CN209209034U - A kind of large capacity carrying unmanned plane - Google Patents
A kind of large capacity carrying unmanned plane Download PDFInfo
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- CN209209034U CN209209034U CN201920155054.3U CN201920155054U CN209209034U CN 209209034 U CN209209034 U CN 209209034U CN 201920155054 U CN201920155054 U CN 201920155054U CN 209209034 U CN209209034 U CN 209209034U
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- bow
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- support rod
- vertical support
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Abstract
The utility model discloses a kind of large capacities to carry unmanned plane, including fuselage, aerofoil system, undercarriage and object storage component；Fuselage includes upper and lower upper frame plate and lower bearing bracket plate disposed in parallel；Aerofoil system is mounted between upper frame plate and lower bearing bracket plate, including wing after two preceding wings, two middle wings and two；Undercarriage includes two groups of bow-shaped support components, four vertical support rods and two chassis that rise and fall；Bow-shaped support component includes two bow-shaped supports disposed in parallel and two attachment bases；Vertical support rod is vertically arranged, and upper end is fixed between the end of two bow-shaped supports in bow-shaped support component；The chassis that rises and falls is fixed on the bottom end of vertical support rod, and two chassis that rise and fall are left and right parallel and horizontally disposed；Object storage component includes storing support frame and storage tank；Storing support frame is horizontally disposed；Storage tank is fixed on storing support frame.The utility model have many advantages, such as can large capacity load-bearing and stability it is good.
Description
Technical field
The utility model belongs to unmanned plane field, is related to a kind of unmanned plane more particularly to a kind of large capacity carrying unmanned plane.
Background technique
UAV referred to as " 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.Currently, unmanned plane is mainly used in the people
With with military aspect, including take photo by plane, agricultural, express transportation, disaster relief, monitoring, mapping, inspection, the disaster relief etc..
But unmanned plane is small in size to also limit its development, it is small in size to mean that unmanned plane storing capacity is small, and volume is big
If be easy to cause quality larger, structure may simultaneously it is unstable, be easy to cause crash.Therefore, a kind of volume appearance is needed at present
The unmanned plane that amount is big, stability is good.
Utility model content
The utility model provides a kind of large capacity carrying unmanned plane, to overcome the deficiencies of existing technologies.
To achieve the above object, the utility model provides a kind of large capacity carrying unmanned plane, including fuselage, aerofoil system,
Undercarriage and object storage component；Fuselage includes upper and lower upper frame plate and lower bearing bracket plate disposed in parallel；Aerofoil system is mounted on machine
Between frame plate and lower bearing bracket plate, including wing after two preceding wings, two middle wings and two；Wing before each, middle wing and
Wing includes support rod, driving motor and propeller afterwards, and one end of support rod is fixed between upper frame plate and lower bearing bracket plate,
Driving motor is mounted on the support rod other end, and propeller is mounted on driving motor, and driving motor drives propeller rotational；It rises and falls
Frame includes two groups of bow-shaped support components, four vertical support rods and two chassis that rise and fall；Bow-shaped support component includes two parallel
The bow-shaped support of setting and two attachment bases；Bow-shaped support, which has, is located at the horizontal segment of middle section and inclining positioned at left and right ends
Oblique section；Tilting section is obliquely installed relative to horizontal segment, and one end continuously connects with the end of horizontal segment, and the other end is towards outer side-lower
Extend；Two tilting sections are symmetrical arranged in the left and right sides of horizontal segment；Attachment base be fixed on two bow-shaped supports horizontal segment it
Between；Attachment base is fixedly connected with the lower surface of the lower bearing bracket plate of fuselage；Two groups of bow-shaped support components are forward and backward to be arranged in parallel in lower machine
The lower surface of frame plate；Vertical support rod is vertically arranged, and upper end is fixed on the end of two bow-shaped supports in bow-shaped support component
Between；Four vertical support rods are distributed in rectangle vertex, and the upper end of the vertical support rod of two of front side is separately fixed at front side
The left and right ends of bow-shaped support component, the upper end of the vertical support rod of two of rear side are separately fixed at the bow-shaped support component of rear side
Left and right ends；The chassis that rises and falls is fixed on the bottom end of vertical support rod, and two chassis that rise and fall are left and right parallel and horizontally disposed, left
The bottom end of the rise and fall chassis and two vertical support rods of front left side and left rear side of side is fixed, rise and fall chassis and the forward right side on right side
It is fixed with the bottom end of two vertical support rods of right lateral side；Object storage component includes storing support frame and storage tank；Storing support frame
Horizontally disposed, the vertical support rod in left side and two left sides is fixed, and the vertical support rod on right side and two right sides is fixed；Storage tank
