CN208325614U - A kind of remote sensing unmanned plane with permanent protective property energy - Google Patents
A kind of remote sensing unmanned plane with permanent protective property energy Download PDFInfo
- Publication number
- CN208325614U CN208325614U CN201820494822.3U CN201820494822U CN208325614U CN 208325614 U CN208325614 U CN 208325614U CN 201820494822 U CN201820494822 U CN 201820494822U CN 208325614 U CN208325614 U CN 208325614U
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- cabinet
- rack
- pop
- parachute
- spring
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Abstract
The utility model discloses a kind of remote sensing unmanned planes with permanent protective property energy, including body, organic frame is arranged in the bottom end of the body, and the rack is fixedly connected with the body, spring stack is provided with below the rack, and the spring stack is fixed with the rack, damping spring is provided on the outside of the spring stack, and the damping spring is fixed with the spring stack；If there is the situation of body failure or battery electric power deficiency, the pop-up of the small-sized parachute of rest-set flip-flop automatic trigger struts, body is avoided directly to drop to ground, body is set the problem of damaging of falling occur, keep the flight of body safer, and damping spring is equipped in the lower section of rack, damping spring can be during body takeoff and landing, play cushioning effect, body is avoided to collide in landing with ground, make body strenuous vibration, the part on body is caused to be damaged, keeps the flight of body more stable.
Description
Technical field
The utility model belongs to remote sensing air vehicle technique field, and in particular to it is a kind of with permanent protective property can remote sensing nobody
Machine.
Background technique
UAV abbreviation unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer, unmanned plane presses application field, can be divided into army
With with civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone, civilian aspect, and unmanned plane industrial application is that unmanned plane is real
Rigid need, at present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, some fields of disaster relief, movies-making are applied.
When in use, unmanned plane is in flight course for original remote sensing unmanned plane, if body breaks down or battery occurs
It is lost excessive, electric power cannot be provided for body and flown by body, body can be made to fall, and then damage may be brought to body
It is bad, it is also possible to will lead to body crash.
Utility model content
The purpose of this utility model is to provide a kind of remote sensing unmanned planes with permanent protective property energy, to solve above-mentioned background
Original remote sensing unmanned plane is proposed in technology when in use, unmanned plane is in flight course, if body breaks down or battery goes out
It is now lost excessive, electric power cannot be provided for body and flown by body, body can be made to fall, and then may brought to body
Damage, it is also possible to will lead to the problem of body crashes.
To achieve the above object, the utility model provides the following technical solutions: it is a kind of with permanent protective property can remote sensing without
It is man-machine, including body, organic frame is arranged in the bottom end of the body, and the rack is fixedly connected with the body, the rack
Lower section be provided with spring stack, and the spring stack is fixed with the rack, is provided with damping on the outside of the spring stack
Spring, and the damping spring is fixed with the spring stack, damping base is provided with below the spring stack, and described
Damping base is fixedly connected with the spring stack, and cabinet, and the cabinet and the rack spiral shell are provided with above the rack
Fixation is connect, is provided with wing fixed frame on the outside of the cabinet, and the wing fixed frame and the cabinet are spirally connected fixation, it is described
Wing mounting base is provided on the left of wing fixed frame, and the wing mounting base is fixedly connected with the wing fixed frame, institute
State and be provided with wing on the outside of wing mounting base, and the wing is fixed with the wing fixed frame, the cabinet it is upper
Surface is provided with control switch, and the control switch is fixedly connected with the cabinet, and the upper surface of the cabinet offers drop
Umbrella mounting groove is fallen, pop-up shaft is provided on the inside of the parachute mounting groove, and the pop-up shaft is fixed with the cabinet
It connects, pop-up flip lid is provided with above the parachute mounting groove, and pop-up flip lid leads to the parachute mounting groove
The pop-up shaft rotation connection is crossed, the parachute mounting groove is internally provided with small-sized parachute, the small-sized parachute
Lower section be provided with rest-set flip-flop, the rest-set flip-flop is fixed with the parachute mounting groove, the control switch and institute
Rest-set flip-flop is stated to be electrically connected with external power supply.
Preferably, it is opened up above the cabinet there are four slot, is equipped with fixing bolt, and institute in four slots
It states fixing bolt and the cabinet is spirally connected fixation.
Preferably, the quantity of the pop-up flip lid is two, and two pop-up flip lids pass through the pop-up shaft
It flips outward.
Preferably, the small-sized parachute is that can flick umbrella-shaped structure, and the small-sized parachute is triggered by the RS
Device pop-up.
Preferably, the inner bottom of the rack offers round slot, and the diameter and the bullet of the round slot
The diameter of spring column is equal, the quantity of the spring stack be it is multiple, multiple spring stacks are respectively symmetrically distributed in the rack
Four corners of lower section are provided with fixing seat above multiple spring stacks.
