CN204979236U - Novel aircraft - Google Patents
Novel aircraft Download PDFInfo
- Publication number
- CN204979236U CN204979236U CN201520179545.3U CN201520179545U CN204979236U CN 204979236 U CN204979236 U CN 204979236U CN 201520179545 U CN201520179545 U CN 201520179545U CN 204979236 U CN204979236 U CN 204979236U
- Authority
- CN
- China
- Prior art keywords
- track
- motor
- course
- cabin
- slide block
- 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
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Classifications
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- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Body Structure For Vehicles (AREA)
Abstract
The utility model provides a novel aircraft belongs to air travel ware technical field, and it is huge heavy and complicated to aim at solving current aircraft overall structure, awkward problem. It is at the internal battery of having installed in cabin, the operation ware, the external portion in cabin be fixed with 4 equipartitions each other the symmetry through the track, every on the track insert have the slider along orbital motion, the slider facial make -up even has the lift, turn to power unit, the bottom that the floor stand dress was even personally experienced sth. Part of the body in the cabin, go up and down, it is by the connecting rod to turn to power unit, motor supporting frame, the motor screw is constituteed, connecting rod one end link block, motor supporting frame is being connected to the other end, and even act as go -between at the slider facial make -up and connecting motor supporting frame, be equipped with the motor screw at the motor supporting frame facial make -up. Its simple structure is practical, is applicable to the operation etc. Of prevening disaster of aircraft industry, meteorological industry, aerial reconnaissance, aerial photographic, agricultural.
Description
Technical field
The utility model belongs to a kind of aircraft in airborne aircraft technical field.
Background technology
Along with aircraft industry, meteorological industry, aerial prospecting, aerophotography, agricultural are taken precautions against natural calamities growing and scientific and technical the advancing by leaps and bounds such as operation, more and more higher to the technical requirements page of airborne aircraft.In known technology, existing aircraft is mainly made up of load motor helical oar, storage battery, mechanical arm etc. on spherical tanks body.But limitting by its structure, its integral structure is huge complicated, practical application controls dumb, and especially direction adjustment, landing are difficult to control, and also make troubles to use.
Utility model content
In order to overcome the deficiencies in the prior art, solve existing aircraft integral structure huge complicated, awkward problem.The object of the utility model is to provide a kind of simple and practical, and practical application controls flexibly, and direction adjustment, landing are easy to control, new aircraft easy to use.
The technical scheme in the invention for solving the above technical problem is:
A kind of course of new aircraft, it comprises: cabin body, motor helical oar, storage battery, mechanical arm, through track, slide block and floor stand, storage battery, mechanical arm is equiped with in the body of cabin, cabin external body be fixed with 4 uniform symmetrically through track, on track, the slide block of orbital motion is installed with at every root, slide block is fitted with lifting, steering power mechanism, floor stand is installed in the bottom of cabin body.
Above-mentioned a kind of course of new aircraft, described lifting, steering power mechanism are made up of pipe link, motor support frame, motor helical oar, pipe link one end connection sliding block, the other end are connected to motor support frame, and on slide block, be fitted with bracing wire be connected to motor support frame, motor support frame is equiped with motor helical oar.
Above-mentioned a kind of course of new aircraft, described lifting, steering power mechanism are band screw propeller external rotor electric machines slide block studding with 2 mutual retrograde rotations.
Above-mentioned a kind of course of new aircraft, described cabin body is the cabin body of the ball-table shape of band segment cap, drum type, spherical, ball-table shape.
Above-mentioned a kind of course of new aircraft, described through track be circular arc type track.
Above-mentioned a kind of course of new aircraft, described slide block is fixed with the mechanical arm in any one connection driving compartment of hydraulic compressor, bracing wire.
Above-mentioned a kind of course of new aircraft, the motor of described motor helical oar, screw propeller external rotor electric machine and mechanical arm are connected the storage battery in driving compartment by electric wire.
When the utility model uses, according to designing requirement, according to actual needs, as aerial pick up camera in load etc., manipulation operation device just can carry out aircraft lifting, the running job such as to turn to.
Because the utility model design have employed technique scheme, efficiently solve existing aircraft integral structure huge complicated, awkward problem.The advantages such as it has simple and practical, and practical application controls flexibly, and direction adjusts, landing is easy to control, applied range, easy to use, are applicable to aircraft industry, meteorological industry, aerial prospecting, take photo in the sky, agricultural takes precautions against natural calamities operation etc.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is described in further detail.
Fig. 1 is the structure diagram of the utility model embodiment.
Fig. 2 is the left view of Fig. 1 embodiment.
