CN221998862U - Fixed-wing model aircraft - Google Patents

Abstract

The utility model discloses a fixed-wing model aircraft, which relates to the technical field of model aircraft, and comprises a nose and a fuselage. The nose is fixed at the front end of the fuselage, the nose comprises a plurality of front ring beams, the interiors of the plurality of front ring beams are connected through front fuselage carbon tubes, the exteriors of the plurality of front ring beams are fixed through front wing ribs, the fuselage comprises a plurality of rear ring beams, the interiors of the plurality of rear ring beams are connected through rear fuselage carbon tubes, the exteriors of the plurality of rear ring beams are fixed through rear wing ribs, wings are arranged on both sides of the fuselage, and a tail is arranged at the rear end of the fuselage. The structure is more stable, more lightweight, and more durable. The overall structure is spliced, which is faster and more secure during assembly.

Description

Fixed wing model aeroplane and model ship aircraft

Technical Field

The utility model relates to the technical field of model aircraft, in particular to a fixed wing model aircraft.

Background

Along with innovation and development of science and technology, model aircraft are also updated, and the model aircraft is a model which simulates a real aircraft as the name implies, so that the model aircraft not only simulates the real aircraft in appearance, but also has internal structure and principle, the model aircraft is not only a simple model or toy, and the model aircraft embodies the technical achievement of the real aircraft to a certain extent.

The model airplane is popular with children and even adults due to excellent interestingness and entertainment. The patent application with the bulletin number of CN205738059U is authorized, a variable wing model aircraft is disclosed, which comprises a wing, a fuselage, a nose, a signal transmitting module, a power supply module and a microprocessor, the wing mounting plate is installed on the left side and the right side of the fuselage, the wing is installed on the wing mounting plate, a wing support is installed below the wing, the wing is movably connected with the wing support through a wing bearing rod, a telescopic link is installed below the wing support, a propeller is installed on the nose, a vertical tail wing and a horizontal tail wing are installed at the tail part of the fuselage, the output end of the signal transmitting module is electrically connected with the input end of the signal receiving module, the output end of the microprocessor is electrically connected with the input end of the power output module, and the power supply module is electrically connected with the microprocessor.

However, the common model aircraft on the market can normally fly, but the model aircraft has unstable structure and low durability, and is not satisfactory.

Disclosure of utility model

In order to overcome the defects of unstable structure and low durability of the model airplane aircraft in the prior art, the utility model provides the fixed wing model airplane which is more stable in structure, lighter and more convenient and has higher durability.

The technical scheme adopted for solving the technical problems is as follows: the utility model provides a fixed wing model aeroplane and model ship aircraft, includes aircraft nose and fuselage, and the aircraft nose is fixed at the front end of fuselage, and the aircraft nose includes the preceding collar tie beam of a plurality of, and the inside of collar tie beam is connected through preceding fuselage carbon tube before the plurality of, and the outside of collar tie beam is fixed through preceding rib before the plurality of, and the fuselage includes the collar tie beam after a plurality of, and the inside of collar tie beam after through back fuselage carbon tube connection after a plurality of, the outside of collar tie beam after a plurality of is fixed through back rib, and the both sides of fuselage all are equipped with the wing, and the rear end of fuselage is equipped with the fin.

As a further improvement of the utility model, the front frame carbon tube is fixedly connected with the rear ring beam, and the rear frame carbon tube is fixedly connected with the front ring beam.

As a further improvement of the utility model, the front end of the machine head is provided with a nozzle frame.

As a further development of the utility model, the wing comprises a spar, on which the wing is mounted.

As a further development of the utility model, the front end of the wing is provided with a propeller.

As a further development of the utility model, the underside of the tail is provided with a tail.

Compared with the prior art, the utility model has the beneficial effects that: in this scheme, the aircraft nose includes the front ring roof beam of a plurality of, and the inside of ring roof beam is connected through preceding fuselage carbon tube before the front ring roof beam of a plurality of, and the outside of ring roof beam is fixed through preceding rib before the front ring roof beam of a plurality of, and the fuselage includes the back ring roof beam of a plurality of, and the inside fuselage carbon tube connection after through of back ring roof beam, the outside of ring roof beam is fixed through back rib after the back of a plurality of, and its structure is more stable, and is lighter, and the durable degree is also higher, and overall structure uses the mode of concatenation, and is more swift when the assembly, more firm.

Drawings

The utility model is further described below with reference to the drawings and the detailed description.

FIG. 1 is a schematic structural view of a fixed wing aircraft of the present utility model.

