CN108146624A - A kind of unmanned plane with forced landing umbrella - Google Patents
A kind of unmanned plane with forced landing umbrella Download PDFInfo
- Publication number
- CN108146624A CN108146624A CN201810137953.0A CN201810137953A CN108146624A CN 108146624 A CN108146624 A CN 108146624A CN 201810137953 A CN201810137953 A CN 201810137953A CN 108146624 A CN108146624 A CN 108146624A
- Authority
- CN
- China
- Prior art keywords
- support column
- unmanned plane
- rear surface
- head
- fixedly connected
- 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
- 230000001681 protective effect Effects 0.000 claims abstract description 13
- 238000003466 welding Methods 0.000 claims description 6
- 238000005215 recombination Methods 0.000 abstract description 2
- 230000006798 recombination Effects 0.000 abstract description 2
- 230000001771 impaired effect Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 206010033799 Paralysis Diseases 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000036561 sun exposure Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
- B64C25/64—Spring shock-absorbers; Springs using rubber or like elements
-
- 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
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
-
- 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
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Walking Sticks, Umbrellas, And Fans (AREA)
Abstract
The invention discloses a kind of unmanned planes with forced landing umbrella, including head, the front surface of the head is provided with stomata, and the bottom end of head is fixedly connected with protective cover, the inside of the protective cover is equipped with camera, and the rear surface of protective cover is provided with fuselage, the both sides of the fuselage have been fixedly connected with telescopic mast, and fuselage is internally provided with safety cage, link block is installed on the outside of the telescopic mast, the bottom end of the link block is equipped with support column upper end.The present invention, by setting spring, support column and changing recombination, efficiently solve the problems, such as that unmanned plane promptly lands and causes support column impaired under emergency case, by setting telescopic mast, it efficiently solve the problems, such ass that in unmanned plane placement its occupied space size can not be reduced when not in use, by setting safety cage, efficiently solve the problems, such as that unmanned plane can not effectively ensure that unmanned plane is safe after the failure of high-altitude.
Description
Technical field
The present invention relates to unmanned air vehicle technique field more particularly to a kind of unmanned planes with forced landing umbrella.
Background technology
Unmanned plane, as the term suggests it is unpiloted aircraft；From the birth of aircraft early 20th century, due to consideration that driving
The idea of UAV just has been proposed in the safety of aircraft, people at that time.
But unmanned plane currently on the market is complicated, and function is single, is not provided with damping device, leads to practical behaviour
When making, encountering emergency case needs to land, and easily leads to support column and is damaged, is not provided with telescopic rod, causes when not in use, it is impossible to
Effectively reduce unmanned plane the space occupied, be not provided with friction pad, can be effectively prevented unmanned plane because with ground friction not
Enough device is caused to be damaged, be not provided with safety cage, can not ensure that unmanned plane is pacified after efficiently solving unmanned plane high-altitude failure
The problem of complete.
Invention content
The purpose of the present invention is to solve problem in the prior art, and a kind of nobody with forced landing umbrella proposed
Machine.
To achieve these goals, present invention employs following technical solutions：A kind of unmanned plane with forced landing umbrella,
Including head, the front surface of the head is provided with stomata, and the bottom end of head is fixedly connected with protective cover, the protective cover
Inside is equipped with camera, and the rear surface of protective cover is provided with fuselage, and the both sides of the fuselage have been fixedly connected with telescopic mast,
And fuselage is internally provided with safety cage, and link block, the bottom end peace of the link block are installed on the outside of the telescopic mast
Top equipped with support column upper end, and link block is equipped with motor, and the bottom end of the support column upper end is equipped with bumper post, described
The bottom end of bumper post is equipped with support column lower end, and the bottom end of the support column lower end is equipped with friction pad, the top of the motor
Wing is installed, the rear surface of the head is equipped with solar panel, and the rear surface of the solar panel is equipped with,
The inside of the support column upper end is equipped with No.1 spring, and the inside of the support column lower end is equipped with No. two springs, the peace
The rear surface of full room is equipped with safety door, and the inside of safety cage is equipped with hyperbaric chamber, and the inside in the hyperbaric chamber is equipped with two
Number electric telescopic rod is equipped with retainer ring, and the rear surface in hyperbaric chamber is equipped with No.1 electric expansion on the inside of the hyperbaric chamber
Bar, the rear surface of the retainer ring are connected with parachute.
Preferably, the motor is fixedly connected with wing by shaft, and there are four the quantity of wing.
Preferably, the battery inside is equipped with reserve battery, the solar panel and battery inside it is standby
It is electrically connected with battery, reserve battery and No.1 electric telescopic rod, No. two electric telescopic rods of the battery inside electrically connect
It connects.
Preferably, the support column upper end is equal with the outer diameter of support column lower end, and support column upper end and support column lower end
Internal diameter it is equal with the outer diameter of bumper post.
Preferably, the upper end of the bumper post is fixedly connected by welding with No.1 spring, and the lower end of bumper post and two
Number spring is fixedly connected by welding.
