CN211435086U - Novel power model airplane - Google Patents
Novel power model airplane Download PDFInfo
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- CN211435086U CN211435086U CN201922272346.8U CN201922272346U CN211435086U CN 211435086 U CN211435086 U CN 211435086U CN 201922272346 U CN201922272346 U CN 201922272346U CN 211435086 U CN211435086 U CN 211435086U
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Abstract
The utility model discloses a novel power model aeroplane and model ship, include: the unmanned aerial vehicle comprises an unmanned aerial vehicle chassis and two first connecting pieces arranged on the lower surface of the unmanned aerial vehicle chassis; the shock absorber is arranged below the first connecting piece, and the first connecting piece is in threaded connection with one end of the shock absorber through a bolt; the second connecting piece is arranged below the shock absorber and is in threaded connection with the other end of the shock absorber through a bolt; and the three-way joint is arranged below the second connecting piece, and one end of the second connecting piece extends to the inside of the three-way joint. The landing gear can absorb part of impact by the aid of the shock absorber in a landing process, so that a buffering effect is achieved, and the service life of the landing gear is prolonged.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to novel power model aeroplane and model ship.
Background
The model airplane is generally the same as a manned airplane and mainly comprises six parts, namely wings, an empennage, a fuselage, an undercarriage, an engine and a control system. The wing-is a device for generating lift force when the model airplane flies, and can keep the lateral stability when the model airplane flies. The model airplane comprises 12 models and tail wings, wherein each tail wing comprises a horizontal tail wing and a vertical tail wing. The horizontal tail wing can keep the pitching stability of the model airplane during flying, and the vertical tail wing can keep the direction stability of the model airplane during flying. The elevator on the horizontal tail wing can control the elevation of the model airplane, and the rudder on the vertical tail wing can control the flight direction of the model airplane. There are also model airplanes that use V-fins and require hybrid control. However, the existing novel power model airplane has larger wings, so that the wings are very easy to damage under the condition of not using.
The first fuselage wing mechanism can enable the second fuselage wing mechanism to be stored, and when the equipment is used, the second fuselage wing mechanism extends out of the first fuselage wing mechanism, so that if the original integral wing can be split into two specific telescopic wings, the service life of the wing is prolonged, and the equipment has profound significance.
SUMMERY OF THE UTILITY MODEL
It is an object of the present invention to solve at least the above problems and to provide at least the advantages which will be described later.
The utility model discloses still another purpose provides novel power model aeroplane and model ship, becomes the wing of two concrete flexible functions with original holistic wing split to the life of extension wing.
In order to achieve the above and other objects, the present invention adopts the following technical solutions:
novel power model aeroplane and model ship includes:
the aircraft nose protection cover is arranged at one end of the upper main body of the model airplane;
the first body wing mechanisms are arranged on the front end surface and the rear end surface of the upper main body of the model airplane, and the two first body wing mechanisms are fixedly connected with the front end surface and the rear end surface of the upper main body of the model airplane;
the two second fuselage wing mechanisms are arranged on one side of the first fuselage wing mechanism and are connected with the two first fuselage wing mechanisms in a sliding manner;
and the three-way joint is arranged below the second connecting piece, and one end of the second connecting piece extends to the inside of the three-way joint.
Preferably, in the novel power model airplane, an instrument cabin is arranged above the upper main body of the model airplane, and a support fixing part is arranged below the upper main body of the model airplane.
Preferably, in the novel power model airplane, a connecting rod is arranged below the bracket fixing piece, a first bracket pulley mechanism is arranged at one end of the connecting rod, two first bracket pulley mechanisms are arranged at the other end of the connecting rod, and two second bracket pulley mechanisms are arranged at the other end of the connecting rod.
