CN201350344Y - Telecontrolled aircraft with missiles - Google Patents
Telecontrolled aircraft with missiles Download PDFInfo
- Publication number
- CN201350344Y CN201350344Y CNU2009200038535U CN200920003853U CN201350344Y CN 201350344 Y CN201350344 Y CN 201350344Y CN U2009200038535 U CNU2009200038535 U CN U2009200038535U CN 200920003853 U CN200920003853 U CN 200920003853U CN 201350344 Y CN201350344 Y CN 201350344Y
- Authority
- CN
- China
- Prior art keywords
- electronic ignition
- telecontrolled aircraft
- ignition head
- remote controller
- guided missile
- 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
Images
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a telecontrolled aircraft with missiles, which comprises a telecontrolled aircraft body and an aircraft control remote controller, wherein the telecontrolled aircraft is provided with an aircraft control receiver, a missile launch tube and an electronic ignition head are arranged on the telecontrolled aircraft body, a pyrotechnical jet body is arranged in the missile launch tube, the back portion of the pyrotechnical jet body is connected with the electronic ignition head, and the electronic ignition head is wirelessly connected with an electronic ignition remote controller through an electronic ignition head control receiver. The telecontrolled aircraft can launch missiles on the fly, and has strong entertainment.
Description
Technical field:
The utility model relates to a kind of toy; Relate in particular to a kind of telecontrolled aircraft.
Background technology:
Existing telecontrolled aircraft comprises a telecontrolled aircraft body and remote controller, by the motion control of remote controller realization to telecontrolled aircraft.But existing telecontrolled aircraft body only can be done remote control distributor, and is recreational smaller.
The utility model content:
In order to overcome the single technical deficiency of existing telecontrolled aircraft noumenon function; The purpose of this utility model provides the telecontrolled aircraft of a kind of can launching a guided missile (spraying the fireworks big gun).
For realizing that the technical scheme that the utility model purpose is taked is:
A kind of telecontrolled aircraft with guided missile, comprise a telecontrolled aircraft body and flight control remote controller, the telecontrolled aircraft body is provided with flight control receiver, it is characterized in that: on the telecontrolled aircraft body, be provided with launch tube and electronic ignition head, be provided with the pyrotechnics ejectisome in launch tube, the rear portion of pyrotechnics ejectisome connects mutually with the electronic ignition head; The electronic ignition head is through electronic ignition control receiver and the wireless connections of electronic ignition remote controller.
Described ventral both sides at the telecontrolled aircraft body are provided with several launch tubes and electronic ignition head thereof, and each electronic ignition head is connected with electronic ignition control receiver respectively.
Described both sides at telecontrolled aircraft body ventral respectively are provided with three fixedly connected launch tube and electronic ignition heads thereof up and down.
Described bottom at telecontrolled aircraft body ventral is provided with three launch tubes that are mutually permanently connected and electronic ignition head thereof.
The rear end and the electronic ignition head of the pyrotechnics ejectisome in the described launch tube are fixedly connected, perhaps the rear end of pyrotechnics ejectisome light line and the electronic ignition head is fixedly connected, the electronic ignition head is fixed on the telecontrolled aircraft body or is located in the launch tube.
Described electronic ignition head is series connection or in parallel in electronic ignition control receiver.
Described flight control receiver and electronic ignition control receiver are the independent receiver or the integrated receiver of integration, and flight control remote controller and electronic ignition remote controller are the independent remote controller or the integrated remote control of integration.
The beneficial effects of the utility model are: the telecontrolled aircraft body can be launched " guided missile " and be rich in recreationally in flight course, " guided missile " can be one by one, by to or emission together.
Description of drawings:
Fig. 1 is the side view of embodiment of the present utility model;
Fig. 2 is the rearview of embodiment of the present utility model;
Fig. 3 is one of connected mode of pyrotechnics ejectisome and electronic ignition head;
Fig. 4 be pyrotechnics ejectisome and electronic ignition head connected mode two.
1, telecontrolled aircraft body; 2, launch tube; 3, electronic ignition head; 4, pyrotechnics ejectisome; 5, electronic ignition power line; 6, light line.
