CN205931212U - Many rotor manned vehicle of partly gravity is overcome with helium balloon - Google Patents
Many rotor manned vehicle of partly gravity is overcome with helium balloon Download PDFInfo
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- CN205931212U CN205931212U CN201620531704.6U CN201620531704U CN205931212U CN 205931212 U CN205931212 U CN 205931212U CN 201620531704 U CN201620531704 U CN 201620531704U CN 205931212 U CN205931212 U CN 205931212U
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- helium balloon
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- aircraft
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Abstract
The utility model belongs to the utensil field of travelling specifically is many rotor manned vehicle of partly gravity is overcome with helium balloon. It includes: helium balloon, many rotor crafts, manned storehouse, connecting device, buffering software, the helium balloon setting is put at many rotor crafts central point, and manned storehouse is under the helium balloon, and the buffering software is pasted in the top position on helium balloon upper portion, and connecting device links together helium balloon, many rotor crafts, manned storehouse according to above -mentioned position. Partly gravity has been overcome for many rotor crafts to the helium balloon, makes the utility model discloses behind the manned year thing, the speed of its motor need not too highly, has solved the flexible nature problem of helium balloon effectively, has also solved the problem of the manned load of many rotor crafts effectively.
Description
Technical field
This utility model belongs to play apparatus field, is specially flown with many rotor manneds that helium balloon overcomes a part of gravity
Row device.
Background technology
Helium balloon can manned go up to the air, but motility, control performance are bad, the skyborne motility of multi-rotor aerocraft,
Controlling is good, but loading capacity is too little, if increasing loading capacity, its production cost and technical difficulty rapidly increase.
Such as：A diameter of 5 meters of helium balloon, has the lifting force of newton more than 600, and balloon monolayer by the gravitation of the earth is
50 newton, the double-deck gravitation being subject to the earth is 250 newton, and the lifting force of a diameter of 50 meters of helium balloon deducts the helium of itself
The terrestrial gravitation of ball material, 600 newton deduct 50 newton, or deduct 200 it is simply that newton more than 500, or newton more than 400,
That is a diameter of 5 meters of helium balloon can lift about more than 50 kilogram, or more than 40 kilogram of weight, and this weight compares one
Personal weight is slightly light, is equivalent to the weight of a people.Although a people can be risen in the air by helium balloon, people
The lifting of uncontrollable helium balloon and flight, especially manned fly up after it is impossible to drop to ground, current technology adopts rope
The mode pulling down, loses a lot of enjoyment.
Multi-rotor aerocraft, adjacent motor positive and negative rotation, when rotating to certain speed, can go up to the air, revolve more
During rotor aircraft balance flight, gyroscopic effect and air force moment of torsion effect are all cancelled.By gesture stability, many rotor flyings
Device rotates along 3 coordinate axess respectively and moves, and does omnibearing flight in the air.In order to keep the stabilized flight of aircraft,
Multi-rotor aerocraft forms inertial navigation module equipped with gyroscope and axle acceleration sensor, can calculate aircraft this
When relatively the attitude in face and acceleration, angular velocity.Flight controller is calculated required when keeping kinestate by algorithm
Revolving force and lift, ensure that by electronic adjusting controller motor exports suitable power.
The frame for movement of multi-rotor aerocraft is much simple than helicopter, and maintenance and the expense changed are also very little, and this allows
Multi-rotor aerocraft has the application advantage bigger than helicopter, especially in recent years some weight with respect to metal material and energy
The appearance of the new material of alternative metals material, and the advancing by leaps and bounds of battery technology, make multi-rotor aerocraft start to set foot in and take photo by plane
Field, logistics field, film manufacture field, crops sprinkling pesticide field, engineer operation, military industry field, with battery technology
Breakthrough further, we predict that multi-rotor aerocraft will be widely used in more fields.
But multi-rotor aerocraft has a maximum defect：Load-carrying is very little.Many rotor flyings on the market now
Device, does not have one, the hundreds of unit of multi-rotor aerocraft dozens of yuan of loading capacity, the thousand of unit of the multi-rotor aerocraft that more than 1 kilogram of load-carrying
One, one, the tens of thousands of unit of the multi-rotor aerocraft that more than 5 kilograms of load-carrying, the multi-rotor aerocraft hundreds of thousands that more than 20 kilograms of load-carrying
One, unit, namely 35 kilograms of seen loading capacity maximum in the market, why can be so？Because working as load-carrying
When amount is bigger, the rotating speed of motor is required very high, the correspondingly requirement to other another parts also increases difficulty, so skill
Art difficulty and production cost all can increase sharply with the increase of loading capacity.
