CN205837181U - A kind of portable aircraft with pooling feature - Google Patents
A kind of portable aircraft with pooling feature Download PDFInfo
- Publication number
- CN205837181U CN205837181U CN201620794819.4U CN201620794819U CN205837181U CN 205837181 U CN205837181 U CN 205837181U CN 201620794819 U CN201620794819 U CN 201620794819U CN 205837181 U CN205837181 U CN 205837181U
- Authority
- CN
- China
- Prior art keywords
- casing
- aircraft
- carbon fiber
- battery
- inner chamber
- 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.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of portable aircraft with pooling feature, including casing, one end of casing is fixedly connected with battery, and the top of casing and battery is installed with cover, the both sides of described casing are all installed with carbon fiber pipe, carbon fiber pipe is fixedly connected with stirring paddle support away from one end of casing, the top of stirring paddle support is fixedly connected with stirring fan blades, the other end of stirring paddle support is installed with buffer unit, the bottom of described chassis cavity is installed with support means, and the inner chamber of casing is provided with photographic head away from one end of battery.This utility model setting by buffer unit; buffer spring and cushion pad can be declined aircraft simultaneously bottom out suffered pressure and buffer; reach to protect the effect of aircraft; carbon fiber is all used to arrange by the carbon fiber pipe in aircraft, upper bracket plate with lower carriage plate; the weight allowing aircraft can be reduced, and reaches to alleviate the effect of aircraft overall weight.
Description
Technical field
This utility model relates to flight technical field of mold, a kind of portable aircraft with pooling feature.
Background technology
Aircraft, also known as quadrotor or four-rotor helicopter, is called for short four axles or four rotors, and four-axle aircraft is one
Planting multi-rotor aerocraft, four propellers of four-axle aircraft are all the simple mechanisms of motor direct-connected, and criss-cross layout allows
Aircraft obtains the power of main body turning by changing motor speed, thus adjusts self attitude, and concrete ins and outs are " basic
Motion principle " in tell about because its intrinsic complexity, the most never have a large-scale commercial four-axle aircraft, in recent years
Benefiting the development of micro electronmechanical control technology, stable four-axle aircraft has obtained paying close attention to widely, and application prospect is the most considerable.
Existing small aircraft carries photographic head, it is possible to achieve low latitude camera function, is used for moving video recording and high level is built
Building the Application comparison such as thing roof supervision extensive, but owing to the capacity of battery is a bottleneck, continuous to fly the time the longest, thus causes work
Shooting efficiency reduction, and aircraft decline during owing to lacking certain buffer unit, cause aircraft to compare
It is easily subject to damage, so that the cost of aircraft use and maintenance is greatly increased.
Utility model content
The purpose of this utility model is to provide a kind of portable aircraft with pooling feature, possesses power and energy saving and flies
Row time length and the advantage of protection aircraft, solve the flight time long problem with rapid wear aircraft.
For achieving the above object, this utility model provides following technical scheme: a kind of have the portable of pooling feature and fly
Row device, including casing, one end of casing is fixedly connected with battery, and the top of casing and battery is installed with cover, institute
The both sides stating casing are all installed with carbon fiber pipe, and carbon fiber pipe is fixedly connected with stirring paddle support away from one end of casing,
The top of stirring paddle support is fixedly connected with stirring fan blades, and the other end of stirring paddle support is installed with buffer unit, described
The bottom of chassis cavity is installed with support means, and the inner chamber of casing is provided with photographic head away from one end of battery.
Preferably, described buffer unit includes that gripper shoe, the bottom of described gripper shoe are installed with connecting plate, connecting plate
Bottom connect have the elevator running through and extending to connecting plate inner chamber, the bottom of described gripper shoe to be installed with and be positioned at connection
The fixing seat of plate inner chamber, elevator is positioned at one end of connecting plate inner chamber and offers dashpot, and the bottom of dashpot is installed with
Cushion pad, and the bottom of fixing seat is installed with the fixing post being connected with cushion pad top, and fixing post is socketed with one end
The buffer spring being connected is fixed with fixing seat bottom portion.
Preferably, described support means includes upper bracket plate and lower carriage plate, the side of described upper bracket plate and lower carriage
The side of plate offers the first screw hole and the second screw hole respectively.
Preferably, the quantity of described carbon fiber pipe is four, and each carbon fiber pipe has been fixedly connected with stirring paddle and has propped up
Frame.
Preferably, the cross-sectional diameter of described cover is total with the cross-sectional diameter of battery equal to the cross-sectional diameter of casing
With.
Compared with prior art, the beneficial effects of the utility model are as follows:
1, this utility model setting by buffer unit, buffer spring can be declined aircraft with cushion pad simultaneously and touches
Pressure at the end and buffer, reach to protect the effect of aircraft.
