CN206797702U - A kind of soft gas-pocket thereof multi-rotor aerocraft - Google Patents
A kind of soft gas-pocket thereof multi-rotor aerocraft Download PDFInfo
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- CN206797702U CN206797702U CN201720112450.9U CN201720112450U CN206797702U CN 206797702 U CN206797702 U CN 206797702U CN 201720112450 U CN201720112450 U CN 201720112450U CN 206797702 U CN206797702 U CN 206797702U
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- dynamical system
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Abstract
The utility model discloses a kind of soft gas-pocket thereof multi-rotor aerocraft, including body and dynamical system, body is integral sealing airbag structure, equipment compartment is provided with body and dynamical system places cabin, dynamical system is placed in cabin and sets connecting cross beam, it is provided with the groove of connecting cross beam upper surface including propeller, the dynamical system that motor and base are formed, the outer stationary plates of motor base are arranged at the outer surface of the bottom surface of groove, internal fixation plate is arranged at the interior surface of groove floor, the utility model is rational in infrastructure, by by body global design into the structure of the air bag without hard skeleton, alleviate the own wt of unmanned plane, add the payload amount of aircraft, the structure of air bag class has good cushioning effect simultaneously, when not in use, release the gas in air bag, also can be easy to carry.
Description
Technical field
The utility model belongs to multi-rotor aerocraft technical field, and in particular to a kind of soft gas-pocket thereof multi-rotor aerocraft.
Background technology
Since development multi-rotor aerocraft, mostly it has been using aluminium, carbon fiber and other hard and has certain
Rigid material manufactures the skeleton of body and wing, the material that conventional aircraft uses, compared with high strength fibre, though
So rigidity is preferable, but general specific strength is relatively low, and anti-fatigue performance is poor, and under the same conditions, they are heavier, create
Aircraft also weigh, payload is smaller on the contrary.
Utility model content
The purpose of this utility model is to provide a kind of soft gas-pocket thereof multi-rotor aerocraft, to solve in above-mentioned background technology
The problem of proposition.
To realize above-mentioned target, the technical solution of the utility model is：A kind of soft gas-pocket thereof multi-rotor aerocraft, its feature
It is：Including being sequentially connected the petal body formed and dynamical system by four semicircles, the body is integral sealing
Airbag structure, on the body among be provided with the equipment compartment that lower surface is through to by its upper surface, surrounding array be evenly equipped with by
Four dynamical systems that its upper surface is through to lower surface place cabin, the dynamical system place be provided among cabin with body
Portion be connected and with body made of identical material connecting cross beam, the connecting cross beam upper surface set it is fluted, it is described recessed
Dynamical system is provided with groove, the dynamical system includes oar portion and stretches out the propeller in dynamical system placement cabin, passes through motor shaft
The motor being connected with propeller and the motor base for fixing motor, the motor base include what is be bolted
Outer stationary plates and internal fixation plate, the outer stationary plates are arranged at the outer surface of the bottom surface of groove, and internal fixation plate is arranged at groove
The interior surface of bottom surface.
It is further preferred that the body is made up of upper fabric, lower fabric and side material, the upper fabric and lower fabric point
Do not formed with side material sealing welding.
It is further preferred that the upper and lower surface of the body is covered with wear-resistant veneer.
It is further preferred that the block upper surface is provided with the metallic channel that slave unit cabin extends to groove.
It is further preferred that the body lower surface is provided with support.
The utility model is rational in infrastructure, by the way that body global design into the structure of the air bag without hard skeleton, is alleviated
The own wt of unmanned plane, the payload amount of aircraft is added, while the structure of air bag class has good cushioning effect,
When not in use, the gas in air bag is released, can be also easy to carry.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model,
Fig. 2 is the structural representation of dynamical system.
Drawing explanation：1st, body, 2, equipment compartment, 3, dynamical system place cabin, 4, connecting cross beam, 5, groove, 6, propeller,
7th, motor, 8, outer stationary plates, 9, internal fixation plate, 10, metallic channel.