It is fixed on storing support frame.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
Wing is arranged from the middle front part position of fuselage to surrounding in increased radioactivity after two preceding wings, two middle wings and two；Before
The bow-shaped support component of side is between preceding wing and the installation site of middle wing, close to the installation site of middle wing；Rear side
Bow-shaped support component is located at the rear side of the installation site of rear wing.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
The upper frame plate of fuselage has bending plate portion, the mounting plate portion positioned at middle section and the tail plate positioned at rear side positioned at front side
Portion；The rear end part in tail plate portion is in fish tail shape, and the edge of rear end is arc-shaped, protrudes towards rear, and the edge of the left and right sides is in
Arc, towards inner recess；The maximum width of bending plate portion and mounting plate portion is respectively less than the maximum of the rear end part in tail plate portion
Width；In undercarriage, two the distance between chassis that rise and fall are greater than the maximum width in bending plate portion and mounting plate portion, are less than tail
The maximum width of the rear end part in plate portion.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
In undercarriage, the front end for the chassis that rises and falls is no more than the front end of fuselage, and the rear end for the chassis that rises and falls is no more than the rear end of fuselage.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
Storing support frame includes two support frame fixed links and two support frame support rods；It is set in parallel before and after two support frame fixed links
It sets, lower part of the both ends of the support frame fixed link of front side respectively with the vertical support rod of two front sides in undercarriage is fixed, after
Lower part of the both ends of the support frame fixed link of side respectively with the vertical support rod of two rear sides in undercarriage is fixed；Support frame branch
The both ends of strut are fixed between two support frame fixed links, and two support frame support rods are left and right to be arranged in parallel.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
The cross section of vertical support rod is in rectangle；The longitudinal section of support frame fixed link is rounded；The end of support frame fixed link passes through perpendicular
Support bars, and be secured to by screw.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
Storage tank includes cabinet and case lid；Cabinet is in cuboid, opening up；Between the vertical support rod of the width of cabinet and the left and right sides
Spacing mutually agree with；The length of cabinet is less than the length for the chassis that rises and falls.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
The longitudinal section of case lid is arched, matches with the shape of bow-shaped support.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
Rise and fall chassis longitudinal section it is rounded；The chassis that rises and falls passes through the bottom end of vertical support rod, and is secured to by screw.
Further, the utility model provides a kind of large capacity carrying unmanned plane, can also have the following features: wherein,
The rise and fall front end of chassis upwarps.
The utility model has the beneficial effects that: the utility model provides a kind of large capacity carrying unmanned plane, fuselage is by upper
Frame plate and lower bearing bracket board group are at structure is simple, can not only reduce the own wt of fuselage, but also can reduce fuselage to greatest extent
Volume, provide antecedent basis for the object storage component of large capacity.Meanwhile undercarriage is structurally reasonable, guarantees big load-bearing and nobody
While machine stability, installation object storage component can also be accommodated.The utility model have can large capacity load-bearing and stability it is good etc.
Advantage.
Detailed description of the invention
Fig. 1 is the perspective view of large capacity carrying unmanned plane；
Fig. 2 is the top view of large capacity carrying unmanned plane；
Fig. 3 is the exploded view of lower bearing bracket plate, undercarriage and object storage component.
Specific embodiment
Illustrate specific embodiment of the present utility model below in conjunction with attached drawing.
As shown in Figure 1-3, the utility model provides a kind of large capacity carrying unmanned plane, including fuselage 1, aerofoil system 2,
Undercarriage 3 and object storage component 4.
Fuselage 1 includes upper and lower upper frame plate 11 and lower bearing bracket plate 12 disposed in parallel.
The upper frame plate 11 of fuselage 1 has the bending plate portion 111 positioned at front side, the mounting plate portion 112 positioned at middle section
With the tail plate portion 113 for being located at rear side.The rear end part in tail plate portion 113 is in fish tail shape, and the edge of rear end is arc-shaped, after
Side's protrusion, the edge of the left and right sides is arc-shaped, towards inner recess.
The maximum that the maximum width of bending plate portion 111 and mounting plate portion 112 is respectively less than the rear end part in tail plate portion 113 is wide
Degree.
Aerofoil system 2 is mounted between upper frame plate 11 and lower bearing bracket plate 12, including two preceding wings, 21, two middle wings
22 and two after wing 23.
Wing 23 is from the middle front part position of fuselage 1 to surrounding in putting after the middle wing 22 of two 21, two, preceding wings and two
The distribution setting of penetrating property.