2, this utility model all uses carbon fiber to set by the carbon fiber pipe in aircraft, upper bracket plate with lower carriage plate
Put, the weight of aircraft can be reduced, reaches to alleviate the effect of aircraft overall weight.
Accompanying drawing explanation
Fig. 1 is that this utility model faces structural representation；
Fig. 2 is that cross-sectional view faced by this utility model buffer unit；
Fig. 3 is this utility model A-A partial structurtes schematic diagram；
Fig. 4 is this utility model plan structure schematic diagram；
Fig. 5 is this utility model top view cross section structural representation；
Fig. 6 is this utility model upper bracket plate structure schematic diagram；
Fig. 7 is this utility model lower carriage plate structure schematic diagram.
In figure: 1 casing, 2 batteries, 3 covers, 4 carbon fiber pipes, 5 stirring paddle supports, 6 stirring fan blades, 7 buffer units, 71
Fagging, 72 connecting plates, 73 elevators, 74 fix seat, 75 fix post, 76 buffer springs, 77 dashpots, 78 cushion pads, 8 shooting
Head, 9 support meanss, 91 upper bracket plates, 92 first screw holes, 93 lower carriage plates, 94 second screw holes.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under making creative work premise
The every other embodiment obtained, broadly falls into the scope of this utility model protection.
Referring to Fig. 1-3, a kind of portable aircraft with pooling feature, including casing 1, one end of casing 1 is fixed
Connecting and have battery 2, battery 2 can provide power for whole aircraft, and the top of casing 1 and battery 2 is installed with cover
3, the cross-sectional diameter of cover 3 is equal to the cross-sectional diameter of casing 1 and the cross-sectional diameter summation of battery 2, and the both sides of casing 1 are equal
Being installed with carbon fiber pipe 4, the quantity of carbon fiber pipe 4 is four, and each carbon fiber pipe 4 has been fixedly connected with stirring paddle
Support 5, carbon fiber pipe 4 is fixedly connected with stirring paddle support 5 away from one end of casing 1, and the top of stirring paddle support 5 is fixing to be connected
Having stirring fan blades 6, the other end of stirring paddle support 5 is installed with buffer unit 7, and buffer unit 7 includes gripper shoe 71, supports
The bottom of plate 71 is installed with connecting plate 72, and the bottom of connecting plate 72 connects the liter running through and extending to connecting plate 72 inner chamber
Fall block 73, the bottom of gripper shoe 71 is installed with the fixing seat 74 being positioned at connecting plate 72 inner chamber, and elevator 73 is positioned at connecting plate
One end of 72 inner chambers offers dashpot 77, and the bottom of dashpot 77 is installed with cushion pad 78, and the end of fixing seat 74
Portion is installed with the fixing post 75 being connected with cushion pad 78 top, fixing post 75 is socketed with bottom one end and fixing seat 74 solid
The fixed buffer spring 76 connected, by the setting of buffer unit 7, allows buffer spring 76 and the cushion pad 78 can be simultaneously under aircraft
Fall bottoms out suffered pressure and buffers, and reaches to protect the effect of aircraft.
Referring to Fig. 4-7, the bottom of casing 1 inner chamber is installed with support means 9, and support means 9 includes upper bracket plate
91 offer the first screw hole 92 and second with lower carriage plate 93, the side of upper bracket plate 91 respectively with the side of lower carriage plate 93
Screw hole 94, the first screw hole 92 and the second screw hole 94 be used to fixing mainboard assembly and fixing camera assembly etc., and
The inner chamber of casing 1 is provided with photographic head 8 away from one end of battery 2, and upper bracket plate 91 and lower carriage plate 93 are carbon fiber structural.
In sum, this has the portable aircraft of pooling feature, by the setting of buffer unit 7, allows buffer spring
76 can bottom out suffered pressure to aircraft decline with cushion pad 78 simultaneously and buffer, and reach to protect the effect of aircraft
Really, all use carbon fiber to arrange by the carbon fiber pipe 4 in aircraft, upper bracket plate 91 with lower carriage plate 93, allow aircraft
Weight can be reduced, and reaches to alleviate the effect of aircraft overall weight.
Embodiment the most of the present utility model, for the ordinary skill in the art,
It is appreciated that in the case of without departing from principle of the present utility model and spirit and these embodiments can be carried out multiple change, repair
Changing, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. there is a portable aircraft for pooling feature, including casing (1), it is characterised in that: one end of casing (1) is fixed
Connecting and have battery (2), and the top of casing (1) and battery (2) is installed with cover (3), the both sides of described casing (1) are equal
Being installed with carbon fiber pipe (4), carbon fiber pipe (4) is fixedly connected with stirring paddle support (5) away from one end of casing (1), stirs
The top mixing oar support (5) is fixedly connected with stirring fan blades (6), and the other end of stirring paddle support (5) is installed with buffering dress
Putting (7), the bottom of described casing (1) inner chamber is installed with support means (9), and the inner chamber of casing (1) is away from battery (2)
One end be provided with photographic head (8).
