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Aircraft with wings capable of rotating integrally

A wing and integral technology, applied in the field of aircraft, can solve the problems of fixed wing angle and inability to adjust the wing angle, and achieve the effect of uniform comfort

Pending Publication Date: 2019-11-15
刘忠革
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The angle of the wing of the existing aircraft is fixed, and the angle of the wing itself cannot be adjusted according to the actual flight situation

Method used

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  • Aircraft with wings capable of rotating integrally
  • Aircraft with wings capable of rotating integrally
  • Aircraft with wings capable of rotating integrally

Examples

Experimental program
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Effect test

Embodiment 1

[0028] see Figure 1~5 , in an embodiment of the present invention, a kind of aircraft with integrally rotatable wings includes a fuselage 1, a wing 2, a braking mechanism 1, a power mechanism and a mounting groove 16, and the head of the fuselage 1 is symmetrically installed with Balance canard 2, balance canard 2 helps to improve the balance of aircraft when flying, fuselage 1 upper end middle part offers installation groove 16, installs wing 3 and power mechanism 14 in the installation groove 16, and power mechanism 14 drives engine The wing 3 rotates, and the rotation angle is less than or equal to 90 degrees (the rotation angle of the wing 3 is the attached Figure 4 middle rotation angle a);

[0029] Described power mechanism 14 comprises power motor one 8 and power gear 9, and power motor one 8 is a biaxial motor, and power gear 9 is all installed on the two motor shafts of power motor one 8, and biaxial motor drives two power gears simultaneously 9 rotation, symmetri...

Embodiment 2

[0039] Such as Image 6 As shown, the difference between this embodiment and Embodiment 1 is that: the inner, front and rear sides of the wing 3 are equipped with two rotating shafts 17, and the two rotating shafts 17 are installed in the rotating shaft seat 11, and the two rotating shafts The shaft two 17 is connected on the motor shaft of the power motor two 19, and the power motor two 19 is a biaxial motor, and the rotating shaft two 17 is provided with a fixed gear two 18, and the body 1 corresponds to two fixed gears two 18 The positions are equipped with braking mechanism two 20, and the braking mechanism two 20 has the same structure as the braking mechanism one.

[0040] When working, the power motor 2 19 works to drive the rotating shaft 2 17 to rotate, and the rotating shaft 2 17 rotates in the rotating shaft seat 11, and the rotating shaft 2 17 can drive the wing 3 to change from a horizontal state to an inclined state, so as to realize the 3 Angle rotation, the br...

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Abstract

The invention discloses an aircraft with wings capable of rotating integrally. The aircraft comprises a fuselage, the wings, a power mechanism and a mounting groove; the head of the fuselage is front-rear symmetrically provided with balance canards, the middle part of the upper end of the fuselage is provided with the mounting groove, and the wings and the power mechanism are installed in the mounting groove; the power mechanism includes a first power motor and a power gear, and the first power motor is a double shaft motor, and two motor shafts of the first power motor are correspondingly provided with power gears; and the inner parts of the wings are provided with a first rotating shaft, the front and rear sides of the first rotating shaft are correspondingly provided with rotating shaftseats in a sleeving mode, and the middle position of the first rotating shaft is provided with a first fixed gear. According to the aircraft with wings capable of rotating integrally, the adjustmentof the wing angle during taking-off, flight and landing can be achieved through structural parts such as the power mechanism, the first rotating shaft, the rotating shaft seats and a first brake mechanism, so that the aircraft can realize vertical taking-off and landing, and at the same time, the aircraft can take off at the most economical and reasonable wing angle so as to realize the unity of safety, stability, economy and comfort level.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an aircraft with integrally rotatable wings. Background technique [0002] Aircraft refers to a heavier-than-air aircraft that has one or more engines to generate forward thrust or pull, the wings of the fuselage to generate lift, and fly in the atmosphere. The airplane is one of the most important inventions in the early 20th century, and it is generally recognized that it was invented by the Wright brothers of the Americans. Their flight on December 17, 1903 was recognized by the Federation of International Aeronautics (FAI) as "the first controlled sustained powered flight by a heavier-than-air aircraft", and in the same year they founded the Wright Aircraft Company . Since the invention of the airplane, the airplane has increasingly become an indispensable tool of modern civilization. It has profoundly changed and influenced people's lives, and opened the history of peopl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/38
CPCB64C3/385
Inventor 刘忠革
Owner 刘忠革
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