The composed structure of preceding wing 21, middle wing 22 and rear wing 23 is all the same, includes support rod, driving motor and spiral shell
Revolve paddle.For the composed structure of wing 21 as explanation, preceding wing 21 included support rod 211, driving motor 212 and propeller in the past
213.One end of support rod 211 is fixed between upper frame plate 11 and lower bearing bracket plate 12, and driving motor 212 is mounted in support rod 211
The other end, propeller 213 are mounted on driving motor 212, and driving motor 212 drives propeller 213 to rotate.
Fuselage 1 is only made of upper frame plate 11 and lower bearing bracket plate 12, and the two is connected and fixed by the support boom end of wing,
Structure is simple, can not only reduce the own wt of fuselage, but also can reduce the volume of fuselage to greatest extent, is large capacity
Object storage component provides antecedent basis.
Undercarriage 3 includes two groups of bow-shaped support component 31, four vertical support rods 32 and two chassis 33 that rise and fall.
Bow-shaped support component 31 includes two bow-shaped supports 311 and two attachment bases 312 disposed in parallel.
Bow-shaped support 311 has the tilting section 3112 positioned at the horizontal segment 3111 of middle section and positioned at left and right both ends.Incline
Oblique section 3112 is obliquely installed relative to horizontal segment 3111, and one end continuously connects with the end of horizontal segment 3111, and the other end is outside
Side-lower extends.Two tilting sections 3112 are symmetrical arranged in the arranged on left and right sides of horizontal segment 3111.The arch knot of bow-shaped support 311
Structure can enhance its load-bearing capacity, while the flight for reducing unmanned plane hinders.
Attachment base 312 is in cuboid, is fixed between the horizontal segment 3111 of two bow-shaped supports 311.
Attachment base 312 is fixedly connected with the lower surface of the lower bearing bracket plate 12 of fuselage 1, to make bow-shaped support component 31 and machine
Body 1 is fixed.
Two bow-shaped supports 311 disposed in parallel both can be with the load bearing effect of effective guarantee bow-shaped support component 31, simultaneously
Also the own wt for avoiding excessive increase unmanned plane, guarantees flight effect.In addition, two bow-shaped supports 311 pass through the two
Between attachment base 312 and fuselage 1 it is fixed, this fixed form is fixedly connected guaranteeing that bow-shaped support component 31 is stablized with fuselage 1
On the basis of, do not weaken the load-bearing capacity of bow-shaped support 311.
The forward and backward lower surface for being arranged in parallel in lower bearing bracket plate 12 of two groups of bow-shaped support components 31.
The bow-shaped support component 31 of front side is between preceding wing 21 and the installation site of middle wing 22, close to middle wing 22
Installation site.The bow-shaped support component 31 of rear side is located at the rear side of the installation site of rear wing 23, to ensure unmanned plane during flying
Stability.
Vertical support rod 32 is vertically arranged, and upper end is fixed on the end of two bow-shaped supports 311 in bow-shaped support component 31
Between portion.
Four vertical support rods 32 are distributed in rectangle vertex, and the upper end of the vertical support rod 32 of two of front side is separately fixed at
The left and right ends of the bow-shaped support component 31 of front side, the upper end of the vertical support rod 32 of two of rear side are separately fixed at the bow of rear side
The left and right ends of shape bracket component 31.
The cross section of vertical support rod 32 is in rectangle.
The chassis 33 that rises and falls is fixed on the bottom end of vertical support rod 32.Two chassis 33 that rise and fall are left and right parallel and horizontally disposed.
Left side rise and fall chassis 33 and the bottom end of two vertical support rods 32 of front left side and left rear side is fixed, the chassis 33 that rises and falls on right side
It is fixed with the bottom end of two vertical support rods 32 of forward right side and right lateral side.
Specifically, the longitudinal section for the chassis 33 that rises and falls is rounded.The chassis 33 that rises and falls passes through the bottom end of vertical support rod 32, and leads to
Screw is crossed to be secured to.
Two the distance between chassis 33 that rise and fall are greater than the maximum width in bending plate portion 111 and mounting plate portion 112, are less than machine
The maximum width of the rear end part in tailgate portion 113.
The rise and fall front end of chassis 33 is no more than the front end of fuselage 1, and the rear end of the chassis 33 that rises and falls is no more than the rear end of fuselage 1.
Above-mentioned 33 positional relationship of chassis of rising and falling is conducive to reinforce the stability of unmanned plane during flying, reduces big weight storing institute
Caused unstable degree.