Compared with prior art, the utility model has the beneficial effects that the inner tip in cabinet offers parachute peace
Tankage is equipped with rest-set flip-flop and small-sized parachute in parachute mounting groove, when body is in flight course, if there is machine
The situation of body failure or battery electric power deficiency, rest-set flip-flop, which can incude, detects that the body problem, automatic trigger are small-sized
The pop-up of parachute struts, and body is avoided directly to drop to ground, so that body the problem of damaging of falling is occurred, further makes body
Flight it is safer, extend the service life of body, and be equipped with damping spring in the lower section of rack, damping spring can be in machine
During body takeoff and landing, cushioning effect is played, avoids body from colliding in landing with ground, shakes body acutely
It is dynamic, cause the part on body to be damaged, further makes the flight of body more stable.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the overlooking structure diagram of the utility model；
Fig. 3 is the vertical view A structural schematic diagram of the utility model；
In figure: 1- body, 2- spring stack, 3- damping base, 4- damping spring, 5- rack, 6- wing mounting base, 7- wing
The small-sized parachute of fixed frame, 8-, 9- wing, 10- fixing bolt, 11- control switch, 12- cabinet, 13- pop up shaft, 14- bullet
Flip lid, 15- parachute mounting groove, 16-RS trigger out.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1-3, the utility model provides a kind of technical solution: it is a kind of with permanent protective property can remote sensing nobody
Organic frame 5 is arranged in the bottom end of machine, including body 1, body 1, and rack 5 is fixedly connected with body 1, and the lower section of rack 5 is provided with
Spring stack 2, and spring stack 2 is fixed with rack 5, the outside of spring stack 2 is provided with damping spring 4, and damping spring 4 and bullet
Spring column 2 is fixed, and the lower section of spring stack 2 is provided with damping base 3, and damping base 3 is fixedly connected with spring stack 2, rack 5
Top be provided with cabinet 12, and cabinet 12 and rack 5 are spirally connected fixation, and the outside of cabinet 12 is provided with wing fixed frame 7, and machine
Wing fixed frame 7 and cabinet 12 are spirally connected fixation, and the left side of wing fixed frame 7 is provided with wing mounting base 6, and wing mounting base 6 with
Wing fixed frame 7 is fixedly connected, and the outside of wing mounting base 6 is provided with wing 9, and wing 9 engages admittedly with wing fixed frame 7
Fixed, the upper surface of cabinet 12 is provided with control switch 11, and control switch 11 is fixedly connected with cabinet 12, the upper surface of cabinet 12
Parachute mounting groove 15 is offered, the inside of parachute mounting groove 15 is provided with pop-up shaft 13, and pops up shaft 13 and cabinet
12 are fixedly connected, and the top of parachute mounting groove 15 is provided with pop-up flip lid 14, and pops up flip lid 14 and parachute mounting groove 15
It is rotatablely connected by pop-up shaft 13, parachute mounting groove 15 is internally provided with small-sized parachute 8, under small-sized parachute 8
Side is provided with rest-set flip-flop 16, and rest-set flip-flop 16 is fixed with parachute mounting groove 15, control switch 11 and rest-set flip-flop 16
It is electrically connected with external power supply.
In the present embodiment, the lower section of rack 5 is provided with spring stack 2, and the outside of spring stack 2 is provided with damping spring 4, spring
The lower section of column 2 is provided with damping base 3, for during 1 takeoff and landing of body, mitigating body 1 by damping spring 4
With the collision and frictional force on ground, avoids body 1 from colliding in landing with ground, make body strenuous vibration, lead to body 1
On part be damaged, further make the flight of body 1 more stable, the upper surface of cabinet 12 offers parachute mounting groove
15, the inside of parachute mounting groove 15 is provided with pop-up shaft 13, and the top of parachute mounting groove 15 is provided with pop-up flip lid 14,
Parachute mounting groove 15 is internally provided with small-sized parachute 8, and the lower section of small-sized parachute 8 is provided with rest-set flip-flop 16, is used for
It breaks down in the flight course of body 1 or electric power deficiency is when so that body 1 is fallen, it can be by rest-set flip-flop 16 from parachute
The small-sized parachute 8 of pop-up, slows down falling for body 1 in mounting groove 15, allows to fall to the ground under the safety of body 1, avoids machine
Quick the phenomenon that the damaging of crashing of body 1, further makes the use more safety and stability of body 1, and extend body 1 uses the longevity
Life.
Further, the top of cabinet 12 is opened up there are four slot, fixing bolt 10 is equipped in four slots, and fixed
Bolt 10 and cabinet 12 are spirally connected fixation.