Existing technology, wants to allow the manned flexible flight of helium balloon, is impossible, wants to make multi-rotor aerocraft manned
Flight, the big high cost of difficulty, and also cost and safety issue cannot effectively solvings.
Utility model content
This utility model is directed to problem above, provides a kind of helium balloon to overcome many rotor manned flights of a part of gravity
Device, helium balloon is arranged on multi-rotor aerocraft center, and multi-rotor aerocraft makes helium balloon flexible, and helium balloon is many
Rotor craft overcomes a part of gravity, and after making this utility model manned, the speed of its motor need not be too high, efficiently solves
The maneuverability sex chromosome mosaicism of helium balloon, also efficiently solves the problem of the manned loads of multi-rotor aerocraft.
In order to realize object above, this utility model employs the following technical solutions.
Overcome many rotor manneds aircraft of a part of gravity with helium balloon, it includes, helium balloon 1, multi-rotor aerocraft
2, manned storehouse 3, attachment means 4, buffer software 5；Described helium balloon 1 is arranged on multi-rotor aerocraft 2 center, manned storehouse 3
Underface in helium balloon 1；Described buffering software 5 is pasted onto the apical position on helium balloon 1 top, and described attachment means 4 are pressed upper
Rheme is put and helium balloon 1, multi-rotor aerocraft 2, manned storehouse 3 is linked together.
The middle part of each adapter in described attachment means 4 is fixedly connected with the frame of multi-rotor aerocraft 2, on
End is connected 4 with other adapters, and lower end is connected with manned storehouse 3.
Described helium balloon 1 is divided into two-layer, and one layer is internal layer, and to seal based on helium, air inlet is a flexible pipe to its function,
Inflation rear hose mouth fluid sealant is shut, and when inflating again, cuts off the seal head of flexible pipe, reinflated after will be inflated with fluid sealant again
Mouthful shut, another layer is outer layer, its function is to increase intensity, overcome tension force, overcome based on friction.
It is provided with seat and operation handle in described manned storehouse 3, described seat is provided with seat belt, seat belt can be by
The chest of people, abdominal part are fixed on seat back, and the two legs of people can also be fixed on seat foreleg for seat belt, described seat
The foreleg of chair is battery, and back leg is reserve battery, and battery is connected with many rotor manneds aircraft, operation handle by electric wire.Institute
State operation handle and multi-rotor aerocraft 2 wired connection, or wireless remotely-controlled.
Adapter in described attachment means 4 is lightweight hardware connecting rod, or software rope.
One piece of macrofoam buffering software as the bottom size shape of manned storehouse 3 is installed in described manned storehouse 3 bottom.
The beneficial effects of the utility model
1st, this utility model adopts multi-rotor aerocraft technology, flexible, can be freely lifted in the air, fly.
2nd, this utility model because helium balloon overcomes most of weight, to the rotating speed of motor, electricity of battery etc. require fall
Low, thus greatly reducing production cost and technical difficulty, and more than 50 kilograms of goods and personnel can be carried, becoming manned
Aircraft.
3rd, this utility model, because employing buffering software, makes contact portion between helium balloon and aircraft gentle, makes helium
Ball is hardly damaged.
4th, this utility model is because bulky, but very light in weight, in the event of mechanically or electrically road fault, will not directly drop
Get off, but descend slowly and lightly, thus very safe.
5th, this utility model power consumption is little, and loading capacity is big, can carry battery more, and long-time pocket stays, flies in the air.
6th, weight of the present utility model concentrates on bottommost, so this utility model is in the air or on ground, can be maximum
Limit keeps not tilting, and drops to macrofoam buffering software and the nearly parallel contact in ground of during contact ground it is ensured that bottom, does not have
There are vibrations, elasticity is less, so that passenger comfort level is greatly increased, so that the old,weak,sick and disabled personnel also can take.
7th, this utility model has adopted wired handle operation and wireless remotely-controlled operation two ways, so disturbs big field in electromagnetism
Conjunction can also normally use.
Brief description
Fig. 1 is this utility model schematic diagram；
Fig. 2 is this utility model example one frame schematic diagram；
Fig. 3 is bar and the mounting rod connection diagram of this utility model example one frame；
Fig. 4 is the schematic top plan view of this utility model example two frame；
Fig. 5 is the schematic front view of this utility model example two frame；
Fig. 6 is this utility model example three frame schematic diagram.