The rise and fall front end of chassis 33 upwarps, convenient for the landing of unmanned plane.
Object storage component 4 includes storing support frame 41 and storage tank 42.
Storing support frame 41 is horizontally disposed, and the vertical support rod 32 in left side and two left sides is fixed, right side and two right sides
Vertical support rod 32 it is fixed.
Storing support frame 41 includes two support frame fixed links 411 and two support frame support rods 412.
Two support frame fixed links 411 are forward and backward to be arranged in parallel.The both ends of the support frame fixed link 411 of front side respectively with rise
The lower part of the vertical support rod 32 of fall in frame 3 two front sides is fixed, the both ends of the support frame fixed link 411 of rear side respectively with rise
The lower part of the vertical support rod 32 of two rear sides fallen in frame 3 is fixed.
Specifically, the longitudinal section of support frame fixed link 411 is rounded.The end of support frame fixed link 411 passes through vertical branch
Strut 32, and be secured to by screw.
The both ends of support frame support rod 412 are fixed between two support frame fixed links 411, two support frame support rods
412 left and right are arranged in parallel.
Storage tank 42 is fixed on storing support frame 41.
Storage tank 42 includes cabinet 421 and case lid 422.
Cabinet 421 is in cuboid, opening up.Between between the vertical support rod 32 of the width of cabinet 421 and the left and right sides
Away from mutually agreeing with, i.e. the width of cabinet 421 is slightly less than the spacing between the vertical support rod 32 in the left and right sides, keeps cabinet 421 rigid
It is placed in well between the vertical support rod 32 in the left and right sides, efficiently uses the space in undercarriage 3.The length of cabinet 421, which is less than, rises and falls
The length of chassis 33, to ensure the stability in unmanned plane during flying.
The longitudinal section of case lid 422 is arched, matches with the shape of bow-shaped support 311, has been mounted on convenient for storage tank 42
It falls in frame 3.
Claims (10)
1. a kind of large capacity carries unmanned plane, it is characterised in that:
Including fuselage, aerofoil system, undercarriage and object storage component；
The fuselage includes upper and lower upper frame plate and lower bearing bracket plate disposed in parallel；
The aerofoil system is mounted between the upper frame plate and the lower bearing bracket plate, including two preceding wings, two middle machines
Wing after the wing and two；
Each preceding wing, middle wing and rear wing include support rod, driving motor and propeller, and the one of the support rod
End is fixed between the upper frame plate and the lower bearing bracket plate, and the driving motor is mounted on the support rod other end, the spiral shell
Rotation paddle is mounted on driving motor, and driving motor drives the propeller rotational；
The undercarriage includes two groups of bow-shaped support components, four vertical support rods and two chassis that rise and fall；
The bow-shaped support component includes two bow-shaped supports disposed in parallel and two attachment bases；
The bow-shaped support has the tilting section positioned at the horizontal segment of middle section and positioned at left and right ends；
The tilting section is obliquely installed relative to the horizontal segment, and one end continuously connects with the end of the horizontal segment, the other end
Extend towards outer side-lower；
Two tilting sections are symmetrical arranged in the left and right sides of the horizontal segment；
The attachment base is fixed between the horizontal segment of two bow-shaped supports；
The attachment base is fixedly connected with the lower surface of the lower bearing bracket plate of the fuselage；
The forward and backward lower surface for being arranged in parallel in the lower bearing bracket plate of bow-shaped support component described in two groups；
The vertical support rod is vertically arranged, upper end be fixed on two bow-shaped supports in the bow-shaped support component end it
Between；
Four vertical support rods are distributed in rectangle vertex, and the upper end of the vertical support rod of two of front side is separately fixed at front side
The bow-shaped support component left and right ends, the upper end of the vertical support rod of two of rear side be separately fixed at rear side the bow
The left and right ends of shape bracket component；
The chassis that rises and falls is fixed on the bottom end of the vertical support rod, and two chassis that rise and fall are left and right parallel and horizontally disposed, left
The bottom end of the rise and fall chassis and two vertical support rods of front left side and left rear side of side is fixed, rise and fall chassis and the forward right side on right side
It is fixed with the bottom end of two vertical support rods of right lateral side；
The object storage component includes storing support frame and storage tank；
The storing support frame is horizontally disposed, and the vertical support rod in left side and two left sides is fixed, right side and two right sides
Vertical support rod fix；
The storage tank is fixed on the storing support frame.