In the present embodiment, the top of cabinet 12 is opened up there are four slot, fixing bolt 10 is equipped in four slots, and solid
Determine bolt 10 and cabinet 12 is spirally connected fixation, the installation for cabinet 12 is more stable, keeps body 1 whole stronger.
Further, the quantity of pop-up flip lid 14 is two, and two pop-up flip lids 14 are outside by pop-up shaft 13
Overturning.
In the present embodiment, the quantity of pop-up flip lid 14 is two, and two pop-ups flip lid 14 by pop up shaft 13 to
Outer overturning is used for ejecting flip lid 14 and flips outward the pop-up that will not hinder small-sized parachute 8 by pop-up shaft 13, do not popping up
When small-sized parachute 8, it can avoid falling into dust or impurity in cabinet 12, further with sealed cabinet 12 by pop-up flip lid 14
The use of small-sized parachute 8 is set not influence the normal work of body 1.
Further, small-sized parachute 8 is that can flick umbrella-shaped structure, and small-sized parachute 8 is popped up by rest-set flip-flop 16.
In the present embodiment, small-sized parachute 8 is that can flick umbrella-shaped structure, and small-sized parachute 8 passes through 16 bullet of rest-set flip-flop
Out, body 1 can be made smoothly to fall to the ground when body 1 breaks down and falls for the pop-up by small-sized parachute 8,
It can make the small-sized parachute 8 of the automatic spring in failure of body 1 by rest-set flip-flop 16, further make the flight of body 1 more
Safety.
Further, the inner bottom of rack 5 offers round slot, and the diameter of round slot and spring stack 2 is straight
Diameter is equal, the quantity of spring stack 2 be it is multiple, multiple spring stacks 2 are respectively symmetrically distributed in four corners of the lower section of rack 5,
The top of multiple spring stacks 2 is provided with fixing seat.
In the present embodiment, the inner bottom of rack 5 offers round slot, and the diameter of round slot and spring stack 2
Diameter is equal, the quantity of spring stack 2 be it is multiple, multiple spring stacks 2 are respectively symmetrically distributed in four turnings of the lower section of rack 5
Place, the top of multiple spring stacks 2 is provided with fixing seat, for body 1 in landing, by damping spring 4 can mitigate with
The collision dynamics on ground, spring stack 2 can be under pressure when body 1 lands, damping spring 4 pressed together, circle is passed through
Spring stack 2 is appeared when slot, fixing seat, which can fix shock structure 2, to fall off from rack 5, further make damping spring 4
Using more stable.
Rest-set flip-flop model 74LS279 in the utility model.
The working principle and process for using of the utility model: after the utility model installs, body 1 is put into place of working
Point connects external power supply, opens control switch 11, and by the takeoff and landing of remote control control body 1, the high speed of wing 9 is revolved
The change of team drives the rising of body 1, and body 1 is during flight, if body 1 breaks down or the insufficient feelings of battery electric power
Condition, rest-set flip-flop 16, which can incude, detects 1 problem of body, and the small-sized parachute of automatic trigger is out of parachute mounting groove 15
Pop-up struts, and keeps the landing of body 1 more stable, and the directly tenesmus of body 1 is avoided further to make the flight of body 1 more to ground
Add safety, damping spring 4 can play cushioning effect during 1 takeoff and landing of body, avoid body 1 in landing
It collides with ground, makes 1 strenuous vibration of body, the part on body 1 is caused to be damaged, further make the flight of body 1
It is more stable.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of remote sensing unmanned plane with permanent protective property energy, it is characterised in that: including body (1), the bottom end of the body (1)
It is arranged organic frame (5), and the rack (5) is fixedly connected with the body (1), is provided with spring below the rack (5)
Column (2), and the spring stack (2) is fixed with the rack (5), is provided with damping spring on the outside of the spring stack (2)
(4), and the damping spring (4) is fixed with the spring stack (2), is provided with damping bottom below the spring stack (2)
Seat (3), and the damping base (3) is fixedly connected with the spring stack (2), is provided with cabinet above the rack (5)
(12), and the cabinet (12) and the rack (5) are spirally connected fixation, are provided with wing fixed frame on the outside of the cabinet (12)
(7), and the wing fixed frame (7) and the cabinet (12) are spirally connected fixation, and the left side setting of the wing fixed frame (7) is organic
Wing mounting base (6), and the wing mounting base (6) is fixedly connected with the wing fixed frame (7), the wing mounting base (6)
Outside be provided with wing (9), and the wing (9) is fixed with the wing fixed frame (7), the cabinet (12) it is upper
Surface is provided with control switch (11), and the control switch (11) is fixedly connected with the cabinet (12), the cabinet (12)
Upper surface offer parachute mounting groove (15), be provided on the inside of the parachute mounting groove (15) pop-up shaft (13),
And the pop-up shaft (13) is fixedly connected with the cabinet (12), is provided with pop-up above the parachute mounting groove (15)
It renovates (14), and pop-up flip lid (14) and the parachute mounting groove (15) are rotated by the pop-up shaft (13) and connected
It connects, the parachute mounting groove (15) is internally provided with small-sized parachute (8), the lower section setting of the small-sized parachute (8)
Have rest-set flip-flop (16), the rest-set flip-flop (16) is fixed with the parachute mounting groove (15), the control switch
(11) it is electrically connected with external power supply with the rest-set flip-flop (16).
2. a kind of remote sensing unmanned plane with permanent protective property energy according to claim 1, it is characterised in that: the cabinet
(12) it is opened up above there are four slot, is equipped with fixing bolt (10) in four slots, and the fixing bolt (10)
It is spirally connected fixation with the cabinet (12).
3. a kind of remote sensing unmanned plane with permanent protective property energy according to claim 1, it is characterised in that: the pop-up is turned over
The quantity for covering (14) is two, and two pop-up flip lids (14) are flipped outward by the pop-up shaft (13).
4. a kind of remote sensing unmanned plane with permanent protective property energy according to claim 1, it is characterised in that: the small-sized drop
Falling umbrella (8) is that can flick umbrella-shaped structure, and the small-sized parachute (8) is popped up by the rest-set flip-flop (16).
5. a kind of remote sensing unmanned plane with permanent protective property energy according to claim 1, it is characterised in that: the rack
(5) inner bottom offers round slot, and the diameter of the round slot is equal with the diameter of the spring stack (2), institute
State spring stack (2) quantity be it is multiple, multiple spring stacks (2) are respectively symmetrically distributed in the four of the lower section of the rack (5)
A corner is provided with fixing seat above multiple spring stacks (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820494822.3U CN208325614U (en) | 2018-04-09 | 2018-04-09 | A kind of remote sensing unmanned plane with permanent protective property energy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820494822.3U CN208325614U (en) | 2018-04-09 | 2018-04-09 | A kind of remote sensing unmanned plane with permanent protective property energy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208325614U true CN208325614U (en) | 2019-01-04 |
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ID=64780894
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820494822.3U Expired - Fee Related CN208325614U (en) | 2018-04-09 | 2018-04-09 | A kind of remote sensing unmanned plane with permanent protective property energy |
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| Country | Link |
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| CN (1) | CN208325614U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112278279A (en) * | 2020-12-30 | 2021-01-29 | 江西云本数字科技有限公司 | Remote sensing monitored control system based on unmanned aerial vehicle |
| CN112455704A (en) * | 2020-12-07 | 2021-03-09 | 国网河北省电力有限公司雄安新区供电公司 | Single screw unmanned aerial vehicle prevent weighing down device |
| CN112591085A (en) * | 2020-11-30 | 2021-04-02 | 中国十七冶集团有限公司 | Unmanned aerial vehicle and inclination measurement system |
| CN112678192A (en) * | 2021-01-08 | 2021-04-20 | 刘江 | Convertible unmanned aerial vehicle of flight gesture |
| WO2022095335A1 (en) * | 2020-11-05 | 2022-05-12 | 北星空间信息技术研究院(南京)有限公司 | Multi-rotor unmanned aerial vehicle-based priority algorithm for jettisonable accessories |
-
2018
- 2018-04-09 CN CN201820494822.3U patent/CN208325614U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022095335A1 (en) * | 2020-11-05 | 2022-05-12 | 北星空间信息技术研究院(南京)有限公司 | Multi-rotor unmanned aerial vehicle-based priority algorithm for jettisonable accessories |
| CN112591085A (en) * | 2020-11-30 | 2021-04-02 | 中国十七冶集团有限公司 | Unmanned aerial vehicle and inclination measurement system |
| CN112591085B (en) * | 2020-11-30 | 2022-08-12 | 中国十七冶集团有限公司 | Unmanned aerial vehicle and inclination measurement system |
| CN112455704A (en) * | 2020-12-07 | 2021-03-09 | 国网河北省电力有限公司雄安新区供电公司 | Single screw unmanned aerial vehicle prevent weighing down device |
| CN112278279A (en) * | 2020-12-30 | 2021-01-29 | 江西云本数字科技有限公司 | Remote sensing monitored control system based on unmanned aerial vehicle |
| CN112278279B (en) * | 2020-12-30 | 2021-03-26 | 荷塘智能科技(固安)有限公司 | Remote sensing monitored control system based on unmanned aerial vehicle |
| CN112678192A (en) * | 2021-01-08 | 2021-04-20 | 刘江 | Convertible unmanned aerial vehicle of flight gesture |
| CN112678192B (en) * | 2021-01-08 | 2023-08-25 | 福建海狮集团有限公司 | Unmanned aerial vehicle with convertible flight posture |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190104 Termination date: 20200409 |