following technical scheme: a kind of unmanned plane wing protective device, including machine
The wing, the two sides of the wing are respectively connected with the first protective frame, and the inside of first protective frame corresponds to be arranged at the position of wing
There is sliding slot, the inside of the sliding slot is provided with rubber block at a side position of wing, is connected on the inside of the rubber block
Spring is connected with triangular prism on the outside of first protective frame, and one end of the first protective frame is provided with card slot, and described first is anti-
The top of retaining frame is connected with the first fixing bolt, and corresponding first fixing bolt in top of the first protective frame above card slot
Position at be provided with the first internal thread hole, the top of first protective frame at a side position of the first fixing bolt far from connecting
It is connected to the second fixing bolt, and is provided with the second internal screw thread at the position of corresponding second fixing bolt in top of the first protective frame
Hole, first protective frame are connected with the second protective frame close to the side of card slot, and one end of second protective frame corresponds to card slot
Position at be provided with fixed column, and the inside of the second protective frame corresponds to and is provided with fixing groove at the position of wing, described first
The inside of protective frame, which is located at two side positions up and down of wing, is respectively connected with fixed link.
As a preferred technical solution of the present invention, the width of the sliding slot is greater than the thickness of wing, the wing with
It is bolted to connection between first protective frame.
As a preferred technical solution of the present invention, connected between first protective frame and the second protective frame by card slot
It connects, the internal diameter of the card slot is greater than the outer diameter of fixed column.
As a preferred technical solution of the present invention, the connection between the fixed link and the first protective frame is welding,
And fixed link is at least provided with four.
As a preferred technical solution of the present invention, the connection between the spring and the first protective frame is welding, and
The length of spring is less than the depth of sliding slot.
Compared with prior art, beneficial effects of the present invention:
1, the present invention passes through the first protective frame of setting and the second protective frame, and in the inside pair of the first protective frame and the second protective frame
It answers and sliding slot and fixing groove is respectively set at the position of wing, protected convenient for the edge to wing.
2, the probability for causing brokenly ring when the present invention collides for the ease of reducing to wing, in sliding slot and fixing groove
Portion is provided with rubber block at a side position of wing.
3, the present invention for the ease of colliding when can buffer impact force to wing, be connected on the inside of rubber block
Spring, and be welded and fixed in the other end of spring with protective frame.
4, the present invention reduces influence of the protective frame installation to unmanned plane speed, first for the ease of reducing air drag
Triangular prism is connected on the outside of protective frame.
Detailed description of the invention
Attached drawing is used to provide further understanding of the present invention, and constitutes part of specification, with reality of the invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention.
In the accompanying drawings:
Fig. 1 is schematic structural view of the invention；
Fig. 2 is main view of the invention；
Fig. 3 is the structural schematic diagram of the second protective frame of the invention；
Fig. 4 is the structural schematic diagram of the first protective frame of the invention；
Figure label: 1, wing；2, the first protective frame；3, sliding slot；4, rubber block；5, spring；6, triangular prism；7, card slot；8,
One fixing bolt；9, fixed link；10, the second fixing bolt；11, the second protective frame；12, fixing groove；13, fixed column；14, second
Internal thread hole；15, the first internal thread hole.
Specific embodiment
Hereinafter, preferred embodiments of the present invention will be described with reference to the accompanying drawings, it should be understood that preferred reality described herein
Apply example only for the purpose of illustrating and explaining the present invention and is not intended to limit the present invention.
Embodiment: as shown in Figs 1-4, the present invention provides a kind of technical solution, a kind of unmanned plane wing protective device, including
Wing 1, the two sides of wing 1 are respectively connected with the first protective frame 2, and the inside of the first protective frame 2 corresponds to be provided at the position of wing 1
The inside of sliding slot 3, sliding slot 3 is provided with rubber block 4 at a side position of wing 1, and the inside of rubber block 4 is connected with spring 5,
The outside of first protective frame 2 is connected with triangular prism 6, and one end of the first protective frame 2 is provided with card slot 7, the top of the first protective frame 2
The top close to card slot 7 is held to be connected with the first fixing bolt 8, and the position of corresponding first fixing bolt 8 in top of the first protective frame 2
The place of setting is provided with the first internal thread hole 15, and the top of the first protective frame 2 at a side position of the first fixing bolt 8 far from being connected with
Second fixing bolt 10, and the second internal screw thread is provided at the position of corresponding second fixing bolt 10 in top of the first protective frame 2
Hole 14, the first protective frame 2 are connected with the second protective frame 11 close to the side of card slot 7, and one end of the second protective frame 11 corresponds to card slot 7
Position at be provided with fixed column 13, and the inside of the second protective frame 11 corresponds to and is provided with fixing groove 12 at the position of wing 1,
The inside of one protective frame 2, which is located at two side positions up and down of wing 1, is respectively connected with fixed link 9.
It can extend into the inside of sliding slot 3 for the ease of wing 1, in the present embodiment, it is preferred that the width of sliding slot 3 is greater than machine
The thickness of the wing 1 is bolted to connection between wing 1 and the first protective frame 2.
For the ease of the fixation between the first protective frame 2 and the second protective frame 11, in the present embodiment, it is preferred that first is anti-
It is connected between retaining frame 2 and the second protective frame 11 by card slot, the internal diameter of card slot 7 is greater than the outer diameter of fixed column 13.
