CN107648867A - A kind of aircraft model with anticollision device, collision-prevention device - Google Patents
A kind of aircraft model with anticollision device, collision-prevention device Download PDFInfo
- Publication number
- CN107648867A CN107648867A CN201710989780.0A CN201710989780A CN107648867A CN 107648867 A CN107648867 A CN 107648867A CN 201710989780 A CN201710989780 A CN 201710989780A CN 107648867 A CN107648867 A CN 107648867A
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- China
- Prior art keywords
- wing
- fuselage
- tail
- collision
- remote
- 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.)
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Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/02—Model aircraft
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H30/00—Remote-control arrangements specially adapted for toys, e.g. for toy vehicles
- A63H30/02—Electrical arrangements
- A63H30/04—Electrical arrangements using wireless transmission
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of aircraft model with anticollision device, collision-prevention device, including head, fuselage, wing, tail and remote-control handle;The head is internally provided with fixed plate and spring, vertical tail and puff prot are provided with the tail, the vertical tail is located at tail crown center, the puff prot is located at the tail end of tail, fuselage both sides middle is provided with porthole, the fuselage bottom is connected with preceding wheel by nose-gear, the fuselage bottom is connected with rear wheel by rear undercarriage, the wing is fixedly mounted on fuselage side, the wing tip portion is provided with micro radar scanner, arrow button is provided with the remote-control handle, shift knob, command antenna and speed button.When the present invention can realize aeromodelling airplane flight in the air, to the avoidance of barrier, the follow-on mission performance of aeromodelling airplane is improved, practical, easy to utilize, the spring that head is set helps to mitigate the infringement to aeromodelling airplane when running into collision.
Description
The invention belongs to model plane technical field, specially a kind of aircraft model with anticollision device, collision-prevention device.
Background technology
In the modern life, aeromodelling airplane obtains the understanding of more and more people and liked, various types of aeromodelling airplane styles
Happen frequently.Even if but in open place, during without other barriers, during the flight in the air simultaneously of multi rack aeromodelling airplane, still deposit
It is possible in collision, a series of troubles are caused, common aeromodelling airplane cost is expensive, technical sophistication, it is often more important that in general model plane
Aircraft does not set safety collision-protection device, and if running into emergency, it is unavoidable to cause damage, therefore aeromodelling airplane
Anticollision device, collision-prevention device setting it is very necessary.
The content of the invention
It is an object of the invention to provide a kind of aircraft model with anticollision device, collision-prevention device, to solve to propose in above-mentioned background technology
The problem of, possessed beneficial effect is:When the present invention can realize aeromodelling airplane flight in the air, to the avoidance of barrier,
The follow-on mission performance of aeromodelling airplane is improved, practical, easy to utilize, the spring that head is set helps to touch running into
Mitigate the infringement to aeromodelling airplane when hitting.
To achieve the above object, the present invention provides following technical scheme:A kind of aircraft model with anticollision device, collision-prevention device, including machine
Head, fuselage, wing, tail and remote-control handle;The head is internally provided with fixed plate and spring, and fixed plate is fixed with spring
Connection, the crown center of the fuselage, which is set, is provided with supporting table, and radio receiver is installed with supporting table, described
Vertical tail and puff prot are provided with tail, and tailplane is provided with vertical tail, the vertical tail is located at tail
At crown center, the puff prot is located at the tail end of tail, and fuselage both sides middle is provided with porthole, and on fuselage outer wall
Hatch door is installed, the fuselage bottom is connected with preceding wheel by nose-gear, and the fuselage bottom passes through rear with rear wheel
Fall frame connection, and rear wheel is provided with two, the wing is fixedly mounted on fuselage side, and the wing tip portion is provided with miniature
Radar scanner, and wing bottom is provided with motor, the motor internal is provided with drive shaft, and drive shaft and propeller rotational
Connection, the motor bottom are provided with charging plug, and arrow button, shift knob, instruction day are provided with the remote-control handle
Line and speed button, and command antenna is located at remote-control handle upper right side.
Preferably, the hatch door is located at the left side of porthole, and porthole is provided with six.
