CN107985615A - A kind of unmanned plane active safety feature - Google Patents
A kind of unmanned plane active safety feature Download PDFInfo
- Publication number
- CN107985615A CN107985615A CN201711331270.0A CN201711331270A CN107985615A CN 107985615 A CN107985615 A CN 107985615A CN 201711331270 A CN201711331270 A CN 201711331270A CN 107985615 A CN107985615 A CN 107985615A
- Authority
- CN
- China
- Prior art keywords
- button
- telescopic rod
- unmanned plane
- frame
- safety feature
- Prior art date
- 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.)
- Pending
Links
- 238000009434 installation Methods 0.000 claims abstract description 11
- 238000003466 welding Methods 0.000 claims description 2
- 208000032826 Ring chromosome 3 syndrome Diseases 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000000926 separation method Methods 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Support Of Aerials (AREA)
Abstract
The invention discloses a kind of unmanned plane active safety feature, its structure includes installation base station, rack, frame ground seat ring, shelves frame, collision button, a kind of unmanned plane active safety feature of the present invention, button is collided when being used and collides wall, button snap-gauge is driven to be moved rearwards, telescopic rod embedded slot deviates from the connection of button snap-gauge, adjustable spring props up pop-up telescopic rod, drive lever pop-up, by the way that equipped with shelves frame, the place for carrying out protection fragility can actively be ejected when wall is struck by realizing the safety device.
Description
Technical field
The present invention is a kind of unmanned plane active safety feature, belongs to unmanned plane field.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel are by equipment such as radars, to it into line trace, positioning, remote control, remote measurement and Digital Transmission.Can be in radio
Take off as conventional airplane or launched with booster rocket under remote control, can also take aerial launch to by machine tool and fly.Recycling
When, the mode automatic Landing as conventional airplane landing mission can be used, can also be recycled by remote control parachute or block.Can
It is reused several times.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
Prior art discloses Application No.：A kind of special type for possessing counter unmanned plane function of CN201720106198.0
Unmanned plane, including unmanned plane body, the camera being arranged on unmanned plane body and unmanned plane counter equipment, the unmanned plane are anti-
Control equipment includes omnidirectional antenna, interference signal generator, power supply, controller and protection shell, the omnidirectional antenna, interference signal
Generator and power supply are placed in protection shell, and the camera, power supply, interference signal generator are connected with controller respectively, institute
Interference signal generator is stated to be connected with omnidirectional antenna.The extraordinary unmanned plane for possessing counter unmanned plane function of the present invention, is provided with
Unmanned plane breaks through equipment, it can be by omnidirectional antenna come the other unmanned planes of comprehensive counter.Due to unmanned plane can fly it is higher
Highly, so the special type unmanned plane breaches the limitation of other low latitudes counter equipment completely.But the unmanned plane of the prior art is prevented
Protection unit security is not high enough.
The content of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of unmanned plane active safety feature, to solve
The problem of unmanned plane protective device security of the prior art is not high enough.
To achieve these goals, the present invention is to realize by the following technical solutions：A kind of unmanned plane active safety
Device, its structure include installation base station, rack, frame ground seat ring, shelves frame, collision button, and four side of the installation base station is welded with
Rack, the gantry base boxing are connected on bottom of the frame, and the shelves frame is movably fixed to above frame ground seat ring, and the collision is pressed
Key is movably nested at frame ground seat ring side, and the collision button is connected with shelves frame internal engagement；The shelves are provided with lever, stretch
Contracting bar, telescopic rod embedded slot, limiting plate, adjustable spring, base shaft, button axle, button axis spring, button snap-gauge, under the lever
Side is welded with two telescopic rods, and the telescopic rod embedded slot is opened in telescopic rod surface, and the limiting plate is welded on telescopic rod
Lower section, the adjustable spring tensioning are nested in the lower section of limiting plate, and the telescopic rod is inside base shaft, the button axle welding
In front of button snap-gauge, for the button axis spring among button snap-gauge and button axle, the collision button is welded on button
Axis front end, the button snap-gauge coordinate with telescopic rod embedded slot, and the base shaft is welded on gantry base ring surface, described to include installation
A diameter of 10cm of base station, the lever are half arc rod structure, and the collision button is circular discs assembling structure, described spacing
Sheet separation coordinates inside base shaft.
Beneficial effect
A kind of unmanned plane active safety feature of the present invention, button is collided when being used and collides wall, drive button
Snap-gauge is moved rearwards, and telescopic rod embedded slot deviates from the connection of button snap-gauge, and adjustable spring props up pop-up telescopic rod, drives lever bullet
Go out, by the way that equipped with shelves frame, the ground for carrying out protection fragility can actively be ejected when wall is struck by realizing the safety device
Side.
Brief description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is a kind of structure diagram of unmanned plane active safety feature of the present invention.
Fig. 2 is the structure diagram of shelves frame of the present invention.
In figure：Installation base station -1, rack -2, frame ground seat ring -3, shelves frame -4, collision button -5, lever -40, telescopic rod -
41st, telescopic rod embedded slot -42, limiting plate -43, adjustable spring -44, base shaft -45, button axle -46, button axis spring -47, button
Snap-gauge -48.
Embodiment
To make the technical means, the creative features, the aims and the efficiencies achieved by the present invention easy to understand, with reference to
Embodiment, the present invention is further explained.