Its in figure, 1 helium balloon, 2 multi-rotor aerocrafts, 21 bars, 22 rod aperture, 23 mounting rods, 24 motors
Extension rod, 25 connecting rods, 211 bolts hole, 3 manned storehouses, 4 attachment means, 5 buffering softwares.
Specific embodiment
Overcome many rotor manneds aircraft of a part of gravity with helium balloon, it includes, helium balloon 1, multi-rotor aerocraft
2, manned storehouse 3, attachment means 4, buffer software 5；Described helium balloon 1 is arranged on multi-rotor aerocraft 2 center, manned storehouse 3
Underface in helium balloon 1；Described buffering software 5 is pasted onto the apical position on helium balloon 1 top, and described attachment means 4 are pressed upper
Rheme is put and helium balloon 1, multi-rotor aerocraft 2, manned storehouse 3 is linked together.
The middle part of each adapter in described attachment means 4 is fixedly connected with the frame of multi-rotor aerocraft 2, on
End is connected 4 with other adapters, and lower end is connected with manned storehouse 3
Described helium balloon 1 is divided into two-layer, and one layer is internal layer, and to seal based on helium, air inlet is a flexible pipe to its function,
Inflation rear hose mouth fluid sealant is shut, and when inflating again, cuts off the seal head of flexible pipe, reinflated after will be inflated with fluid sealant again
Mouthful shut, another layer is outer layer, its function is to increase intensity, overcome tension force, overcome based on friction.
It is provided with seat and operation handle in described manned storehouse 3, described seat is provided with seat belt, seat belt can be by
The chest of people, abdominal part are fixed on seat back, and the two legs of people can also be fixed on seat foreleg for seat belt, described seat
The foreleg of chair is battery, and back leg is reserve battery, and battery is connected with many rotor manneds aircraft, operation handle by electric wire.Institute
State operation handle and multi-rotor aerocraft 2 wired connection, or wireless remotely-controlled.
Adapter in described attachment means 4 is lightweight hardware connecting rod, or software rope.
One piece of macrofoam buffering software as the bottom size shape of manned storehouse 3 is installed in described manned storehouse 3 bottom.
With reference to embodiment and accompanying drawing, this utility model is described in further details：
Example one embodiment as shown in Figure 1：Overcome many rotor manneds aircraft of a part of gravity with helium balloon, its bag
Include, helium balloon 1, multi-rotor aerocraft 2, manned storehouse 3, attachment means 4, buffer software 5；Described helium balloon 1 is arranged on many rotors
Aircraft 2 center, manned storehouse 3 is in the underface of helium balloon 1；Described buffering software 5 is pasted onto helium balloon 1, described connection
Helium balloon 1, multi-rotor aerocraft 2, manned storehouse 3 are linked together by device 4 by above-mentioned position.
A diameter of 5.5 meters of the helium balloon 1 of embodiment one, is divided into two-layer, and outer layer is preferably TPU composite, and internal layer is preferred
For TPU material, the Chinese of TPU is Polyurethane Thermoplastic Elastomer, and TPU material has very strong high-tension, high-tensile strength, strong
Toughness and ageing-resistant characteristic, are both and also have high water proofing property poisture-penetrability, Radix Saposhnikoviae, cold-proof, antibacterial, mould proof, warming, uvioresistant
And many excellent functions such as energy release.The internal layer of helium balloon 1, its function to seal based on helium, outer layer, its function with
Increase intensity, overcome tension force, overcome based on friction.Helium balloon 1 inflation inlet is a silica gel tube, and helium is filled with helium by silica gel tube
After balloon 1, sealing compound seals its mouth, prevents gas from leaking, if necessary to fill helium again, silica gel tube head is sliced off, is filled with helium again
Gas, seals its mouth with sealing compound again, prevents gas from leaking.
The buffering software 5 of embodiment one is pasted onto helium balloon 1 top.Its material is preferably the EPP material of macrofoam（Poly- third
Alkene Foamex）, it is a kind of high professional qualification environmental protection foamed materialss, has high intensity, high resilience, impact resistance, corrosion-resistant, is difficult
The excellent properties such as breakage.
The gravity of helium balloon 1 removing described in the present embodiment itself, has the lifting force of newton more than 500, the present embodiment institute
The manned storehouse 3 stated, the weight of 2, human body three of multi-rotor aerocraft have the lifting force of downward newton more than 600, lifting force
And terrestrial gravitation, on the contrary, both impetus concentrate on helium balloon 1 top to the power of both, then this position is to be easiest to
The place of abrasion, so here pastes one a diameter of 3 meters of buffering software 5, to ensure the intact of helium balloon 1.