In the figure: 1. a machine head; 2. a body; 3. a front ring beam; 4. a front fuselage carbon tube; 5. front wing rib tube; 6. a rear ring beam; 7. a rear fuselage carbon tube; 8. rear ribs; 9. a wing; 10. a tail wing; 11. a mouth frame; 12. a spar; 13. wings; 14. a propeller; 15. tail.

Detailed Description

In order that the technical scheme and the beneficial effects of the utility model become more apparent, the utility model is further described in detail below with reference to specific embodiments.

Referring to fig. 1, the embodiment of the utility model discloses a fixed wing model aircraft, which comprises a nose 1 and a fuselage 2, wherein the nose 1 is fixed at the front end of the fuselage 2, the nose 1 comprises a plurality of front ring beams 3, the interiors of the plurality of front ring beams 3 are connected through a front fuselage carbon tube 4, the exteriors of the plurality of front ring beams 3 are fixed through a front wing rib 5, the fuselage 2 comprises a plurality of rear ring beams 6, the interiors of the plurality of rear ring beams 6 are connected through a rear fuselage carbon tube 7, the exteriors of the plurality of rear ring beams 6 are fixed through rear wing ribs 8, wings 9 are arranged on two sides of the fuselage 2, the wings 9 comprise wing beams 12, and wings 13 are arranged on the wing beams 12. The front end of the wing 9 is provided with a propeller 14. The rear end of the fuselage 2 is provided with a tail 10.

Wherein, the front end of aircraft nose 1 is equipped with mouth frame 11, and the downside of fin 10 is equipped with tail 15, improves stable in structure, reinforcing flight stability, increases aesthetic feeling.

The fixed wing model aeroplane and model ship aircraft includes aircraft nose 1, fuselage 2, wing 9 and fin 10, adopts the profile modeling design, and overall structure is fixed wing structure, and aircraft nose 1 includes circle roof beam 3 before the several, and the inside of circle roof beam 3 is passed through preceding fuselage carbon tube 4 and is connected, and the outside of circle roof beam 3 is fixed through preceding wing rib 5 before the several, and fuselage 2 includes that circle roof beam 6 after the several, the inside of circle roof beam 6 is connected through back fuselage carbon tube 7 after the several, and the outside of circle roof beam 6 is fixed through back wing rib 8 after the several, and circle roof beam 6 after the preceding fuselage carbon tube 4 fixed connection, circle roof beam 3 before the back fuselage carbon tube 7 fixed connection. Adopt 3mm carbon fiber board to assemble the concatenation to make, its structure is more stable, and is lighter, and degree of durability is also higher, and overall structure uses the mode of concatenation, and is more swift when the assembly, more firm.

The fixed wing model aircraft adopts the principle of motor differential control, is simpler in operation and is easy to use. The 5010 disc type power motor is adopted, the power is stronger, the output power is more stable, and therefore the flying attitude is more stable. Through the form of combining science and technology and art, not only brings people with a sense of beauty, but also shows people with a sense of science and technology and future sense of life.

It should be understood that the detailed description is presented for purposes of understanding only and is not intended to limit the utility model to all other embodiments that may be obtained by one skilled in the art without making any inventive effort.

Claims (6)

1. The utility model provides a fixed wing model aeroplane and model ship aircraft which characterized in that: including aircraft nose (1) and fuselage (2), aircraft nose (1) is fixed in the front end of fuselage (2), aircraft nose (1) include that the inside of circle roof beam (3) is connected through preceding fuselage carbon tube (4) before a plurality of, the outside of circle roof beam (3) is fixed through preceding wing rib (5), fuselage (2) include that circle roof beam (6) after a plurality of, the inside is connected through back fuselage carbon tube (7) after a plurality of circle roof beam (6), the outside of circle roof beam (6) is fixed through back wing rib (8) after a plurality of, both sides of fuselage (2) all are equipped with wing (9), the rear end of fuselage (2) is equipped with fin (10).

2. A fixed wing aircraft as claimed in claim 1, wherein: the front frame carbon tube (4) is fixedly connected with the rear ring beam (6), and the rear frame carbon tube (7) is fixedly connected with the front ring beam (3).

3. A fixed wing aircraft as claimed in claim 2, wherein: the front end of the machine head (1) is provided with a nozzle frame (11).

4. A fixed wing aircraft as claimed in claim 3, wherein: the wing (9) comprises a wing spar (12), and the wing (13) is arranged on the wing spar (12).

5. A fixed wing aircraft as claimed in claim 4, wherein: the front end of the wing (9) is provided with a propeller (14).

6. A fixed wing aircraft as claimed in claim 5, wherein: the tail (15) is arranged at the lower side of the tail wing (10).