- Fig. 2 is please referred to Fig.1, the present invention provides a kind of unmanned plane active safety feature technical solution：A kind of unmanned plane is actively
Safety device, its structure include installation base station 1, rack 2, frame ground seat ring 3, shelves frame 4, collision button 5, the installation base station 1
Organic frame 2 is welded in four sides, and the frame ground seat ring 3 is welded on 2 bottom of rack, and the shelves frame 4 is movably fixed to frame ground seat ring 3
Top, the collision button 5 are movably nested at 3 side of frame ground seat ring, and the collision button 5 is connected with 4 internal engagement of shelves frame；
The shelves frame 4 is equipped with lever 40, telescopic rod 41, telescopic rod embedded slot 42, limiting plate 43, adjustable spring 44, base shaft 45, button axle
46th, button axis spring 47, button snap-gauge 48, the lower section of lever 40 are welded with two telescopic rods 41, the telescopic rod embedded slot
42 are opened in 41 surface of telescopic rod, and the limiting plate 43 is welded on the lower section of telescopic rod 41, and the adjustable spring 44 is tensioned nesting
In the lower section of limiting plate 43, for the telescopic rod 41 inside base shaft 45, the button axle 46 is welded on the front of button snap-gauge 48,
For the button axis spring 47 among button snap-gauge 48 and button axle 46, the collision button 5 is welded on 46 front end of button axle,
The button snap-gauge 48 coordinates with telescopic rod embedded slot 42, and the base shaft 45 is welded on 3 surface of frame ground seat ring, described to include installation
A diameter of 10cm of base station 1, the lever 40 are half arc rod structure, and the collision button 5 is circular discs assembling structure, described
43 clearance fit of limiting plate is inside base shaft 45.
Shelves frame 4 described in this patent is the shelf for protecting propeller to be damaged, and PVC material, length is original after pop-up
Twice.
Button 5 is collided when being used and collides wall, drives button snap-gauge 48 to be moved rearwards, telescopic rod embedded slot 42
Deviate from the connection of button snap-gauge 48, adjustable spring 44 props up pop-up telescopic rod 41, drives lever 40 to eject.
The basic principles, main features and the advantages of the invention have been shown and described above, for this area skill
For art personnel, it is clear that the invention is not restricted to the details of above-mentioned one exemplary embodiment, and without departing substantially from the present invention spirit or
In the case of essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes fallen in the implication and scope of the equivalency of claim in the present invention
It is interior.Any reference numeral in claim should not be considered as to the involved claim of limitation.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical solution, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (5)
1. a kind of unmanned plane active safety feature, its structure includes installation base station (1), rack (2), frame ground seat ring (3), shelves frame
(4), button (5) is collided, it is characterised in that：
The installation base station (1) four side welding organic frame (2), the frame ground seat ring (3) is welded on rack (2) bottom, described
Shelves frame (4) is movably fixed to above frame ground seat ring (3), and the collision button (5) is movably nested at frame ground seat ring (3) side
Face, the collision button (5) are connected with shelves frame (4) internal engagement；
The shelves frame (4) is equipped with lever (40), telescopic rod (41), telescopic rod embedded slot (42), limiting plate (43), adjustable spring
(44), base shaft (45), button axle (46), button axis spring (47), button snap-gauge (48), lever (40) lower section are welded with two
Root telescopic rod (41), the telescopic rod embedded slot (42) are opened in telescopic rod (41) surface, and the limiting plate (43), which is welded on, stretches
The lower section of contracting bar (41), adjustable spring (44) tensioning are nested in the lower section of limiting plate (43), and the telescopic rod (41) is embedded in
Base shaft (45) is internal, and the button axle (46) is welded in front of button snap-gauge (48), and the button axis spring (47) is embedded in button
Among snap-gauge (48) and button axle (46), the collision button (5) is welded on button axle (46) front end, the button snap-gauge (48)
Coordinate with telescopic rod embedded slot (42), the base shaft (45) is welded on frame ground seat ring (3) surface.
A kind of 2. unmanned plane active safety feature according to claim 1, it is characterised in that：It is described to include installation base station (1)
A diameter of 10cm.
A kind of 3. unmanned plane active safety feature according to claim 1, it is characterised in that：The lever (40) is half arc
Shape rod structure.
A kind of 4. unmanned plane active safety feature according to claim 1, it is characterised in that：It is described collision button (5) be
Circular discs assembling structure.
A kind of 5. unmanned plane active safety feature according to claim 1, it is characterised in that：Limiting plate (43) gap
Coordinate internal in base shaft (45).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711331270.0A CN107985615A (en) | 2017-12-13 | 2017-12-13 | A kind of unmanned plane active safety feature |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711331270.0A CN107985615A (en) | 2017-12-13 | 2017-12-13 | A kind of unmanned plane active safety feature |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107985615A true CN107985615A (en) | 2018-05-04 |
Family
ID=62038398
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711331270.0A Pending CN107985615A (en) | 2017-12-13 | 2017-12-13 | A kind of unmanned plane active safety feature |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107985615A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108910029A (en) * | 2018-08-02 | 2018-11-30 | 滨州学院 | A kind of protection mechanism of unmanned plane wing |
-
2017
- 2017-12-13 CN CN201711331270.0A patent/CN107985615A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108910029A (en) * | 2018-08-02 | 2018-11-30 | 滨州学院 | A kind of protection mechanism of unmanned plane wing |
| CN108910029B (en) * | 2018-08-02 | 2021-06-04 | 滨州学院 | Protection mechanism of unmanned aerial vehicle wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180504 |