CN205699452U - A kind of aircraft model plane being applicable under fast state clear shooting and forced landing - Google Patents
A kind of aircraft model plane being applicable under fast state clear shooting and forced landing Download PDFInfo
- Publication number
- CN205699452U CN205699452U CN201620414031.6U CN201620414031U CN205699452U CN 205699452 U CN205699452 U CN 205699452U CN 201620414031 U CN201620414031 U CN 201620414031U CN 205699452 U CN205699452 U CN 205699452U
- Authority
- CN
- China
- Prior art keywords
- forced landing
- fuselage
- applicable under
- under fast
- fast state
- 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
Abstract
The utility model discloses a kind of aircraft model plane being applicable under fast state clear shooting and forced landing, clap as device including fuselage and high definition, described front fuselage is provided with head, described fuselage both sides are provided with wing, described wing interior lower end is provided with speed setting unit, described high definition is clapped as the internal right top of device is provided with projection screen, described projection screen left end is provided with image amplifying device, described high definition is clapped as device right-hand member is provided with connection cross bar, described connection cross bar right-hand member is provided with body and controls main body, described body controls to be provided with guiding flight instruments in the middle of the left top of main body, described guiding flight instruments upper end is provided with flight adjusting means, described flight adjusting means upper right side is provided with guiding flight instruments, described body controls main body right-hand member and is provided with fuselage bascule.This utility model is applicable under fast state the aircraft model plane of clear shooting and forced landing and changes the not fogging clear problem that in the past shoots, and flight safety is quick.
Description
Technical field
This utility model relates to aircraft model plane technical field, a kind of aircraft model plane being applicable under fast state clear shooting and forced landing.
Background technology
" model airplane is a kind of to overweight air to clear stipulaties in the rules of contest that International Aeronautical Federation formulates, there is size limitation, with or without electromotor, remote-controlled can not be manned airborne vehicle, " aeromodelling airplane is general as manned aircraft, main by wing, empennage, fuselage, undercarriage and electromotor and control system six part form, but existing aircraft model plane require the highest owing to flight speed is too fast for aerial shooting, and the problem such as the picture that usually there will be shooting is unintelligible, simultaneously it is also possible to there will be prominent emergency of meeting not know problems such as how avoiding.
Summary of the invention
The purpose of this utility model is to provide a kind of aircraft model plane being applicable under fast state clear shooting and forced landing, with the problem solving to propose in above-mentioned background technology.
nullFor achieving the above object，This utility model provides following technical scheme: a kind of being applicable under fast state clearly shoots and the aircraft model plane of forced landing，Clap as device including fuselage and high definition，Described front fuselage is provided with head，Described fuselage both sides are provided with wing，Described wing interior lower end is provided with speed setting unit，Described speed setting unit upper end is provided with electromotor，Its wing、Electromotor and speed setting unit are uniformly and symmetrically distributed in fuselage both sides，Described afterbody both sides are provided with empennage，And it is symmetrical，Described high definition is clapped as the internal right top of device is provided with projection screen，Described projection screen left end is provided with image amplifying device，Described image amplifying device left end is provided with data image stocking system，Described data image stocking system lower end is provided with telescopic stem，Described telescopic stem lower end is provided with high-definition camera，Described high definition is clapped as device right-hand member is provided with connection cross bar，Described connection cross bar right-hand member is provided with body and controls main body，Described body controls to be provided with guiding flight instruments in the middle of the left top of main body，Described guiding flight instruments upper end is provided with flight adjusting means，Described flight adjusting means upper right side is provided with fixed number device，Described fixed number device lower end is provided with PLC ECU，Described PLC ECU lower end is provided with forced landing safe mode device，Described body controls main body right-hand member and is provided with fuselage bascule.
Preferably, in the middle of described empennage, tail is installed.
Preferably, the internal middle-end of described telescopic stem is provided with photographic head focalizer.
Preferably, described photographic head focalizer is connected with high-definition camera by photographic head connecting rod.
Preferably, described connection cross bar both sides are separately installed with wheel.
Preferably, described forced landing safe mode device left end is provided with intelligent display regulation control panel.
Compared with prior art, the beneficial effects of the utility model are: this kind is applicable under fast state clear shooting and uses high-end PLC control technology with the aircraft model plane of forced landing, whole process is controlled according to the wish of people, front fuselage is provided with high-end filming apparatus, multiple high-definition camera is utilized to form a flight arc formula photographic head group, focus on through photographic head focalizer and integrate, the aircraft flight too fast object problem that should not choose shooting when can solve flight, ensure that the clarity of shooting object, and the design of also forced landing safe mode device, avoid the aerial prominent problem meeting danger, alleviate the extent of damage to material, make its mold cycle utilization rate high.