For the ease of the fixation of fixed link 9, and then the first protective frame 2 can be made to stablize, in the present embodiment, it is preferred that Gu
Connection between fixed pole 9 and the first protective frame 2 is welding, and fixed link 9 is at least provided with four.
For the ease of the installation of spring 5, in the present embodiment, it is preferred that the connection between spring 5 and the first protective frame 2 is
Welding, and the length of spring 5 is less than the depth of sliding slot 3.
The working principle of the invention and process for using: firstly, the first protective frame 2 is respectively connected in the two sides of wing 1, first
The side of protective frame 2 is connected with the second protective frame 11, and the inside of the first protective frame 2 corresponds to and is provided with sliding slot at the position of wing 1
3, the inside of the second protective frame 11 corresponds to and is provided with fixing groove 12 at the position of wing 1, protects convenient for the edge to wing 1
Shield；Secondly, rubber block 4 is provided at a side position of wing 1 in the inside of sliding slot 3 and fixing groove 12, convenient for reducing
The probability of ring is caused brokenly when colliding to wing；Then, it is connected with spring 5 in the inside of rubber block 4, and in the another of spring 5
One end is welded and fixed with protective frame, and the impact force to wing 1 can be buffered when convenient for colliding；Finally, in the first protective frame 2
Outside be connected with triangular prism 6, convenient for reducing air drag, reduce protective frame and influence to unmanned plane speed be installed.
Finally, it should be noted that being not intended to restrict the invention the foregoing is merely preferred embodiment of the invention, to the greatest extent
Present invention has been described in detail with reference to the aforementioned embodiments for pipe, for those skilled in the art, still can be with
It modifies the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features.It is all
Within the spirit and principles in the present invention, any modification, equivalent replacement, improvement and so on should be included in guarantor of the invention
Within the scope of shield.
Claims (5)
1. a kind of unmanned plane wing protective device, including wing (1), it is characterised in that: the two sides of the wing (1) are respectively connected with
First protective frame (2), the inside of first protective frame (2) correspond to and are provided with sliding slot (3), the cunning at the position of wing (1)
The inside of slot (3) is provided with rubber block (4) at a side position of wing (1), is connected with bullet on the inside of the rubber block (4)
Spring (5) is connected with triangular prism (6) on the outside of first protective frame (2), and one end of the first protective frame (2) is provided with card slot
(7), the top of first protective frame (2) is connected with the first fixing bolt (8) above card slot (7), and the first protection
It is provided with the first internal thread hole (15) at the position at the top of frame (2) corresponding first fixing bolt (8), first protective frame
(2) top is connected with the second fixing bolt (10) at the side position far from the first fixing bolt (8), and the first protective frame
(2) it is provided with the second internal thread hole (14) at the position at top corresponding second fixing bolt (10), first protective frame (2)
Side close to card slot (7) is connected with the second protective frame (11), and one end of second protective frame (11) corresponds to the position of card slot (7)
The place of setting is provided with fixed column (13), and the inside of the second protective frame (11) corresponds to and is provided with fixing groove at the position of wing (1)
(12), the inside of first protective frame (2), which is located at two side positions up and down of wing (1), is respectively connected with fixed link (9).
2. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: the width of the sliding slot (3)
Greater than the thickness of wing (1), it is bolted to connection between the wing (1) and the first protective frame (2).
3. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: first protective frame (2)
It is connect between the second protective frame (11) by card slot, the internal diameter of the card slot (7) is greater than the outer diameter of fixed column (13).
4. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: the fixed link (9) and the
Connection between one protective frame (2) is welding, and fixed link (9) is at least provided with four.
5. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: the spring (5) and first
Connection between protective frame (2) is welding, and the length of spring (5) is less than the depth of sliding slot (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810488036.7A CN110510136A (en) | 2018-05-21 | 2018-05-21 | A kind of unmanned plane wing protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810488036.7A CN110510136A (en) | 2018-05-21 | 2018-05-21 | A kind of unmanned plane wing protective device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110510136A true CN110510136A (en) | 2019-11-29 |
Family
ID=68621695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810488036.7A Withdrawn CN110510136A (en) | 2018-05-21 | 2018-05-21 | A kind of unmanned plane wing protective device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110510136A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113247275A (en) * | 2021-06-25 | 2021-08-13 | 斗山创新(深圳)有限公司 | Hydrogen fuel cell system for industrial-grade vertical take-off and landing fixed wing unmanned aerial vehicle |
| CN113669352A (en) * | 2021-08-26 | 2021-11-19 | 嘉兴涵祺汽配科技股份有限公司 | Double-end automobile bolt with protect function |
-
2018
- 2018-05-21 CN CN201810488036.7A patent/CN110510136A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113247275A (en) * | 2021-06-25 | 2021-08-13 | 斗山创新(深圳)有限公司 | Hydrogen fuel cell system for industrial-grade vertical take-off and landing fixed wing unmanned aerial vehicle |
| CN113669352A (en) * | 2021-08-26 | 2021-11-19 | 嘉兴涵祺汽配科技股份有限公司 | Double-end automobile bolt with protect function |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20191129 |