Embodiment
With reference to accompanying drawing be described in detail the technical solution of the utility model, a kind of soft gas-pocket thereof multi-rotor aerocraft, including by
Four semicircles are sequentially connected the petal body 1 and dynamical system of composition, and the body is integral sealing airbag structure, institute
State among on body and be provided with the equipment compartment 2 that lower surface is through to by its upper surface, surrounding array is evenly equipped with to be passed through by its upper surface
Four dynamical systems worn to lower surface place cabin 3, and the dynamical system places to be provided among cabin to be connected with internal body
And connecting cross beam 4, the connecting cross beam upper surface made of identical material set fluted 5, set in the groove with body
Dynamical system is equipped with, the dynamical system includes oar portion and stretches out the propeller 6 in dynamical system placement cabin, passes through motor shaft and spiral
The motor 7 that oar is connected and the motor base for fixing motor, the motor base are outer solid including being bolted
Fixed board 8 and internal fixation plate 9, the outer stationary plates are arranged at the outer surface of the bottom surface of groove, and internal fixation plate is arranged at groove-bottom
The interior surface in face；The body by upper fabric, lower fabric and side material form, the upper fabric and lower fabric respectively with side
Material sealing welding forms；The upper and lower surface of the body is covered with wear-resistant veneer；The block upper surface is provided with
Slave unit cabin extends to the metallic channel 10 of groove；The body lower surface is provided with support.
The course of work of the present utility model is：Aerodynamically with the requirement of mechanics, will be flown through testing and improving
Device is designed to that as shown in Figure 1 body is the petal integral sealing airbag structure that four semicircles are sequentially connected composition,
Aircraft is divided into upper fabric and lower fabric in manufacturing process to form with side material sealing welding respectively, has optimized with simplicity and has made
Technique, the equipment compartment are used to place flight control, and block upper surface sets metallic channel, facilitates control system to dynamic
The arrangement of wire when Force system passes through polygon control survey, the interior connecting cross beam set of groove, for maintaining the global shape of air bag to prevent
The expansion that only limits air bag and deform.
General principle of the present utility model, principal character and advantage has been shown and described above, it is new not departing from this practicality
On the premise of type spirit and scope, the utility model also has various changes and modifications, and these changes and improvements both fall within requirement and protected
The scope of the utility model of shield.
Claims (5)
- A kind of 1. soft gas-pocket thereof multi-rotor aerocraft, it is characterised in that：Including being sequentially connected the petal formed by four semicircles The body and dynamical system of shape, the body are integral sealing airbag structure, on the body among be provided with by its upper surface The equipment compartment of lower surface is through to, surrounding array is evenly equipped with four dynamical systems placement that lower surface is through to by its upper surface Cabin, the dynamical system places to be provided among cabin is connected and is connected with body made of identical material horizontal stroke with internal body Beam, the connecting cross beam upper surface setting is fluted, dynamical system is provided with the groove, the dynamical system includes oar portion Stretch out propeller, the motor being connected by motor shaft with propeller and the electricity for fixing motor that dynamical system places cabin Machine base, the motor base include the outer stationary plates and internal fixation plate being bolted, and the outer stationary plates are arranged at recessed The outer surface of the bottom surface of groove, internal fixation plate are arranged at the interior surface of groove floor.
- A kind of 2. soft gas-pocket thereof multi-rotor aerocraft according to claim 1, it is characterised in that：The body is by above Material, lower fabric and side material composition, the upper fabric and lower fabric form with side material sealing welding respectively.
- A kind of 3. soft gas-pocket thereof multi-rotor aerocraft according to claim 1, it is characterised in that：The upper surface of the body With lower surface covered with wear-resistant veneer.
- A kind of 4. soft gas-pocket thereof multi-rotor aerocraft according to claim 1, it is characterised in that：The block upper surface is set It is equipped with the metallic channel that slave unit cabin extends to groove.
- A kind of 5. soft gas-pocket thereof multi-rotor aerocraft according to claim 1, it is characterised in that：The body lower surface is set It is equipped with support.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720112450.9U CN206797702U (en) | 2017-02-07 | 2017-02-07 | A kind of soft gas-pocket thereof multi-rotor aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720112450.9U CN206797702U (en) | 2017-02-07 | 2017-02-07 | A kind of soft gas-pocket thereof multi-rotor aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206797702U true CN206797702U (en) | 2017-12-26 |
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ID=60728582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720112450.9U Active CN206797702U (en) | 2017-02-07 | 2017-02-07 | A kind of soft gas-pocket thereof multi-rotor aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206797702U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111717382A (en) * | 2020-05-27 | 2020-09-29 | 西南科技大学 | Many rotor crafts of medium are striden to empty amphibious of water |
-
2017
- 2017-02-07 CN CN201720112450.9U patent/CN206797702U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111717382A (en) * | 2020-05-27 | 2020-09-29 | 西南科技大学 | Many rotor crafts of medium are striden to empty amphibious of water |
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