Accompanying drawing explanation
Fig. 1 is a kind of aircraft model plane agent structure schematic diagram being applicable under fast state clear shooting and forced landing of this utility model；
Fig. 2 is that this utility model is a kind of is applicable under fast state the clear shooting aircraft model plane high definition bat with forced landing as apparatus structure schematic diagram；
Fig. 3 is a kind of aircraft model plane body control agent structure schematic diagram being applicable under fast state clear shooting and forced landing of this utility model.
In figure: 1-wing；2-wheel；3-fuselage；4-head；5-high definition is clapped as device；6-connects cross bar；7-speed setting unit；8-electromotor；9-body controls main body；10-fuselage bascule；11-empennage；12-tail；13-high-definition camera；14-photographic head connecting rod；15-photographic head focalizer；16-telescopic stem；17-data image stocking system；18-image amplifying device；19-shows screen；20-guides flight instruments；21-flight adjusting means；22-fixed number device；23-PLC ECU；24-forced landing safe mode device；25-intelligent display regulation control panel.
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 clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
nullRefer to Fig. 1-3，A kind of embodiment that this utility model provides: a kind of aircraft model plane being applicable under fast state clear shooting and forced landing，Clap as device 5 including fuselage 3 and high definition，Fuselage 3 front end is provided with head 4，Fuselage 3 both sides are provided with wing 1，Wing 1 interior lower end is provided with speed setting unit 7，Speed setting unit 7 upper end is provided with electromotor 8，Its wing 1、Electromotor 8 and speed setting unit 7 are uniformly and symmetrically distributed in fuselage 3 both sides，Fuselage 3 two sides of tail is provided with empennage 11，And it is symmetrical，In the middle of empennage 11, tail 12 is installed，High definition is clapped as the internal right top of device 5 is provided with projection screen 19，Projection screen 19 left ends are provided with image amplifying device 18，Image amplifying device 18 left end is provided with data image stocking system 17，Data image stocking system 17 lower end is provided with telescopic stem 16，The internal middle-end of telescopic stem 16 is provided with photographic head focalizer 15，Photographic head focalizer 15 is connected with high-definition camera 13 by photographic head connecting rod 14，Telescopic stem 16 lower end is provided with high-definition camera 13，High definition is clapped as device 5 right-hand member is provided with connection cross bar 6，Connect cross bar 6 both sides and be separately installed with wheel 2，Connect cross bar 6 right-hand member and body control main body 9 is installed，Body controls to be provided with guiding flight instruments 20 in the middle of the left top of main body 9，Guide flight instruments 20 upper end and flight adjusting means 21 is installed，Flight adjusting means 21 upper right side is provided with fixed number device 22，Fixed number device 22 lower end is provided with PLC ECU 23，PLC ECU 23 lower end is provided with forced landing safe mode device 24，Forced landing safe mode device 24 left end is provided with intelligent display regulation control panel 25，Body controls main body 9 right-hand member and is provided with fuselage bascule 10.
Specifically used mode: this utility model, user is by the regulation to intelligent display regulation control panel 25, by fixed number device 22 is controlled its heading flight time and flying distance, by PLC ECU 23, flight adjusting means 21 is controlled, under the co-ordination of flight adjusting means 21, aircraft is through engine start, speed per hour is regulated through speed setting unit 7, aircraft is kept to fly steadily through fuselage bascule 10, these a kind of aircraft model plane being applicable under fast state clear shooting and forced landing are flown, forced landing safe mode device 24 forced landing can be passed through when in case of emergency, until whole flight terminates, whole aircraft model plane complete the process of taking a flight test.
It is obvious to a person skilled in the art that this utility model is not limited to the details of above-mentioned one exemplary embodiment, and in the case of without departing substantially from spirit or essential attributes of the present utility model, it is possible to realize this utility model in other specific forms.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above, it is intended that all changes fallen in the implication of equivalency and scope of claim included in this utility model.Should not be considered as limiting involved claim by any reference in claim.