Preferably, novel power model airplane in, the other end of main part is provided with main part under the model airplane on the model airplane, one side of main part is provided with perpendicular fin mechanism under the model airplane, the one end of perpendicular fin mechanism is provided with adjusts the fuselage fin, all be provided with fixed external member under the model airplane on the preceding terminal surface of main part and perpendicular fin mechanism and the rear end face, and fixed external member is provided with two, the below of fixed external member is provided with horizontal fin mechanism, and horizontal fin mechanism is provided with two, the both sides of main part below are provided with light emitting lamp area mechanism under the model airplane.
Preferably, the novel power model airplane in, the below of main part is provided with the power safety cover under the model airplane, the one end of power safety cover is provided with the air inlet, the other end of power safety cover is provided with jet-propelled export, the below of power safety cover is provided with third support pulley mechanism.
Preferably, novel power model aeroplane and model ship in, two one side of second fuselage wing mechanism all is provided with outer aileron, and outer aileron is provided with two, the inside of main part is provided with overhauls the region on the model aeroplane and model ship, one side of overhauing the region is provided with first inner chamber, the inside weather detection device that is provided with of first inner chamber, the opposite side of overhauing the region is provided with the oil tank, the below of oil tank is provided with the air inlet pipeline, one side of air inlet pipeline is provided with engine mechanism, one side of engine mechanism is provided with jet-propelled outlet pipeline, the top of engine mechanism is provided with controller mechanism, controller mechanism passes through signal line and adjusts fuselage fin fixed connection.
The utility model discloses at least, include following beneficial effect:
the utility model discloses an among the novel power model aeroplane and model ship, through setting original whole wing into first fuselage wing mechanism and second fuselage wing mechanism, through letting first fuselage wing mechanism and second fuselage wing mechanism sliding connection to when not using this model aeroplane and model ship, can effectively protect the wing with the inside of second fuselage wing mechanism indentation first fuselage wing mechanism.
Through the fixed external member that sets up, let under the model aeroplane and model ship main part and vertical tail wing mechanism can reduce the probability that drops, because of vertical tail wing mechanism and model aeroplane and model ship lower part main part be perpendicular connection and lack protection device in traditional model aeroplane and model ship tail wing structure, easily with vertical tail wing mechanism carelessly break down in the operation.
Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention.
Drawings
Fig. 1 is a schematic structural view of a novel power model airplane provided by the present invention;
fig. 2 is a schematic view of a novel power model airplane in a top view structure;
fig. 3 is a schematic view of the side internal structure of the novel power model airplane.
Detailed Description
The present invention is described in detail below with reference to the attached drawings so that those skilled in the art can implement the invention by referring to the description.
As shown in fig. 1-3, the novel power model airplane comprises: the aircraft model upper main body 1 and the aircraft nose protection cover 2 are arranged at one end of the aircraft model upper main body 1.
And the first body wing mechanisms 24 are arranged on the front end surface and the rear end surface of the upper body 1 of the model airplane, two first body wing mechanisms 24 are arranged, and the two first body wing mechanisms 24 are fixedly connected with the front end surface and the rear end surface of the upper body 1 of the model airplane.
And the second fuselage wing mechanisms 25 are arranged on one side of the first fuselage wing mechanisms 24, and the number of the second fuselage wing mechanisms 25 is two, and the two second fuselage wing mechanisms 25 are connected with the two first fuselage wing mechanisms 23 in a sliding manner.
And four spoiler mechanisms 26 are arranged on the upper surfaces of the first fuselage wing mechanism 24 and the second fuselage wing mechanism 25, and the spoiler mechanisms 26 are fixedly connected with the upper surfaces of the first fuselage wing mechanism 24 and the second fuselage wing mechanism 25.