The specific embodiment:
Below in conjunction with drawings and Examples the utility model is described in further detail.
Among the embodiment as shown in Figure 1 and Figure 2, the utility model comprises a telecontrolled aircraft body 1 (helicopter) and flight control remote controller, on telecontrolled aircraft body 1, be provided with launch tube 2, flight control receiver and electronic ignition 3, be provided with three fixedly connected up and down launch tubes 2 and electronic ignition 3 in the both sides of telecontrolled aircraft body 1 ventral, be provided with three launch tubes that are mutually permanently connected 2 and electronic ignition 3 (seeing accompanying drawing 2) in the bottom of telecontrolled aircraft body 1 ventral.Each electronic ignition 3 is connected with electronic ignition control receiver respectively.Electronic ignition 3 is connected through electronic ignition power line 5 and electronic ignition control receiver.
In launch tube 2, be provided with pyrotechnics ejectisome 4, the rear portion of pyrotechnics ejectisome 4 and electronic ignition 3 connection mutually.Electronic ignition 3 is through electronic ignition control receiver and the wireless connections of electronic ignition remote controller.
The rear end of the pyrotechnics ejectisome 4 in the launch tube and electronic ignition 3 be fixedly connected (Fig. 4), perhaps line 6 and the electronic ignition 3 of lighting of pyrotechnics ejectisome 4 rear ends is fixedly connected (Fig. 3), and electronic ignition 3 is fixed on the telecontrolled aircraft body or is located in the launch tube.What pyrotechnics ejectisome 4 can be directly lighted in electronic ignition 3 lights line 6, also can light the thrust gunpowder in the pyrotechnics ejectisome 4.
" guided missile " is pyrotechnics ejectisome 4 or sprays the fireworks big gun and light through electronic ignition 3 that " guided missile " just launched." guided missile " can be launched one by one or by to emission, also can launch together.Electronic ignition 3 is series connection or in parallel in electronic ignition control receiver.
Flight control receiver and electronic ignition control receiver are the independent receiver or the integrated receiver of integration, and flight control remote controller and electronic ignition remote controller are the independent remote controller or the integrated remote control of integration
What the pyrotechnics ejectisome comprised anterior bullet and rear portion propels nitre (gunpowder), " guided missile " can launch how far depend on propel nitre how much; Do not have when lighting line, the electronic ignition head with propel nitre and contact and fix.
Claims (7)
1, a kind of telecontrolled aircraft with guided missile, comprise a telecontrolled aircraft body and flight control remote controller, the telecontrolled aircraft body is provided with flight control receiver, it is characterized in that: on the telecontrolled aircraft body, be provided with launch tube and electronic ignition head, be provided with the pyrotechnics ejectisome in launch tube, the rear portion of pyrotechnics ejectisome connects mutually with the electronic ignition head; The electronic ignition head is through electronic ignition control receiver and the wireless connections of electronic ignition remote controller.
2, a kind of telecontrolled aircraft with guided missile according to claim 1 is characterized by: be provided with several launch tubes and electronic ignition head thereof in the ventral both sides of telecontrolled aircraft body, each electronic ignition head is connected with electronic ignition control receiver respectively.
3, a kind of telecontrolled aircraft with guided missile according to claim 2 is characterized by: respectively be provided with three fixedly connected launch tube and electronic ignition heads thereof up and down in the both sides of telecontrolled aircraft body ventral.
4, a kind of telecontrolled aircraft with guided missile according to claim 1 is characterized by: be provided with three launch tubes that are mutually permanently connected and electronic ignition head thereof in the bottom of telecontrolled aircraft body ventral.
5, a kind of telecontrolled aircraft according to claim 1 with guided missile, it is characterized by: the rear end and the electronic ignition head of the pyrotechnics ejectisome in the launch tube are fixedly connected, perhaps the rear end of pyrotechnics ejectisome light line and the electronic ignition head is fixedly connected, the electronic ignition head is fixed on the telecontrolled aircraft body or is located in the launch tube.
6, a kind of telecontrolled aircraft with guided missile according to claim 1 is characterized by: the electronic ignition head is series connection or in parallel in electronic ignition control receiver.