Claims (6)
- null1. the aircraft model plane being applicable under fast state clear shooting and forced landing，Clap as device (5) including fuselage (3) and high definition，Its feature is: described fuselage (3) front end is provided with head (4)，Described fuselage (3) both sides are provided with wing (1)，Described wing (1) interior lower end is provided with speed setting unit (7)，Described speed setting unit (7) upper end is provided with electromotor (8)，Wing (1) and electromotor (8) are uniformly and symmetrically distributed in fuselage (3) both sides with speed setting unit (7)，Described fuselage (3) two sides of tail is provided with empennage (11)，And it is symmetrical，Described high definition is clapped as the internal right top of device (5) is provided with projection screen (19)，Described projection screen (19) left end is provided with image amplifying device (18)，Described image amplifying device (18) left end is provided with data image stocking system (17)，Described data image stocking system (17) lower end is provided with telescopic stem (16)，Described telescopic stem (16) lower end is provided with high-definition camera (13)，Described high definition is clapped as device (5) right-hand member is provided with connection cross bar (6)，Described connection cross bar (6) right-hand member is provided with body and controls main body (9)，Described body controls to be provided with in the middle of main body (9) left top guiding flight instruments (20)，Described guiding flight instruments (20) upper end is provided with flight adjusting means (21)，Described flight adjusting means (21) upper right side is provided with fixed number device (22)，Described fixed number device (22) lower end is provided with PLC ECU (23)，Described PLC ECU (23) lower end is provided with forced landing safe mode device (24)，Described body controls main body (9) right-hand member and is provided with fuselage bascule (10).
- A kind of aircraft model plane being applicable under fast state clear shooting and forced landing the most according to claim 1, it is characterised in that: in the middle of described empennage (11), tail (12) is installed.
- A kind of aircraft model plane being applicable under fast state clear shooting and forced landing the most according to claim 1, it is characterised in that: the internal middle-end of described telescopic stem (16) is provided with photographic head focalizer (15).
- A kind of aircraft model plane being applicable under fast state clear shooting and forced landing the most according to claim 1, it is characterised in that: described photographic head focalizer (15) is connected with high-definition camera (13) by photographic head connecting rod (14).
- A kind of aircraft model plane being applicable under fast state clear shooting and forced landing the most according to claim 1, it is characterised in that: described connection cross bar (6) both sides are separately installed with wheel (2).
- A kind of aircraft model plane being applicable under fast state clear shooting and forced landing the most according to claim 1, it is characterised in that: described forced landing safe mode device (24) left end is provided with intelligent display regulation control panel (25).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620414031.6U CN205699452U (en) | 2016-05-10 | 2016-05-10 | A kind of aircraft model plane being applicable under fast state clear shooting and forced landing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620414031.6U CN205699452U (en) | 2016-05-10 | 2016-05-10 | A kind of aircraft model plane being applicable under fast state clear shooting and forced landing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205699452U true CN205699452U (en) | 2016-11-23 |
Family
ID=57304118
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620414031.6U Expired - Fee Related CN205699452U (en) | 2016-05-10 | 2016-05-10 | A kind of aircraft model plane being applicable under fast state clear shooting and forced landing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205699452U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107050882A (en) * | 2017-02-18 | 2017-08-18 | 佛山市三水区希望火炬教育科技有限公司 | A kind of tractor aeroplane with music apparatus |
-
2016
- 2016-05-10 CN CN201620414031.6U patent/CN205699452U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107050882A (en) * | 2017-02-18 | 2017-08-18 | 佛山市三水区希望火炬教育科技有限公司 | A kind of tractor aeroplane with music apparatus |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205386330U (en) | Unmanned aerial vehicle laser CS recreation fight system | |
| JP2017206238A5 (en) | ||
| CN205699452U (en) | A kind of aircraft model plane being applicable under fast state clear shooting and forced landing | |
| CN204406207U (en) | Based on the system of travelling of unmanned air vehicle technique and head movement capturing technology | |
| CN106114881B (en) | Unmanned plane | |
| CN106915453A (en) | A kind of takeoff and landing mode and system | |
| Gerathewohl et al. | Experiments during weightlessness: A study of the oculo-agravic illusion. | |
| CN204956947U (en) | Can multidirectional model aeroplane and model ship of gathering real -time image | |
| CN207580162U (en) | A kind of visible ray and thermal imaging quadrotor unmanned plane | |
| CN104192301B (en) | A kind of manpower variable wing plane | |
| CN206885351U (en) | A kind of takeoff and landing system | |
| CN206125432U (en) | Unmanned plane flaming device | |
| CN206492210U (en) | A kind of model aircraft of suitable night flying | |
| CN204364885U (en) | A kind of duct model plane | |
| US8733705B2 (en) | Aircraft rescue device | |
| CN211178156U (en) | Unmanned drone | |
| CN105730697A (en) | Camera shooting aircraft | |
| CN209912190U (en) | Ejection life-saving training system based on VR | |
| CN203497168U (en) | Front camera bin of unmanned plane | |
| CN202642097U (en) | Flight detector | |
| CN104443417A (en) | Aerial photographing aircraft | |
| RU173153U1 (en) | Attraction simulator with a multi-rotor drone type | |
| CN108829122A (en) | A kind of take-off attitude control method of horizontal air-drop unmanned plane | |
| CN205055432U (en) | Model aeroplane and model ship aircraft with water skis | |
| RU186196U1 (en) | FOKIN SAFE PLANE |
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: 20161123 Termination date: 20170510 |