In the scheme, the front end surface and the rear end surface of the upper main body of the model airplane are respectively provided with the first body wing mechanism through the arrangement of the upper main body of the model airplane, the second body wing mechanism is in sliding connection with the first body wing mechanism, the second body wing mechanism can be retracted into the first body wing mechanism when the model airplane is not used, and can be extended out from the first body wing mechanism when the model airplane is used, so that the space volume can be effectively reduced, the maximum protection can be realized when the model airplane is not used at ordinary times, the arranged spoiler mechanism plays an auxiliary role when the model airplane ascends or descends, the air physics is utilized to the maximum, and the use of fuel is reduced to the maximum.
In a preferable scheme, an instrument cabin 4 is arranged above the model airplane upper main body 1, and a bracket fixing part 5 is arranged below the model airplane upper main body 1.
In the above-mentioned scheme, through the instrument storehouse that is provided with, can all conclude in an area by effectual instrument and the small-size part with a series of equipment to can be when overhauing, the staff just can overhaul most equipment at this instrument storehouse.
In a preferred scheme, a connecting rod 8 is arranged below the bracket fixing part 5, a first bracket pulley mechanism 6 is arranged at one end of the connecting rod 8, two first bracket pulley mechanisms 6 are arranged at the other end of the connecting rod 8, a second bracket pulley mechanism 7 is arranged at the other end of the connecting rod 8, and two second bracket pulley mechanisms 7 are arranged at the other end of the connecting rod.
In the scheme, the first support pulley mechanism and the second support pulley mechanism which are arranged through the connecting rod enable the model airplane equipment to slide when not in use, so that the model airplane equipment can be effectively protected.
In a preferred scheme, the other end of the model airplane upper main body 1 is provided with a model airplane lower main body 3, one side of the model airplane lower main body 3 is provided with a vertical tail wing mechanism 23, one end of the vertical tail wing mechanism 23 is provided with an adjusting fuselage tail wing 10, the front end surface and the rear end surface of the model airplane lower main body 3 and the vertical tail wing mechanism 23 are respectively provided with two fixing external members 11, a horizontal tail wing mechanism 12 is arranged below the fixing external members 11, the horizontal tail wing mechanisms 12 are arranged in two, and light-emitting lamp strip mechanisms 28 are arranged on two sides below the model airplane lower main body 3.
In the scheme, the lower body and the vertical tail wing mechanism of the model airplane can reduce the falling probability through the arranged fixing sleeve, and the vertical tail wing mechanism is easily carelessly broken in the operation process because the vertical tail wing mechanism is vertically connected with the lower body of the model airplane and lacks a protection device in the traditional model airplane tail wing structure.
In a preferable scheme, a power generation protective cover 13 is arranged below the model airplane lower main body 3, an air inlet 14 is arranged at one end of the power generation protective cover 13, an air outlet 15 is arranged at the other end of the power generation protective cover 13, and a third support pulley mechanism 9 is arranged below the power generation protective cover 13.
In the scheme, the air inlet is arranged to provide continuous assistance to oxygen in air when the model airplane works under the power generation.
In a preferred scheme, two one side of second fuselage wing mechanism 25 all is provided with outer aileron 27, and outer aileron 27 is provided with two, the inside of main part 1 is provided with overhauls regional 16 on the model aeroplane and model ship, one side of overhauing regional 16 is provided with first inner chamber 17, the inside weather detection device 18 that is provided with of first inner chamber 17, the opposite side of overhauing regional 16 is provided with oil tank 29, the below of oil tank 29 is provided with air inlet pipeline 19, one side of air inlet pipeline 19 is provided with engine mechanism 21, one side of engine mechanism 21 is provided with jet-propelled outlet pipeline 20, the top of engine mechanism 21 is provided with controller mechanism 22, controller mechanism 22 passes through signal line 30 and adjusts fuselage fin 10 fixed connection.
In the scheme, the fixed maintenance window is arranged in the maintenance area, and parts inside the instrument bin can be maintained through the maintenance window.
While the embodiments of the invention have been described above, it is not intended to be limited to the details shown, or described, but rather to cover all modifications, which would come within the scope of the invention, as defined by the claims and the equivalents thereof, and which fall within the limits of the claims and the equivalents thereof.