Preferably, the wing includes port wing and starboard wing, and port wing is symmetrically fixed with starboard wing by fuselage.
Preferably, the micro radar scanner is provided with one, and micro radar scanner is fixed on port wing.
Compared with prior art, the beneficial effects of the invention are as follows:When the present invention can realize aeromodelling airplane flight in the air,
To the avoidance of barrier, the follow-on mission performance of aeromodelling airplane is improved, practical, easy to utilize, the bullet that head is set
Spring helps to mitigate the infringement to aeromodelling airplane when running into collision, and the micro radar scanner installed on wing can be supplied to
Aeromodelling airplane in flight around obstacle information, when barrier occurs, information can be fed back to by radio receiver
On remote-control handle so that aeromodelling airplane can be effectively prevented from flight way bumping against with barrier.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention;
Fig. 2 is the top view of the present invention;
Fig. 3 is the structural representation of remote-control handle of the present invention.
In figure:1- fixed plates;2- springs;3- heads;4- fuselages;5- supporting tables;6- radio receivers;The horizontal tails of 7-
The wing;8- vertical tails;9- hatch doors;10- nose-gears;Wheel before 11-;12- propellers;13- micro radar scanners;14- electricity
Machine;15- charging plugs;16- wings;17- drive shafts;Wheel after 18-;Undercarriage after 19-;20- portholes;21- tails;22- sprays
Gas port;23- remote-control handles;24- arrow buttons;25- shift knobs;26- command antennas;27- speed buttons.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
Refer to Fig. 1-3, a kind of embodiment provided by the invention:A kind of aircraft model with anticollision device, collision-prevention device, including head
3rd, fuselage 4, wing 16, tail 21 and remote-control handle 23;Head 3 is internally provided with fixed plate 1 and spring 2, and fixed plate 1 and bullet
Spring 2 is fixedly connected, and the crown center of fuselage 4, which is set, is provided with supporting table 5, and is installed with radio reception in supporting table 5
Device 6, vertical tail 8 and puff prot 22 are provided with tail 21, and tailplane 7 is provided with vertical tail 8, vertical tail 8
At the crown center of tail 7, puff prot 22 is located at the tail end of tail 21, and the both sides middle of fuselage 4 is provided with porthole 20, and machine
Hatch door 9 is installed, the bottom of fuselage 4 is connected with preceding wheel 11 by nose-gear 10, the bottom of fuselage 4 and rear wheel on the outer wall of body 4
18 are connected by rear undercarriage 19, and rear wheel 18 is provided with two, and wing 16 is fixedly mounted on the side of fuselage 4, and wing 16 pushes up
Portion is provided with micro radar scanner 13, and the bottom of wing 16 is provided with motor 14, and motor 14 is internally provided with drive shaft 17, and
Drive shaft 17 is rotatablely connected with propeller 12, and the bottom of motor 14 is provided with charging plug 15, and direction is provided with remote-control handle 23
Button 24, shift knob 25, command antenna 26 and speed button 27, and command antenna 26 is located at the upper right side of remote-control handle 23, cabin
Door 9 is located at the left side of porthole 20, and porthole 20 is provided with six, and wing 16 includes port wing and starboard wing, and port wing and the right side
Wing is symmetrically fixed by fuselage 4, and micro radar scanner 13 is provided with one, and micro radar scanner 13 is fixed on left machine
On the wing.
Operation principle:That presses shift knob 25 drives button so that remote-control handle 23 is in running order, then passes through behaviour
Make arrow button 24 and speed button 27 so that instruction is sent to the radio at the top of aeromodelling airplane by command antenna 26
On receiver 6, in the microprocessor that then instruction is delivered in motor 14 so that the work of motor 14 drives 12 turns of propeller
Dynamic, so that aeromodelling airplane can fly, the micro radar scanner 13 on wing 16 is used for scanning peripheral obstacle information,
Obstacle information is effectively fed back on remote-control handle by radio receiver 6, so as to timely hide obstacle
Thing, the interior spring 2 set of head 4 can effectively mitigate the infringement that aeromodelling airplane receives in collision.