7, a kind of telecontrolled aircraft according to claim 1 with guided missile, it is characterized by: flight control receiver and electronic ignition control receiver are the independent receiver or the integrated receiver of integration, and flight control remote controller and electronic ignition remote controller are the independent remote controller or the integrated remote control of integration.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2009200038535U CN201350344Y (en) | 2009-02-11 | 2009-02-11 | Telecontrolled aircraft with missiles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2009200038535U CN201350344Y (en) | 2009-02-11 | 2009-02-11 | Telecontrolled aircraft with missiles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201350344Y true CN201350344Y (en) | 2009-11-25 |
Family
ID=41373732
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2009200038535U Expired - Fee Related CN201350344Y (en) | 2009-02-11 | 2009-02-11 | Telecontrolled aircraft with missiles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201350344Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101898637A (en) * | 2010-06-17 | 2010-12-01 | 河海大学 | Method for simulating chemical fireworks by utilizing aircraft to release electronic fireworks |
| CN107376359A (en) * | 2017-03-31 | 2017-11-24 | 泉州鹰击长空遥控科技有限公司 | A kind of remote controlled games system |
-
2009
- 2009-02-11 CN CNU2009200038535U patent/CN201350344Y/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101898637A (en) * | 2010-06-17 | 2010-12-01 | 河海大学 | Method for simulating chemical fireworks by utilizing aircraft to release electronic fireworks |
| CN107376359A (en) * | 2017-03-31 | 2017-11-24 | 泉州鹰击长空遥控科技有限公司 | A kind of remote controlled games system |
| CN107441713A (en) * | 2017-03-31 | 2017-12-08 | 泉州鹰击长空遥控科技有限公司 | A kind of remote control system that can be achieved precisely to shoot |
| CN107441712A (en) * | 2017-03-31 | 2017-12-08 | 泉州鹰击长空遥控科技有限公司 | A kind of telecontrolled aircraft |
| CN107441712B (en) * | 2017-03-31 | 2020-09-22 | 黄巧香 | Remote control airplane |
| CN107441713B (en) * | 2017-03-31 | 2020-09-22 | 黄巧香 | Remote control system capable of realizing accurate shooting |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101726219B (en) | Multielement seeding combustion explosion type rainfall-increasing and anti-hail rocket | |
| WO2002032762A3 (en) | Artillery launched flyer assembly | |
| CN107441712B (en) | Remote control airplane | |
| CN201350344Y (en) | Telecontrolled aircraft with missiles | |
| CN111038699B (en) | Separable composite range extending system and method on aircraft | |
| CN209147840U (en) | A kind of normal arrangement individual soldier hand-thrown type scout missile | |
| CN202947541U (en) | Hand grenade with boosting devices | |
| CN115649500A (en) | Folding many rotor unmanned aerial vehicle | |
| JP2005509834A (en) | Weapon platform configuration | |
| CN205561674U (en) | Rocket dummy round of laying mines | |
| CN200984454Y (en) | Remote controlled toy aircraft for battling | |
| CN204891199U (en) | Simulation architecture and toy | |
| CN201921503U (en) | Remote control combat attack helicopter | |
| CN202155043U (en) | Aviation model plane provided with launchers | |
| CN201752579U (en) | Combat toy tank | |
| CN202315300U (en) | Wireless remote control model combat vehicle capable of emitting ammunitions | |
| CN201941977U (en) | Attack system for small-sized police unmanned aerial vehicle | |
| CN109323633B (en) | Single-soldier hand-thrown type fly-round projectile with conventional layout | |
| CN201184774Y (en) | Cannonball capable of being used as glider | |
| CN218515076U (en) | Air bubble agricultural plant protection system based on unmanned vehicle | |
| CN101078611A (en) | Streamlined gun (shell) bullet | |
| CN2662190Y (en) | Airborne rain increasing flame bomb and emitter therefor | |
| CN216222921U (en) | Multifunctional toy water bullet car | |
| CN214148988U (en) | Electric soft bullet gun with acousto-optic smoke | |
| CN216536904U (en) | Multifunctional toy gun |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091125 Termination date: 20120211 |