A kind of portable aircraft with pooling feature the most according to claim 1, it is characterised in that: described buffering dress
Put (7) and include that gripper shoe (71), the bottom of described gripper shoe (71) are installed with connecting plate (72), the bottom of connecting plate (72)
Connecting and have the elevator (73) running through and extending to connecting plate (72) inner chamber, the bottom of described gripper shoe (71) is installed with position
In the fixing seat (74) of connecting plate (72) inner chamber, elevator (73) is positioned at one end of connecting plate (72) inner chamber and offers dashpot
(77), the bottom of dashpot (77) is installed with cushion pad (78), and the bottom of fixing seat (74) is installed with slow
The fixing post (75) that die head (78) top is connected, fixing post (75) is socketed with one end and fixes with fixing seat (74) bottom and to be connected
Buffer spring (76).
A kind of portable aircraft with pooling feature the most according to claim 1, it is characterised in that: described support fills
Put (9) and include upper bracket plate (91) and lower carriage plate (93), the side of described upper bracket plate (91) and the side of lower carriage plate (93)
Face offers the first screw hole (92) and the second screw hole (94) respectively.
A kind of portable aircraft with pooling feature the most according to claim 1, it is characterised in that: described carbon fiber
The quantity of pipe (4) is four, and each carbon fiber pipe (4) has been fixedly connected with stirring paddle support (5).
A kind of portable aircraft with pooling feature the most according to claim 1, it is characterised in that: described cover
(3) cross-sectional diameter is equal to the cross-sectional diameter of casing (1) and the cross-sectional diameter summation of battery (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620794819.4U CN205837181U (en) | 2016-07-26 | 2016-07-26 | A kind of portable aircraft with pooling feature |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620794819.4U CN205837181U (en) | 2016-07-26 | 2016-07-26 | A kind of portable aircraft with pooling feature |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205837181U true CN205837181U (en) | 2016-12-28 |
Family
ID=57640107
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620794819.4U Expired - Fee Related CN205837181U (en) | 2016-07-26 | 2016-07-26 | A kind of portable aircraft with pooling feature |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205837181U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045570A (en) * | 2018-02-24 | 2018-05-18 | 冯林娟 | A kind of unmanned plane undercarriage of more rotors |
-
2016
- 2016-07-26 CN CN201620794819.4U patent/CN205837181U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045570A (en) * | 2018-02-24 | 2018-05-18 | 冯林娟 | A kind of unmanned plane undercarriage of more rotors |
| CN108045570B (en) * | 2018-02-24 | 2019-04-16 | 冯林娟 | A kind of unmanned plane undercarriage of more rotors |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203727646U (en) | Unmanned helicopter | |
| US11305881B2 (en) | Arm for unmanned aerial vehicle | |
| CN110418755A (en) | A kind of unmanned vehicle | |
| CN205837181U (en) | A kind of portable aircraft with pooling feature | |
| CN107505116A (en) | The aircraft support meanss and transonic wind tunnel experimental provision of air formation flight experiment | |
| CN105059541A (en) | Novel multi-axis unmanned aerial vehicle | |
| CN101520364B (en) | Inverted cup-type drop test bed cradle | |
| CN106428524B (en) | A kind of multi-rotor aerocraft with the free wing | |
| CN206939034U (en) | Multi-rotor unmanned aerial vehicle boxlike load fuselage | |
| CN205256671U (en) | Screw power balance mechanism for unmanned aerial vehicle | |
| CN205469808U (en) | Photovoltaic power plant detection device | |
| CN218703898U (en) | Sand land patrol unmanned aerial vehicle for preventing and controlling sand | |
| CN215284246U (en) | Wall climbing inspection robot and system | |
| CN208775012U (en) | A kind of VTOL flying platform high efficiency lift unit | |
| CN106542093A (en) | Efficient multi-rotor aerocraft | |
| CN206307280U (en) | A kind of unmanned plane aerial device | |
| CN205931255U (en) | Spherical unmanned aerial vehicle based on ARM | |
| CN104843191A (en) | Non-contact type intelligent rainproof device for unmanned aerial vehicle | |
| CN206485573U (en) | A kind of auxiliary external member of operation fixed-wing unmanned plane VTOL | |
| CN212616097U (en) | A earthquake-resistant structure for architectural design | |
| CN208619958U (en) | A kind of computer server mounting rack | |
| CN201086824Y (en) | Dish shaped aircraft | |
| CN207725615U (en) | The self-balancing wing of unmanned plane | |
| CN2896255Y (en) | Down-fitted vertical wind-tunnel of power system | |
| CN209535437U (en) | A kind of aircraft frame and its aircraft |
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: 20161228 Termination date: 20210726 |