Claims (6)
1. Novel power model aeroplane and model ship, its characterized in that includes:
the aircraft nose protection cover is arranged at one end of the upper main body of the model airplane;
the first body wing mechanisms are arranged on the front end surface and the rear end surface of the upper main body of the model airplane, and the two first body wing mechanisms are fixedly connected with the front end surface and the rear end surface of the upper main body of the model airplane;
the two second fuselage wing mechanisms are arranged on one side of the first fuselage wing mechanism and are connected with the two first fuselage wing mechanisms in a sliding manner;
and four spoiler mechanisms are arranged on the upper surfaces of the first fuselage wing mechanism and the second fuselage wing mechanism, and are fixedly connected with the upper surfaces of the first fuselage wing mechanism and the second fuselage wing mechanism.
2. The novel power model airplane as claimed in claim 1, wherein an instrument cabin is arranged above the upper main body of the model airplane, and a bracket fixing piece is arranged below the upper main body of the model airplane.
3. The novel power model airplane as claimed in claim 2, wherein a connecting rod is disposed below said bracket fixing member, a first bracket pulley mechanism is disposed at one end of said connecting rod, and said first bracket pulley mechanism is disposed in two, a second bracket pulley mechanism is disposed at the other end of said connecting rod, and said second bracket pulley mechanism is disposed in two.
4. The novel power model airplane as claimed in claim 1, wherein the other end of the upper model airplane body is provided with a lower model airplane body, one side of the lower model airplane body is provided with a vertical tail mechanism, one end of the vertical tail mechanism is provided with an adjusting fuselage tail, the front end face and the rear end face of the lower model airplane body and the vertical tail mechanism are both provided with two fixing external members, the lower part of the fixing external member is provided with a horizontal tail mechanism, the lower part of the horizontal tail mechanism is provided with two light-emitting strip mechanisms, and the two sides of the lower model airplane body are provided with light-emitting strip mechanisms.
5. The novel power model airplane as claimed in claim 4, wherein a power generating protective cover is arranged below the model airplane lower main body, an air inlet is arranged at one end of the power generating protective cover, an air outlet is arranged at the other end of the power generating protective cover, and a third support pulley mechanism is arranged below the power generating protective cover.
6. The novel power model airplane as claimed in claim 1, wherein two outer ailerons are arranged on one side of each of the two second fuselage wing mechanisms, and two outer ailerons are arranged on each of the two second fuselage wing mechanisms, an overhaul region is arranged inside the upper main body of the model airplane, a first inner cavity is arranged on one side of the overhaul region, a weather detection device is arranged inside the first inner cavity, an oil tank is arranged on the other side of the overhaul region, an air inlet pipeline is arranged below the oil tank, an engine mechanism is arranged on one side of the air inlet pipeline, an air jet outlet pipeline is arranged on one side of the engine mechanism, and a controller mechanism is arranged above the engine mechanism and is fixedly connected with an adjusting fuselage tail wing through a signal line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922272346.8U CN211435086U (en) | 2019-12-04 | 2019-12-04 | Novel power model airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922272346.8U CN211435086U (en) | 2019-12-04 | 2019-12-04 | Novel power model airplane |
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| Publication Number | Publication Date |
|---|---|
| CN211435086U true CN211435086U (en) | 2020-09-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922272346.8U Active CN211435086U (en) | 2019-12-04 | 2019-12-04 | Novel power model airplane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113304489A (en) * | 2021-07-05 | 2021-08-27 | 河北呆喵智能科技有限公司 | Model airplane fixed-wing aircraft for flight training and competition |
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2019
- 2019-12-04 CN CN201922272346.8U patent/CN211435086U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113304489A (en) * | 2021-07-05 | 2021-08-27 | 河北呆喵智能科技有限公司 | Model airplane fixed-wing aircraft for flight training and competition |
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