CN2564215Y - Electric remote-controlled model aircraft - Google Patents
Electric remote-controlled model aircraft Download PDFInfo
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- CN2564215Y CN2564215Y CN 02266024 CN02266024U CN2564215Y CN 2564215 Y CN2564215 Y CN 2564215Y CN 02266024 CN02266024 CN 02266024 CN 02266024 U CN02266024 U CN 02266024U CN 2564215 Y CN2564215 Y CN 2564215Y
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- fuselage
- fixed
- empennage
- remote control
- rudder face
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Abstract
The utility model discloses an electric remote-control model airplane, comprising an airframe (3), a main wing (5), a front wheel (24), an airframe fiber tube (7), a tail wing, a back wheel (23), a power device (6) and a remote control device. The main wing (5) is fixed on the airframe (3). The airframe fiber tube (7) is fixed on the airframe (3). The tail wing is fixed on the rear of the airframe fiber tube (7). The tail wing is composed of a left stabilizing plane (11), a right stabilizing plane (10), a left control surface (12) and a right control surface (13). The upper surfaces and the lower surfaces between the left stabilizing plane (11) and the left control surface (12), between the right stabilizing plane (10) and the right control surface (13) are adhered in flexible flake connection. The tail wing is V-shaped. Adopting the stabilizing planes of the tail wing are in fixed connection with the control surfaces and the control surfaces swing flexibly upwards and downwards. The stabilizing planes have the functions of vertical stabilizing and horizontal stabilizing. The control surfaces have the functions of rising and turning. The utility model has the advantages of simple structure, convenient control and operation, good flying performance, firm connection, good properties of anti-collision and wind resistance, thus the utility model is suitable for the beginners.
Description
One, technical field
The invention relates to a kind of model of an airplane, particularly a kind of electric remote control model of an airplane that can transmit and receive simulated aircraft flight by remote control.
Two, background technology
Along with the development of society and the progress of science, the development of model plane motion has received each personage's of society concern, and increasing teenager joins in the model plane cause.Existing electric remote control model of an airplane empennage generally is made up of tailplane and vertical tail, and wherein tailplane comprises horizontal stabilization and lifting rudder face, controlled by remote control and finishes lifting action; Vertical tail comprises vertical stabilization and steering vane, is subjected to remote control control to finish go to action; Its weak point one is that complex structure, installation accuracy require height, the difficult control of flight; The 2nd, single face is connected between stabilization and the rudder face, and the rudder face swing is dumb, connections is insecure, reseting performance is poor, very easily rupture.In addition, the measure of existing electric remote control model of an airplane fuselage head unprotect lands or causes that easily fuselage breaks when out of control; There are not windproof means, big, the flight instability of resistance etc. during flight yet.
Three, summary of the invention
To be connected insecure, rudder face between existing electric remote control model of an airplane tail structure complexity, stabilization and the rudder face and to swing disadvantage dumb, crashproof windproof poor performance in order to overcome, the invention provides between a kind of stabilization and the rudder face and is connected firmly, controls conveniently, and the electric remote control model of an airplane crashproof, windproof performance is arranged.The invention solves the technical scheme that its technical problem adopts and comprises fuselage, main wing, front-wheel, the fuselage fibre pipe, empennage, trailing wheel and power set and remote control, main wing is fixed on the fuselage by the wing rubber band, the fuselage fibre pipe is fixedlyed connected with afterbody, empennage is fixed on the afterbody of fuselage fibre pipe, remote control is made up of transmitter and receiver, receiver is fixed on the fuselage, empennage is by a left side, a right stabilization and a left side, the right standard rudder face is formed, and make by flexible foam film composite board, reach between right standard rudder face and the right stabilization between left rudder face and the left stabilization by heating, extruding is flexible coupling composite board upper surface and lower surface bonds flakiness, by a left side, the empennage that right stabilization constitutes becomes V font structure.
Fix left and right rocking arm on the left and right rudder face successively, the steering wheel that climbs on the receiver is connected with left and right rocking arm respectively by flexible cord, and the steering-engine on the receiver is connected with left and right rocking arm respectively by flexible cord.
Fuselage head is fixed with the metal head-shield, is fixed with the passenger cabin radome fairing on the position of fuselage passenger cabin.
Be fixed with main wing on the main wing and strengthen the carbon element pipe, the main wing both sides are fixed with main wing fixed angle sheet.
Be provided with the auxiliary reset rubber band on the left and right rocking arm in the back side of left and right rudder face, auxiliary reset rubber band one end is fixed on left rocking arm, and the other end is walked around the fuselage fibre pipe of empennage front and got back on the right rocking arm from the bottom of empennage from the bottom of empennage.After adopting said structure, the stabilization of empennage and the rudder face not easy fracture that is connected firmly, rudder face swings up and down flexibly and the reset function that has, empennage adopts V font empennage, the existing vertically stable laterally stable effect that has again of its stabilization, its rudder face not only can play and climb but also can play the effect that turns to, fuselage head adds the metal head-shield can prevent collision, add the passenger cabin radome fairing at the fuselage passenger cabin and can reduce flight resistance, have simple in structure, easy to operate, flying quality good, turn to and climb fast, use advantages such as firm, suitablely begin to learn the fan and use.