The multi-rotor aerocraft 2 of embodiment one is 8 axle rotor crafts, and frame is made up of carbon fibre material, such as Fig. 1, figure
2nd, shown in Fig. 3, frame is octagon, and its frame includes：Bar 21, mounting rod 23, are provided with bar in the center position of bar 21
Hole 22.Adjacent two bars 21 and mounting rod 23 are bolted by bolt hole 211, and eight bar 21 fixations are become positive eight by bolt
Side shape, each mounting rod 23 is bolted a motor by bolt hole 211, and adjacent motor direction of rotation is contrary.Described
Bolt is the bolt manufactured with carbon fibre material, the plane of the silking composition of carbon fiber bolt and carbon fiber nut, twists with nut
The tight angle forming 20 degree and 50 degree with the direction exited, produced vibrations during such this utility model motion are just difficult to make spiral shell
Cap loosens.
It is provided with seat, operation handle, remote controller in described manned storehouse 3, described seat is provided with seat belt, seat belt
The chest of people, abdominal part can be fixed on seat back, the two legs of people can also be fixed on seat foreleg for seat belt.
Antidetonation lithium battery is installed in seat foreleg.The EPP material of one layer of macrofoam is installed in the bottom in manned storehouse 3.
Adapter in described attachment means 4 is nylon rope, and nylon rope passes through the machine frame hole 22 of multi-rotor aerocraft 2, and
Bundle firm with bar 21, upper end and other 7 nylon ropes are fixed together, and it is firm that lower end and manned storehouse 3 bundle.
As shown in Figure 4, Figure 5, the multi-rotor aerocraft of embodiment two is 6 axle rotor crafts, and frame is by carbon fibre material
Make, frame is circle, its frame includes：Bar 21, mounting rod 23, motor extension rod 24, mounting rod 23 and mounting rod 23 it
Between the centre position of bar 21 be provided with rod aperture 22.Together with bar 21 and mounting rod 23 are bolted by bolt hole, each peace
A motor installed by dress bar 23, and motor is fixedly connected with mounting rod 23 with by motor extension rod 24, the work of motor extension rod 24
With being to prevent the propeller on motor from contacting with helium balloon, adjacent motor direction of rotation is contrary.
The helium balloon of embodiment two, is arranged on 6 axle rotor craft centers, its a diameter of 6 meters, is divided into two-layer, outward
Layer is preferably carbon cloth, and internal layer is preferably TPU material.
Adapter in the attachment means of embodiment two is cordage, and cordage passes through the machine frame hole of multi-rotor aerocraft,
And bundling firm with bar, upper end is fixed together with other 5 nylon ropes, and lower end and the binding of manned storehouse are firm.
As shown in fig. 6, the multi-rotor aerocraft of embodiment three is 4 axle rotor crafts, frame is by titanium alloy tube material system
Become, frame includes：Bar 21, mounting rod 23, connecting rod 25, bar 21 and mounting rod 23 are coupled together by connecting rod 25, play reinforcing
Effect, bar 21 is four, and every bar 21 is the arcuate structure of quadrant, is connected in top, every bar 21 another
One end is fixedly connected with one end of mounting rod 23, and mounting rod 23 is two right-angle sides of right angled triangle, and the other end installs motor
And propeller, because propeller extends vertically upwards, so propeller will not contact helium balloon.
The top half of helium balloon in frame, lived by nylon rope by the latter half.
In order to further illustrate this utility model, use process of the present utility model and method are described as follows：
Taking embodiment one as a example it is described.
Indoors, or in outdoor wind scale, under the weather conditions below three-level, embodiment one is fixed on ground by nylon rope
On the spud pile of face, at this moment embodiment one has the lifting force of newton more than 400, the people of 60 kilogram weights, has about 600 newton
Terrestrial gravitation, after this people sits into manned storehouse, the earth adds the lifting force of embodiment one helium to the gravitation of embodiment one,
That is to say, that embodiment one adds that the gross weight of human body is about public to 20 at 10 kilograms about between 100 newton to 200 newton
Between jin.
This people sits into after manned storehouse, fastens breast, abdomen, lower limb seat belt, unties the nylon rope for fixing on the ground, beat
Open the battery power switch on seat foreleg, with the hands operate operation handle, this utility model can go up to the air, flies, land.
By surface personnel by the present embodiment bolt fortunately ground spud pile after landing, this people opens manned storehouse, walks
Go out manned storehouse.