It is obvious to a person skilled in the art that the invention is not restricted to the details of above-mentioned one exemplary embodiment, Er Qie
In the case of without departing substantially from spirit or essential attributes of the invention, the present invention can be realized 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, the scope of the present invention is by appended power
Profit requires rather than described above limits, it is intended that all in the implication and scope of the equivalency of claim by falling
Change is included in the present invention.Any reference in claim should not be considered as to the involved claim of limitation.
Claims (4)
1. a kind of aircraft model with anticollision device, collision-prevention device, including head (3), fuselage (4), wing (16), tail (21) and remote control hand
Handle (23);It is characterized in that:The head (3) is internally provided with fixed plate (1) and spring (2), and fixed plate (1) and spring
(2) it is fixedly connected, the crown center of the fuselage (4), which is set, is provided with supporting table (5), and is installed with supporting table (5)
Radio receiver (6), tail (21) place is provided with vertical tail (8) and puff prot (22), and is set on vertical tail (8)
Tailplane (7) is equipped with, the vertical tail (8) is located at tail (7) crown center, and the puff prot (22) is located at tail
(21) tail end, fuselage (4) the both sides middle is provided with porthole (20), and is provided with hatch door (9) on fuselage (4) outer wall,
Fuselage (4) bottom is connected with preceding wheel (11) by nose-gear (10), and fuselage (4) bottom is logical with rear wheel (18)
Later undercarriage (19) connects, and rear wheel (18) is provided with two, and the wing (16) is fixedly mounted on fuselage (4) side,
Micro radar scanner (13) is provided with the top of the wing (16), and wing (16) bottom is provided with motor (14), the electricity
Machine (14) is internally provided with drive shaft (17), and drive shaft (17) is rotatablely connected with propeller (12), motor (14) bottom
Charging plug (15) is provided with, arrow button (24), shift knob (25), command antenna are provided with the remote-control handle (23)
(26) and speed button (27), and command antenna (26) is located at remote-control handle (23) upper right side.
A kind of 2. aircraft model with anticollision device, collision-prevention device according to claim 1, it is characterised in that:The hatch door (9) is located at
The left side of porthole (20), and porthole (20) is provided with six.
A kind of 3. aircraft model with anticollision device, collision-prevention device according to claim 1, it is characterised in that:The wing (16) includes
Port wing and starboard wing, and port wing and starboard wing are symmetrically fixed by fuselage (4).
A kind of 4. aircraft model with anticollision device, collision-prevention device according to claim 1, it is characterised in that:The micro radar scanning
Instrument (13) is provided with one, and micro radar scanner (13) is fixed on port wing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710989780.0A CN107648867A (en) | 2017-10-21 | 2017-10-21 | A kind of aircraft model with anticollision device, collision-prevention device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710989780.0A CN107648867A (en) | 2017-10-21 | 2017-10-21 | A kind of aircraft model with anticollision device, collision-prevention device |
Publications (1)
Publication Number | Publication Date |
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CN107648867A true CN107648867A (en) | 2018-02-02 |
Family
ID=61118958
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710989780.0A Withdrawn CN107648867A (en) | 2017-10-21 | 2017-10-21 | A kind of aircraft model with anticollision device, collision-prevention device |
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CN (1) | CN107648867A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108888970A (en) * | 2018-09-18 | 2018-11-27 | 高岩 | A kind of fixed-wing model plane convenient for landing training |
CN109173286A (en) * | 2018-09-19 | 2019-01-11 | 范翰臻 | A kind of aeromodelling airplane with anticollison block |
-
2017
- 2017-10-21 CN CN201710989780.0A patent/CN107648867A/en not_active Withdrawn
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108888970A (en) * | 2018-09-18 | 2018-11-27 | 高岩 | A kind of fixed-wing model plane convenient for landing training |
CN108888970B (en) * | 2018-09-18 | 2023-10-27 | 高岩 | Fixed wing model aeroplane and model ship convenient to take off and land training |
CN109173286A (en) * | 2018-09-19 | 2019-01-11 | 范翰臻 | A kind of aeromodelling airplane with anticollison block |
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PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WW01 | Invention patent application withdrawn after publication | ||
WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180202 |