Four, description of drawings
Fig. 1 is the main TV structure schematic diagram of the invention.
Fig. 2 is the structural representation of looking up of the invention.
Tail structure schematic diagram when Fig. 3 climbs for the invention.
Fig. 4 is the local structure for amplifying schematic diagram of Fig. 3.
Tail structure schematic diagram when Fig. 5 turns left for the invention.
Fig. 6 is the local structure for amplifying schematic diagram of Fig. 5.
Tail structure schematic diagram when Fig. 7 turns right for the invention.
Fig. 8 is the local structure for amplifying schematic diagram of Fig. 7.
Fig. 9 is the right TV structure schematic diagram of the invention.
Five, the specific embodiment
Fig. 1, Fig. 2 and shown in Figure 9, specific embodiments for a kind of electric remote control model of an airplane of the invention, it comprises fuselage 3, main wing 5, front-wheel 24, fuselage fibre pipe 7, empennage, trailing wheel 23 and power set 6 and remote control, be fixed with main wing on the main wing 5 and strengthen carbon element pipe 17, main wing 5 both sides are fixed with main wing fixed angle sheet 19, main wing 5 is fixed on the gim peg 4 of fuselage 3 by wing rubber band 18, fuselage fibre pipe 7 is fixedlyed connected with fuselage 3 afterbodys, empennage is fixed on the afterbody of fuselage fibre pipe 7 by fixed screw 21 by empennage compressing tablet 16 and empennage support chip, power set 6 are installed on the fuselage 3, remote control is made up of ground transmitter and receiver 26, receiver 26 is installed in the fuselage 3, empennage is by a left side, right stabilization 11,10 and left, right standard rudder face 12,13 form, and make by flexible foam film composite board, reach between right standard rudder face 13 and the right stabilization 10 between left rudder face 12 and the left stabilization 11 by heating, extruding is flexible coupling composite board upper surface and lower surface bonds flakiness, makes the not easy fracture that is connected firmly between stabilization and the rudder face; The empennage that is made of left and right stabilization 11,10 becomes V font structure, makes that stabilization is existing vertically stablely to be had laterally stablely again, and rudder face not only can play and climb but also can play the effect that turns to; Fix left and right rocking arm 14,15 on the left and right rudder face 12,13 successively, the steering wheel 28 that climbs on the receiver 26 is connected with left and right rocking arm 14,15 respectively by flexible cord 9b, 8b, steering-engine 27 on the receiver 26 is connected with left and right rocking arm 14,15 respectively by flexible cord 9a, 8a, and rudder face is swung up and down flexibly.On the left and right rocking arm 14,15 in the back side of left and right rudder face 12,13, be provided with auxiliary reset rubber band 22, auxiliary reset rubber band 22 1 ends are fixed on left rocking arm 14, the other end is walked around the fuselage fibre pipe 7 of empennage front and is got back on the right rocking arm 15 from the bottom of empennage from the bottom of empennage, make empennage have reset function.In order to prevent that collision from causing damage, fuselage 3 heads are fixed with the metal head-shield 1 by stainless steel stretched moulding; In order to reduce flight resistance, improve flying speed, on the position of fuselage 3 passenger cabins, be fixed with passenger cabin radome fairing 2.
When the utility model uses, at first open switch 25, connect power supply, the electric remote control model of an airplane is in takeoff condition.After telecontrol transmitter sent the signal that takes off, receiver 26 received control signal, and power set 6 are started working, and the electric remote control model of an airplane is in off state.After reaching takeoff speed, telecontrol transmitter sends the signal that takes off, and receiver 26 receives control signal, the steering wheel 28 that climbs of receiver rotates to clockwise direction, flexible cord 9b, 8b are upwards drawn left and right rudder face 12,13, and the model of an airplane enters climb mode, as shown in Figure 3 and Figure 4; After the model of an airplane rose to certain height, telecontrol transmitter sent reset signal, and receiver 26 receives control signals, and right standard rudder face 12,13 is resetted, and kept concordant with right stabilization 10 with left stabilization 11, and the model of an airplane enters the straight and level flight state.When telecontrol transmitter sends the left-hand bend signal, receiver 26 receives control signal, the steering-engine 27 of receiver is to counterclockwise rotating, make flexible cord 8a pulling right standard rudder face 13 upwards, and unclamp flexible cord 9a, but left rudder face 12 held by flexible cord 9b, and its auxiliary reset rubber band 22 pulling force below empennage equate, and do not make left rudder face 12 and keep concordant downwards with left stabilization 11, as shown in Figure 5 and Figure 6; After telecontrol transmitter sent restoring signal, receiver 26 received control signal, and the steering-engine 27 of receiver recovers reset condition, and right standard rudder face 13 automatically resets.When telecontrol transmitter sends the right-hand bend signal, receiver 26 receives control signal, the steering-engine 27 of receiver rotates to clockwise direction, make flexible cord 9a pulling left rudder face 12 upwards, and unclamp flexible cord 8a, but right standard rudder face 13 held by flexible cord 8b, and its auxiliary reset rubber band 22 pulling force below empennage equate, and do not make right standard rudder face 13 and keep concordant downwards with left stabilization 10, as shown in Figure 7 and Figure 8; After telecontrol transmitter sent restoring signal, receiver 26 received control signal, and the steering-engine 27 of receiver recovers reset condition, and right standard rudder face 12 automatically resets.Thereby reach the model plane requirement of electric remote control simulated flight.