The structure diagram of Fig. 3 to be another embodiment cabin body of the utility model be ball-table shape cabin body.
The structure diagram of Fig. 4 to be the utility model another embodiment cabin body be spherical tanks body.
In accompanying drawing, each label is: the ball-table shape cabin body of 1 band segment cap; 1-1 ball-table shape cabin body; 1-2 spherical tanks body; 2 through track; 3 motor helical oars; 3-1 is with screw propeller external rotor electric machine; 4 slide blocks; 5 floor stands; 6 mechanical arms; 7 storage batterys; 8 motor support frames; 9 bracing wires.
Detailed description of the invention
As accompanying drawing 1-2 illustrated embodiment, the utility model comprises: the ball-table shape cabin body 1 of band segment cap, motor helical oar 3, storage battery 7, mechanical arm 6, through track 2, the floor stand 5 of motor support frame 8 and band elasticity rubber tire, storage battery 7 is equiped with in the ball-table shape cabin body 1 of segment cap, mechanical arm 6, be connected with motor support frame 8 with the ball-table shape cabin body 1 of segment cap is equipped with pipe link, motor support frame 8 is equiped with motor helical oar 3, floor stand 5 is installed in the bottom of cabin body, cabin external body be fixed with 4 uniform through track 2, on track 2, the slide block 4 of orbital motion is installed with at every root, slide block 4 is fixed with the motor support frame 8 of annular, and on slide block 4, be fitted with bracing wire 9 be connected to motor support frame 8, be circular arc type track through track 2, slide block 4 is fixed with the mechanical arm 6 in hydraulic compressor connection driving compartment, the motor of motor helical oar 3 is connected the storage battery 7 in driving compartment respectively by electric wire with screw propeller external rotor electric machine, mechanical arm.
See accompanying drawing 3 embodiment, described cabin body is ball-table shape cabin body 1-1.
See accompanying drawing 4, the cabin body of the present embodiment is spherical tanks body 1-2, studs with the band screw propeller external rotor electric machine 3-1 of 2 mutual retrograde rotations on the slide block 4 of track 2.
Claims (7)
1. a course of new aircraft, it comprises cabin body, motor helical oar, storage battery, mechanical arm, it is characterized in that, also comprise through track, slide block and floor stand, be equiped with storage battery, mechanical arm in the body of cabin, cabin external body be fixed with 4 uniform symmetrically through track, on track, be installed with the slide block of orbital motion at every root, slide block is fitted with lifting, steering power mechanism, floor stand is installed in the bottom of cabin body.
2. a kind of course of new aircraft according to claim 1, it is characterized in that, lifting, steering power mechanism are made up of pipe link, motor support frame, motor helical oar, pipe link one end connection sliding block, the other end are connected to motor support frame, and on slide block, be fitted with bracing wire be connected to motor support frame, motor support frame is equiped with motor helical oar.
3. a kind of course of new aircraft according to claim 1, is characterized in that, lifting, steering power mechanism are the band screw propeller external rotor electric machines studding with 2 mutual retrograde rotations on the slide block of track.
4. a kind of course of new aircraft according to claim 1, is characterized in that, cabin body is the cabin body of the ball-table shape of band segment cap, drum type, spherical, ball-table shape.
5. a kind of course of new aircraft according to claim 1, is characterized in that, is circular arc type track through track.
6. a kind of course of new aircraft according to claim 1, is characterized in that, slide block is fixed with the mechanical arm in any one connection driving compartment of hydraulic compressor, bracing wire.
7. a kind of course of new aircraft according to claim 1 or 3, is characterized in that, the motor of motor helical oar, screw propeller external rotor electric machine, mechanical arm are connected the storage battery in driving compartment by electric wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520179545.3U CN204979236U (en) | 2015-03-27 | 2015-03-27 | Novel aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520179545.3U CN204979236U (en) | 2015-03-27 | 2015-03-27 | Novel aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204979236U true CN204979236U (en) | 2016-01-20 |
Family
ID=55113630
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520179545.3U Expired - Fee Related CN204979236U (en) | 2015-03-27 | 2015-03-27 | Novel aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204979236U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109071009A (en) * | 2016-09-26 | 2018-12-21 | 常泰荣 | The aerial vehicle of multipurpose |
-
2015
- 2015-03-27 CN CN201520179545.3U patent/CN204979236U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109071009A (en) * | 2016-09-26 | 2018-12-21 | 常泰荣 | The aerial vehicle of multipurpose |
| CN109071009B (en) * | 2016-09-26 | 2019-09-24 | 常泰荣 | The aerial vehicle of multipurpose |
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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 |
Granted publication date: 20160120 Termination date: 20180327 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |