CN107284682A - A kind of GPS supports of unmanned plane - Google Patents
A kind of GPS supports of unmanned plane Download PDFInfo
- Publication number
- CN107284682A CN107284682A CN201710525316.6A CN201710525316A CN107284682A CN 107284682 A CN107284682 A CN 107284682A CN 201710525316 A CN201710525316 A CN 201710525316A CN 107284682 A CN107284682 A CN 107284682A
- Authority
- CN
- China
- Prior art keywords
- pole
- gps
- chassis
- mounting
- installing
- 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.)
- Pending
Links
- 230000008054 signal transmission Effects 0.000 abstract description 4
- 238000013461 design Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
- B64U2201/104—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] using satellite radio beacon positioning systems, e.g. GPS
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The invention discloses a kind of GPS supports of unmanned plane, belong to the design field of unmanned plane, chassis that the GPS supports include being fixed on the fuselage of unmanned plane, the pole that is vertically set on chassis and be installed on pole top and the mounting disc for installing GPS navigation device；Chassis is diametrically offering the mounting groove for installing pole；Pole is up-narrow and down-wide trapezoidal, and the bottom of pole has the mounting bar being fixed in mounting groove, and top, which is provided with, is used for the screwed hole for installing mounting disc.The GPS supporting structures of the present invention are stable, are difficult to be influenceed by weather, to the firm supporting of GPS navigation device, so that the signal transmission of GPS navigation device is more stablized.
Description
Technical field
The present invention relates to the design field of unmanned plane, specifically, it is related to a kind of GPS supports of unmanned plane.
Background technology
In recent years, unmanned air vehicle technique has the development advanced by leaps and bounds.Because its cost is low, mobility is good, survival ability
By force, the advantages of risk that no one was injured, unmanned plane occupies extremely important status in modern military war, in civil area
Have boundless prospect, at present taking photo by plane, agricultural, plant protection, miniature auto heterodyne, express transportation, disaster relief, observe wild dynamic
The occasions such as thing, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance obtain widely should
With having expanded the purposes and value of unmanned plane in itself significantly.
GPS navigation device would generally be carried on unmanned plane to be used to control flight path, and current GPS navigation device is typically directly pacified
Installed on the fuselage of unmanned plane or by GPS supports, be easy to the transmission of signal.Existing GPS supports are in order to mitigate
The overall weight of unmanned plane, GPS navigation device is installed using the pole of thin rod shape, causes GPS navigation device easily by environment or day
The influence of gas, such as in weather of blowing because pole carefully causes GPS navigation device to rock back and forth very much, influence signal transmission.
The content of the invention
The purpose of the present invention is provides a kind of GPS supports of unmanned plane, and the GPS supports can transmit the signal of unmanned plane
More stablize.
To achieve these goals, the GPS supports for the unmanned plane that the present invention is provided include the fuselage for being fixed on unmanned plane
On chassis, the pole that is vertically set on chassis and be installed on pole top and the mounting disc for installing GPS navigation device；
Chassis is diametrically offering the mounting groove for installing pole；Pole is up-narrow and down-wide trapezoidal, the bottom tool of pole
There is the mounting bar being fixed in mounting groove, top is provided with the screwed hole for being used for installing mounting disc.
GPS supporting structures in above-mentioned technical proposal are stable, are difficult to be influenceed by weather, to the firm supporting of GPS navigation device,
So that the signal transmission of GPS navigation device is more stablized.
Specific scheme is provided with boss, boss for the bottom of mounting disc and is provided with fixing groove, and bottom land is offered and screwed hole
Corresponding through hole.The top of pole is stretched into fixing groove and is fixed again by screw, prevents mounting disc from being rotated relative to pole,
Further increase the stability of GPS supports.
Another specific scheme is that pole is provided with to mitigate some hollow outs of own wt, and hollow out is symmetrically distributed in branch
The center line both sides of bar.Make pole more attractive in appearance along pole center line is symmetrical hollow out.
Another specific scheme is chassis provided with some arcuate sockets for being used to fixing and adjusting itself direction, arcuate socket
It is interior to be provided with the step for being easily installed screw.Can making chassis by arcuate socket, arcuately direction adjusts self-view when fixing, with
Find optimum signal position.
Further specific scheme is that the middle part of mounting groove is provided with the positioning hole with raised rotary shaft contraposition on fuselage, is installed
Screwed hole of the two ends of groove provided with fastening mounting bar.Further increased by the rotary shaft for setting positioning hole and coordinating with positioning hole
The stability of GPS supports is added.
Another specific scheme is provided with the surrounding edge for being used for installing and protect GPS navigation device for the edge of mounting disc, and this encloses
The breach for leading to line is offered on side.
Compared with prior art, beneficial effects of the present invention are：
The GPS supports of the present invention are compared to existing GPS supports, and it, which is installed, more stablizes, and has guarantor to GPS navigation utensil
Shield is acted on, and is transmitted the signal of unmanned plane and is more stablized.
Brief description of the drawings
Fig. 1 is the front view of the embodiment of the present invention；
Fig. 2 is the stereogram of the embodiment of the present invention；
Fig. 3 is the stereogram on the chassis of the embodiment of the present invention；
Fig. 4 is the stereogram of the pole of the embodiment of the present invention；
Fig. 5 is the stereogram of the mounting disc of the embodiment of the present invention.
Wherein：4th, GPS supports；41st, chassis；411st, arcuate socket；412nd, mounting groove；413rd, positioning hole；414th, screwed hole；
42nd, pole；421st, mounting bar；422nd, through hole；423rd, screwed hole；43rd, mounting disc；431st, boss；432nd, fixing groove；433rd, lead to
Hole；434th, surrounding edge；435th, breach.
Embodiment
With reference to embodiments and its accompanying drawing the invention will be further described.
Embodiment
Referring to Fig. 1 to Fig. 5, the GPS supports 4 of unmanned plane include chassis 41, pole 42 and mounting disc 43, and pole 42 is hung down
Directly it is fixed on chassis 41, mounting disc 43 is fixed on the top of pole 42, for installing GPS navigation device.
Chassis 41, which is provided with some arcuate sockets 411, arcuate socket 411, is provided with step, is easily installed screw, screw leads to successively
The screwed hole crossed on arcuate socket 411 and fuselage upper casing, which is tightened, makes chassis 41 be fixed on fuselage, meanwhile, can by arcuate socket 411
The angle of the whole GPS supports 4 of rotation adjustment, so as to adjust the receiving side signal of GPS navigation device to find optimum orientation.
Chassis 41 is diametrically offering the mounting groove 412 for installing pole 42, the middle part of mounting groove 412 be provided with fuselage
The positioning hole 413 of raised rotary shaft contraposition, screwed hole 414 is additionally provided with the two ends of mounting groove 412, and screwed hole 414 is used to fasten
Pole 42.
Pole 42 is up-narrow and down-wide trapezoidal, and its thickness is between 5~8mm, and bottom has the peace coordinated with mounting groove 412
Bar 421 is filled, mounting bar 421 is provided with through hole 422 corresponding with screwed hole 414.The top of pole 42, which is provided with, to be used to install
The screwed hole 423 of disk 43.Pole 42 is provided with some hollow outs, to mitigate own wt, for visual appearance, all hollow outs edges branch
The center line of bar 42 is arranged symmetrically.
The bottom of mounting disc 43 is provided with boss 431, boss 431 provided with the fixing groove for accommodating and fixing the top of pole 42
432, bottom land offers through hole 433, and the through hole 433 is corresponding with screwed hole 423.The edge of mounting disc 43 be provided be used for install and
The surrounding edge 434 of GPS navigation device is protected, the breach 435 for leading to line is offered on surrounding edge 434.
The foregoing is only the preferable implementation example of the present invention, be not intended to limit the invention, it is all in spirit of the invention and
Within principle, any modification, equivalent substitution and improvements made etc. should be included in the scope of the protection.
Claims (6)
1. a kind of GPS supports of unmanned plane, it is characterised in that：
Including the chassis being fixed on the fuselage of unmanned plane, the pole being vertically set on the chassis and it is installed on the branch
Bar top and the mounting disc for installing GPS navigation device；
The chassis is diametrically offering the mounting groove for installing the pole；
The pole is up-narrow and down-wide trapezoidal, and the bottom of pole has the mounting bar being fixed in the mounting groove, and top is set
There is the screwed hole for installing the mounting disc.
2. GPS supports according to claim 1, it is characterised in that：
The bottom of the mounting disc, which is provided with boss, boss, is provided with fixing groove, and bottom land offers corresponding with the screwed hole logical
Hole.
3. GPS supports according to claim 1, it is characterised in that：
Described pole is provided with to mitigate some hollow outs of own wt, and hollow out is symmetrically distributed in the center line both sides of pole.
4. GPS supports according to claim 1, it is characterised in that：
Described chassis is easily installed spiral shell provided with some arcuate sockets for being used to fixing and adjusting itself direction, interior be provided with of arcuate socket
The step of nail.
5. GPS supports according to claim 4, it is characterised in that：
The middle part of the mounting groove is provided with the positioning hole with raised rotary shaft contraposition on fuselage, and the two ends of mounting groove are provided with fastening institute
State the screwed hole of mounting bar.
6. GPS supports according to claim 1, it is characterised in that：
The edge of the mounting disc is provided with the surrounding edge for being used for installing and protect GPS navigation device, the surrounding edge and offered for leading to line
Breach.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710525316.6A CN107284682A (en) | 2017-06-30 | 2017-06-30 | A kind of GPS supports of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710525316.6A CN107284682A (en) | 2017-06-30 | 2017-06-30 | A kind of GPS supports of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107284682A true CN107284682A (en) | 2017-10-24 |
Family
ID=60099675
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710525316.6A Pending CN107284682A (en) | 2017-06-30 | 2017-06-30 | A kind of GPS supports of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107284682A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108163218A (en) * | 2017-12-29 | 2018-06-15 | 顺丰科技有限公司 | Navigate stent |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2261523Y (en) * | 1996-02-12 | 1997-09-03 | 圣宥电器工业股份有限公司 | Electric fan seat |
| CN103950539A (en) * | 2014-05-27 | 2014-07-30 | 姜学海 | Multifunctional unmanned aerial vehicle |
| CN203873792U (en) * | 2014-06-16 | 2014-10-15 | 刘玉栋 | B ultrasonic examination device |
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN205424332U (en) * | 2015-12-19 | 2016-08-03 | 云南熙祥航空科技有限公司 | GPS installing support |
| US9527588B1 (en) * | 2012-09-28 | 2016-12-27 | Scott B. Rollefstad | Unmanned aircraft system (UAS) with active energy harvesting and power management |
| CN206125436U (en) * | 2016-08-31 | 2017-04-26 | 长沙拓航农业科技有限公司 | Many rotors of abnormal shape plant protection unmanned aerial vehicle |
| CN206914657U (en) * | 2017-06-30 | 2018-01-23 | 浙江大学 | A kind of GPS supports on unmanned plane |
-
2017
- 2017-06-30 CN CN201710525316.6A patent/CN107284682A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2261523Y (en) * | 1996-02-12 | 1997-09-03 | 圣宥电器工业股份有限公司 | Electric fan seat |
| US9527588B1 (en) * | 2012-09-28 | 2016-12-27 | Scott B. Rollefstad | Unmanned aircraft system (UAS) with active energy harvesting and power management |
| CN103950539A (en) * | 2014-05-27 | 2014-07-30 | 姜学海 | Multifunctional unmanned aerial vehicle |
| CN203873792U (en) * | 2014-06-16 | 2014-10-15 | 刘玉栋 | B ultrasonic examination device |
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN205424332U (en) * | 2015-12-19 | 2016-08-03 | 云南熙祥航空科技有限公司 | GPS installing support |
| CN206125436U (en) * | 2016-08-31 | 2017-04-26 | 长沙拓航农业科技有限公司 | Many rotors of abnormal shape plant protection unmanned aerial vehicle |
| CN206914657U (en) * | 2017-06-30 | 2018-01-23 | 浙江大学 | A kind of GPS supports on unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108163218A (en) * | 2017-12-29 | 2018-06-15 | 顺丰科技有限公司 | Navigate stent |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171024 |
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| RJ01 | Rejection of invention patent application after publication |