Compared with prior art, the present invention provides a kind of unmanned planes with forced landing umbrella, have following beneficial to effect
Fruit：
1st, it, by setting spring, support column and changing recombination, should be efficiently solved with the unmanned plane of forced landing umbrella
The problem of unmanned plane promptly lands and support column is caused to be damaged under emergency case.
2nd, there should be the unmanned plane of forced landing umbrella, and by setting telescopic mast, efficiently solve and placed not in unmanned plane
The problem of its occupied space size can not be reduced during use.
3rd, there should be the unmanned plane of forced landing umbrella, and by setting safety cage, efficiently solve unmanned plane in high-altitude event
It can not effectively ensure the problem of unmanned plane is safe after barrier.
It is same as the prior art or the prior art can be used realized that part is not directed in the device, structure of the present invention
It is scientific and reasonable, it is simple to operate.
Description of the drawings
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is side view of the present invention；
Fig. 3 is the structure diagram of safety cage of the present invention.
In figure：1st, head；2nd, protective cover；3rd, camera；4th, fuselage；5th, friction pad；6th, support column lower end；7th, bumper post；
8th, support column upper end；9th, link block；10th, wing；11st, motor；12nd, telescopic mast；13rd, stomata；14th, solar panel；15th, one
Number spring；16th, No. two springs；17th, safety cage；18th, No.1 electric telescopic rod；19th, No. two electric telescopic rods；20th, retainer ring；
21st, hyperbaric chamber；22nd, safety door；23rd, parachute；24th, battery case.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.
In the description of the present invention, it is to be understood that term " on ", " under ", "front", "rear", "left", "right", " top ",
The orientation or position relationship of the instructions such as " bottom ", " interior ", " outer " are based on orientation shown in the drawings or position relationship, merely to just
In the description present invention and simplify description rather than instruction or imply signified device or element must have specific orientation, with
Specific azimuth configuration and operation, therefore be not considered as limiting the invention.
With reference to Fig. 1-3, a kind of unmanned plane with forced landing umbrella, including head 1, the front surface of head 1 is provided with gas
Hole 13, and the bottom end of head 1 is fixedly connected with protective cover 2, the inside of protective cover 2 is equipped with camera 3, and after protective cover 2
Surface is provided with fuselage 4, the both sides of fuselage 4 have been fixedly connected with telescopic mast 12, and fuselage 4 is internally provided with safety cage 17,
The outside of telescopic mast 12 is installed with link block 9, and the bottom end of link block 9 is equipped with support column upper end 8, and the top of link block 9
End is equipped with motor 11, and the bottom end of support column upper end 8 is equipped with bumper post 7, and the bottom end of bumper post 7 is equipped with support column lower end 6,
The bottom end of support column lower end 6 is equipped with friction pad 5, and the top of motor 11 is equipped with wing 10, and the rear surface of head 1 is equipped with too
Positive energy solar panel 14, the rear surface of solar panel 14 are equipped with 24, and the inside of support column upper end 8 is equipped with No.1 spring
15, the inside of support column lower end 6 is equipped with No. two springs 16, and the rear surface of safety cage 17 is equipped with safety door 22, and safety cage
17 inside is equipped with hyperbaric chamber 21, and the inside in hyperbaric chamber 21 is equipped with No. two electric telescopic rods 19, the inside peace in hyperbaric chamber 21
Rear surface equipped with retainer ring 20, and hyperbaric chamber 21 is equipped with No.1 electric telescopic rod 18, and the rear surface of retainer ring 20 is connected with
Parachute 23.
It is rotated for the ease of wing with unmanned plane is driven to go up to the air, in the present embodiment, it is preferred that motor 11 passes through with wing 10
Shaft is fixedly connected, and there are four the quantity of wing 10.
For the ease of reserve battery storage electric energy with being energized to telescopic rod, in the present embodiment, it is preferred that inside battery case 24
Reserve battery is installed, solar panel 14 is electrically connected with the reserve battery inside battery case 24, inside battery case 24
18, No. two electric telescopic rods 19 of reserve battery and No.1 electric telescopic rod are electrically connected.
For the ease of the fixation of bumper post 7, in the present embodiment, it is preferred that the outer diameter of dagger upper end 8 and support column lower end 6
It is equal, and support column upper end 8 is equal with the outer diameter of bumper post 7 with the internal diameter of support column lower end 6.
It is fixed for the ease of 15, No. two paralysis 16 of bumper post and No.1 spring, in the present embodiment, it is preferred that bumper post 7
Upper end is fixedly connected by welding with No.1 spring 15, and the lower end of bumper post 7 is fixedly connected by welding with No. two springs 16.
The operation principle and process for using of the present invention：First, when unmanned plane lands, friction pad 5 is contacted with ground to be produced
Raw enough frictional force makes unmanned plane stablize as early as possible, and generated impact force is sent by the production of friction pad 5 to No. two springs 16 and one
On number spring 15, impact force can be completely dispersed and thereby protect unmanned plane safety；Then, in unmanned plane in use, in solar energy
After solar panel 14 and sun exposure, solar panel 14 can convert solar energy into electrical energy, then electric energy is stored in battery case
In reserve battery in 24；Finally, it is controlled in 2 battery cases 4 by controller in use, after the failure of high-altitude in unmanned plane
Reserve battery gives No.1 electric telescopic rod 18, No. two 19 functions of electric telescopic rod, and the elongation of No.1 electric telescopic rod 18 is made to open peace
Air cock 22 shrinks No. two electric telescopic rods 19, sprays the high pressure gas in hyperbaric chamber 21, and parachute 23 is driven to spray, and drops
It falls umbrella 23 by rope with retainer ring 20 to be connected, you can its peace can not be ensured in high-altitude catastrophic failure by efficiently solving unmanned plane
The problem of complete.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (5)
1. a kind of unmanned plane with forced landing umbrella, including head (1), which is characterized in that the front surface of the head (1) is set
Stomata (13) is equipped with, and the bottom end of head (1) is fixedly connected with protective cover (2), the inside of the protective cover (2) is equipped with camera shooting
Head (3), and the rear surface of protective cover (2) is provided with fuselage (4), the both sides of the fuselage (4) have been fixedly connected with telescopic mast
(12), and fuselage (4) is internally provided with safety cage (17), and link block (9) is installed on the outside of the telescopic mast (12),
The bottom end of the link block (9) is equipped with support column upper end (8), and the top of link block (9) is equipped with motor (11), the branch
The bottom end of dagger upper end (8) is equipped with bumper post (7), and the bottom end of the bumper post (7) is equipped with support column lower end (6), described
The bottom end of support column lower end (6) is equipped with friction pad (5), and the top of the motor (11) is equipped with wing (10), the head
(1) rear surface is equipped with solar panel (14), and the rear surface of the solar panel (14) is equipped with battery case
(24), the inside of the support column upper end (8) is equipped with No.1 spring (15), and the inside of the support column lower end (6) is equipped with
No. two springs (16), the rear surface of the safety cage (17) are equipped with safety door (22), and the inside of safety cage (17) is equipped with
Hyperbaric chamber (21), the inside of the hyperbaric chamber (21) are equipped with No. two electric telescopic rods (19), the inside of the hyperbaric chamber (21)
Retainer ring (20) is installed, and the rear surface of hyperbaric chamber (21) is equipped with No.1 electric telescopic rod (18), the retainer ring (20)
Rear surface be connected with parachute (23).
2. a kind of unmanned plane with forced landing umbrella according to claim 1, which is characterized in that the motor (11) with
Wing (10) is fixedly connected by shaft, and there are four the quantity of wing (10).
A kind of 3. unmanned plane with forced landing umbrella according to claim 1, which is characterized in that the battery case (24)
Inside is equipped with reserve battery, and the solar panel (14) is electrically connected with the internal reserve battery of battery case (24), institute
The internal reserve battery of battery case (24) is stated to be electrically connected with No.1 electric telescopic rod (18), No. two electric telescopic rods (19).
A kind of 4. unmanned plane with forced landing umbrella according to claim 1, which is characterized in that the support column upper end
(8) it is equal with the outer diameter of support column lower end (6), and support column upper end (8) and the internal diameter of support column lower end (6) and bumper post (7)
Outer diameter it is equal.
A kind of 5. unmanned plane with forced landing umbrella according to claim 1, which is characterized in that the bumper post (7)
Upper end be fixedly connected by welding with No.1 spring (15), and the lower end of bumper post (7) and No. two springs (16) pass through welding
It is fixedly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810137953.0A CN108146624A (en) | 2018-02-10 | 2018-02-10 | A kind of unmanned plane with forced landing umbrella |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810137953.0A CN108146624A (en) | 2018-02-10 | 2018-02-10 | A kind of unmanned plane with forced landing umbrella |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108146624A true CN108146624A (en) | 2018-06-12 |
Family
ID=62457248
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810137953.0A Pending CN108146624A (en) | 2018-02-10 | 2018-02-10 | A kind of unmanned plane with forced landing umbrella |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108146624A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112591127A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Safety landing device for protecting camera during unmanned aerial vehicle fault |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986340A (en) * | 2015-06-15 | 2015-10-21 | 西华大学 | Multi-rotor craft emergency protection system and method |
| CN105947191A (en) * | 2016-05-19 | 2016-09-21 | 郑琳琳 | Novel multi-rotor unmanned aerial vehicle |
| CN107651199A (en) * | 2017-10-30 | 2018-02-02 | 四川道勤信业科技有限公司 | A kind of umbrella cabin device of unmanned plane |
-
2018
- 2018-02-10 CN CN201810137953.0A patent/CN108146624A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986340A (en) * | 2015-06-15 | 2015-10-21 | 西华大学 | Multi-rotor craft emergency protection system and method |
| CN105947191A (en) * | 2016-05-19 | 2016-09-21 | 郑琳琳 | Novel multi-rotor unmanned aerial vehicle |
| CN107651199A (en) * | 2017-10-30 | 2018-02-02 | 四川道勤信业科技有限公司 | A kind of umbrella cabin device of unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112591127A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Safety landing device for protecting camera during unmanned aerial vehicle fault |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180612 |