Claims (7)
1. overcome many rotor manneds aircraft of a part of gravity it is characterised in that it includes with helium balloon, helium balloon, revolves more
Rotor aircraft, manned storehouse, attachment means, buffer software；Described helium balloon is arranged on multi-rotor aerocraft center, manned storehouse
Underface in helium balloon；The described buffering apical position on helium balloon top for the soft body pasting, described attachment means press upper rheme
Put and helium balloon, multi-rotor aerocraft, manned storehouse link together, the middle part of each adapter in described attachment means
It is fixedly connected with the frame of multi-rotor aerocraft, upper end is connected with other adapters, and lower end is connected with manned storehouse.
2. helium balloon according to claim 1 overcome a part of gravity many rotor manneds aircraft it is characterised in that
Described helium balloon (1) is divided into two-layer, and one layer is internal layer, and to seal based on helium, air inlet is a flexible pipe to its function, after inflation
Hose port fluid sealant is shut, and when inflating again, cuts off the seal head of flexible pipe, reinflated after with fluid sealant, flexible pipe is shut again,
Another layer is outer layer, and its function is to increase intensity, overcome tension force, overcome based on friction.
3. helium balloon according to claim 1 overcome a part of gravity many rotor manneds aircraft it is characterised in that
Be provided with seat, operation handle in described manned storehouse, described seat be provided with seat belt, seat belt can by the chest of people,
Abdominal part is fixed on seat back, and the two legs of people can also be fixed on seat foreleg for seat belt, the foreleg of described seat
For battery, back leg is reserve battery, and battery is connected with many rotor manneds aircraft, operation handle by electric wire, described manipulator
Handle and multi-rotor aerocraft are wired connection, or wireless remotely-controlled.
4. helium balloon according to claim 1 overcome a part of gravity many rotor manneds aircraft it is characterised in that
The bolt being adopted in frame is carbon fiber bolt nut, the plane of the silking composition of carbon fiber bolt and carbon fiber nut, with
Nut is tightened and the direction exited forms one 20 degree to 50 degree of angle.
5. helium balloon according to claim 1 overcome a part of gravity many rotor manneds aircraft it is characterised in that
Adapter in described attachment means is lightweight hardware connecting rod, or software rope.
6. helium balloon according to claim 1 overcome a part of gravity many rotor manneds aircraft it is characterised in that
The material of buffering software is macrofoam material, is shaped as circular arc body, is sized for being pasted onto helium balloon top.
7. helium balloon according to claim 1 overcome a part of gravity many rotor manneds aircraft it is characterised in that
One layer of soft material is installed in the bottom in manned storehouse.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620531704.6U CN205931212U (en) | 2016-06-04 | 2016-06-04 | Many rotor manned vehicle of partly gravity is overcome with helium balloon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620531704.6U CN205931212U (en) | 2016-06-04 | 2016-06-04 | Many rotor manned vehicle of partly gravity is overcome with helium balloon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205931212U true CN205931212U (en) | 2017-02-08 |
Family
ID=57931815
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620531704.6U Expired - Fee Related CN205931212U (en) | 2016-06-04 | 2016-06-04 | Many rotor manned vehicle of partly gravity is overcome with helium balloon |
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| CN (1) | CN205931212U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947168A (en) * | 2016-06-04 | 2016-09-21 | 郑州中德美游乐设备有限公司 | Multi-rotor manned craft adopting helium balloon to overcome part of gravity |
| CN111516852A (en) * | 2020-05-01 | 2020-08-11 | 梅向瑾 | Manned hot air balloon for safe weather measurement and control and environment monitoring and method |
| CN112498674A (en) * | 2020-12-11 | 2021-03-16 | 太阳月亮（北京）新能源科技有限公司 | Inflatable full-electric rotary wing civil helicopter |
-
2016
- 2016-06-04 CN CN201620531704.6U patent/CN205931212U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947168A (en) * | 2016-06-04 | 2016-09-21 | 郑州中德美游乐设备有限公司 | Multi-rotor manned craft adopting helium balloon to overcome part of gravity |
| CN111516852A (en) * | 2020-05-01 | 2020-08-11 | 梅向瑾 | Manned hot air balloon for safe weather measurement and control and environment monitoring and method |
| CN112498674A (en) * | 2020-12-11 | 2021-03-16 | 太阳月亮（北京）新能源科技有限公司 | Inflatable full-electric rotary wing civil helicopter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20170208 Termination date: 20170604 |