Claims (5)
1, a kind of electric remote control model of an airplane, comprise fuselage (3), main wing (5), front-wheel (24), fuselage fibre pipe (7), empennage, trailing wheel (23) and power set (6) and remote control, main wing (5) is fixed on the fuselage (3) by wing rubber band (18), fuselage fibre pipe (7) is fixedlyed connected with fuselage (3) afterbody, empennage is fixed on the afterbody of fuselage fibre pipe (7), remote control is made up of transmitter and receiver (26), receiver (26) is fixed on the fuselage (3), it is characterized in that: described empennage is by a left side, right stabilization (11,10) and a left side, right standard rudder face (12,13) form, and make by flexible foam film composite board, reach between right standard rudder face (13) and the right stabilization (10) between left rudder face (12) and the left stabilization (11) by heating, extruding is flexible coupling composite board upper surface and lower surface bonds flakiness, by a left side, right stabilization (11,10) empennage of Gou Chenging becomes V font structure.
2, the electric remote control model of an airplane according to claim 1, it is characterized in that: fix left and right rocking arm (14,15) on the described left and right rudder face (12,13) successively, the steering wheel that climbs (28) on the receiver (26) is connected with left and right rocking arm (14,15) respectively by flexible cord (9b, 8b), and the steering-engine (27) on the receiver (26) is connected with left and right rocking arm (14,15) respectively by flexible cord (9a, 8a).
3, the electric remote control model of an airplane according to claim 1 and 2 is characterized in that: described fuselage (3) head is fixed with metal head-shield (1), is fixed with passenger cabin radome fairing (2) on the position of fuselage (3) passenger cabin.
4, the electric remote control model of an airplane according to claim 3 is characterized in that: be fixed with main wing on the described main wing (5) and strengthen carbon element pipe (17), main wing (5) both sides are fixed with main wing fixed angle sheet (19).
5, the electric remote control model of an airplane according to claim 4, it is characterized in that: on the left and right rocking arm in the back side (14,15) of left and right rudder face (12,13), be provided with auxiliary reset rubber band (22), auxiliary reset rubber band (22) one ends are fixed on left rocking arm (14), and the other end is walked around the fuselage fibre pipe (7) of empennage front and got back on the right rocking arm (15) from the bottom of empennage from the bottom of empennage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02266024 CN2564215Y (en) | 2002-07-31 | 2002-07-31 | Electric remote-controlled model aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02266024 CN2564215Y (en) | 2002-07-31 | 2002-07-31 | Electric remote-controlled model aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2564215Y true CN2564215Y (en) | 2003-08-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02266024 Expired - Fee Related CN2564215Y (en) | 2002-07-31 | 2002-07-31 | Electric remote-controlled model aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2564215Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103223249A (en) * | 2012-01-26 | 2013-07-31 | 潘佳辰 | Forced landing mechanism for self-wing-rotating rocket model in world championships |
| CN103723268A (en) * | 2013-11-05 | 2014-04-16 | 湖北易瓦特科技有限公司 | Unmanned aerial vehicle |
| CN114104264A (en) * | 2021-12-17 | 2022-03-01 | 江西洪都航空工业集团有限责任公司 | Control surface mounting structure |
-
2002
- 2002-07-31 CN CN 02266024 patent/CN2564215Y/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103223249A (en) * | 2012-01-26 | 2013-07-31 | 潘佳辰 | Forced landing mechanism for self-wing-rotating rocket model in world championships |
| CN103223249B (en) * | 2012-01-26 | 2015-07-01 | 潘佳辰 | Forced landing mechanism for self-wing-rotating rocket model in world championships |
| CN103723268A (en) * | 2013-11-05 | 2014-04-16 | 湖北易瓦特科技有限公司 | Unmanned aerial vehicle |
| CN103723268B (en) * | 2013-11-05 | 2016-06-29 | 湖北易瓦特科技股份有限公司 | A kind of unmanned aerial vehicle |
| CN114104264A (en) * | 2021-12-17 | 2022-03-01 | 江西洪都航空工业集团有限责任公司 | Control surface mounting structure |
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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: 20030806 Termination date: 20100731 |