2. large capacity according to claim 1 carries unmanned plane, it is characterised in that:
Wherein, two preceding wings, two middle wings and two it is described after wings by the fuselage middle front part position
It is arranged to surrounding in increased radioactivity；
The bow-shaped support component of front side is between the preceding wing and the installation site of middle wing, close to the peace of middle wing
Holding position；
The bow-shaped support component of rear side is located at the rear side of the installation site of the rear wing.
3. large capacity according to claim 1 carries unmanned plane, it is characterised in that:
Wherein, the upper frame plate of the fuselage has positioned at bending plate portion, the mounting plate portion positioned at middle section and the position of front side
In the tail plate portion of rear side；
The rear end part in tail plate portion is in fish tail shape, and the edge of rear end is arc-shaped, protrudes towards rear, the side of the left and right sides
Edge is arc-shaped, towards inner recess；
The maximum that the maximum width of the bending plate portion and the mounting plate portion is respectively less than the rear end part in tail plate portion is wide
Degree；
In the undercarriage, the distance between the chassis that rises and falls described in two is greater than the bending plate portion and the mounting plate portion most
Big width, less than the maximum width of the rear end part in tail plate portion.
4. large capacity according to claim 1 carries unmanned plane, it is characterised in that:
Wherein, in the undercarriage, the front end of the chassis that rises and falls is no more than the front end of the fuselage, and the rear end for the chassis that rises and falls is not
More than the rear end of fuselage.
5. large capacity according to claim 1 carries unmanned plane, it is characterised in that:
Wherein, the storing support frame includes two support frame fixed links and two support frame support rods；
Be arranged in parallel before and after two support frame as described above fixed links, the both ends of the support frame fixed link of front side respectively with the undercarriage
In the lower parts of the vertical support rod of two front sides fix, the both ends of the support frame fixed link of rear side are respectively and in undercarriage
The lower parts of vertical support rod of two rear sides fix；
The both ends of support frame as described above support rod are fixed between two support frame as described above fixed links, two support frame support rods left sides,
The right side is arranged in parallel.
6. large capacity according to claim 5 carries unmanned plane, it is characterised in that:
Wherein, the cross section of the vertical support rod is in rectangle；
The longitudinal section of support frame as described above fixed link is rounded；
The end of support frame as described above fixed link passes through the vertical support rod, and is secured to by screw.
7. large capacity according to claim 1 carries unmanned plane, it is characterised in that:
Wherein, the storage tank includes cabinet and case lid；
The cabinet is in cuboid, opening up；
Spacing between the width of the cabinet and the left and right sides vertical support rod is mutually agreed with；
The length of the cabinet is less than the length of the chassis that rises and falls.
8. large capacity according to claim 7 carries unmanned plane, it is characterised in that:
Wherein, the longitudinal section of the case lid is arched, matches with the shape of the bow-shaped support.
9. large capacity according to claim 1 carries unmanned plane, it is characterised in that:
Wherein, the longitudinal section of the chassis that rises and falls is rounded；
The chassis that rises and falls passes through the bottom end of the vertical support rod, and is secured to by screw.
10. large capacity according to claim 9 carries unmanned plane, it is characterised in that:
Wherein, the front end of the chassis that rises and falls upwarps.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920155054.3U CN209209034U (en) | 2019-01-29 | 2019-01-29 | A kind of large capacity carrying unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920155054.3U CN209209034U (en) | 2019-01-29 | 2019-01-29 | A kind of large capacity carrying unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209209034U true CN209209034U (en) | 2019-08-06 |
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ID=67467747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920155054.3U Expired - Fee Related CN209209034U (en) | 2019-01-29 | 2019-01-29 | A kind of large capacity carrying unmanned plane |
Country Status (1)
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| CN (1) | CN209209034U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111196365A (en) * | 2020-01-20 | 2020-05-26 | 北京京邦达贸易有限公司 | Unmanned aerial vehicle's support and unmanned aerial vehicle |
-
2019
- 2019-01-29 CN CN201920155054.3U patent/CN209209034U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111196365A (en) * | 2020-01-20 | 2020-05-26 | 北京京邦达贸易有限公司 | Unmanned aerial vehicle's support and unmanned aerial vehicle |
| CN111196365B (en) * | 2020-01-20 | 2021-09-17 | 北京京邦达贸易有限公司 | Unmanned aerial vehicle's support and unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Lanzhou Lanzhi Wujiang Intelligent Technology Co., Ltd Assignor: Zhang Qiang Contract record no.: X2020980006780 Denomination of utility model: A large capacity carrier UAV Granted publication date: 20190806 License type: Common License Record date: 20201015 |
|
| 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: 20190806 Termination date: 20210129 |