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Solar energy and air energy composite aircraft

A composite aircraft and air energy technology, applied in the field of aircraft, can solve problems such as safety accidents, collisions between express aircraft and surrounding objects, and unstable flight of express aircraft

Active Publication Date: 2020-08-25
CHONGQING NORMAL UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a composite aircraft of solar energy and air energy, aiming at solving the inertial movement of the package caused by the express delivery aircraft in the prior art after the package is loaded by the connecting arm, taking off, turning, and emergency stop, etc. The flight of the courier aircraft is unstable, which may easily cause the courier aircraft to collide with surrounding objects, causing technical problems in safety accidents

Method used

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  • Solar energy and air energy composite aircraft
  • Solar energy and air energy composite aircraft
  • Solar energy and air energy composite aircraft

Examples

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no. 1 example

[0027] see figure 1 and figure 2, the present invention provides a composite aircraft 100 of solar energy and air energy, comprising a body 1, a connecting arm 2, a cargo box 3, a connecting arm shock absorbing device 4 and a body shock absorbing device 5; the connecting arm 2 and the body 1 is slidingly connected, and the number is multiple, respectively located on both sides of the body 1, the cargo box 3 cooperates with the connecting arm 2, and is located at the end of the connecting arm 2 away from the body 1, so The connecting arm damping device 4 is slidably connected to the body 1 and fixedly connected to the connecting arm 2, and is located between the body 1 and the connecting arm 2. The body shock absorbing device 5 is connected to the connecting arm 2. The body 1 is slidably connected and fixedly connected with the connecting arm shock absorbing device 4, and is located at the end of the body 1 away from the connecting arm 2; the connecting arm shock absorbing de...

no. 2 example

[0033] see Figure 1 to Figure 4 , the present invention provides a composite aircraft 100 of solar energy and air energy, comprising a body 1, a connecting arm 2, a cargo box 3, a connecting arm shock absorbing device 4 and a body shock absorbing device 5; the connecting arm 2 and the body 1 is slidingly connected, and the number is multiple, respectively located on both sides of the body 1, the cargo box 3 cooperates with the connecting arm 2, and is located at the end of the connecting arm 2 away from the body 1, so The connecting arm damping device 4 is slidably connected to the body 1 and fixedly connected to the connecting arm 2, and is located between the body 1 and the connecting arm 2. The body shock absorbing device 5 is connected to the connecting arm 2. The body 1 is slidably connected and fixedly connected with the connecting arm shock absorbing device 4, and is located at the end of the body 1 away from the connecting arm 2; the connecting arm shock absorbing dev...

no. 3 example

[0042] see figure 1 and figure 2 and Figure 5 , the present invention provides a composite aircraft 100 of solar energy and air energy, comprising a body 1, a connecting arm 2, a cargo box 3, a connecting arm shock absorbing device 4 and a body shock absorbing device 5; the connecting arm 2 and the body 1 is slidingly connected, and the number is multiple, respectively located on both sides of the body 1, the cargo box 3 cooperates with the connecting arm 2, and is located at the end of the connecting arm 2 away from the body 1, so The connecting arm damping device 4 is slidably connected to the body 1 and fixedly connected to the connecting arm 2, and is located between the body 1 and the connecting arm 2. The body shock absorbing device 5 is connected to the connecting arm 2. The body 1 is slidably connected and fixedly connected with the connecting arm shock absorbing device 4, and is located at the end of the body 1 away from the connecting arm 2; the connecting arm sh...

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Abstract

The invention discloses a solar energy and air energy composite aircraft. When the solar energy and air energy composite aircraft turns and slows down, a joint bearing drives an action shaft to swingcircumferentially; a horizontal thrust is applied to a second piston; a damping spring is driven to absorb pressure brought by the second piston; meanwhile, the second piston transmits pressure to a first air cylinder; the first air cylinder is driven to extrude internal air towards a direction of a first piston to slow down an impact; the first air cylinder located on the opposite side of an aircraft body sucks the air through a damping control valve; and a separation speed of the first air cylinder and the first piston is reduced, and then rebound vibration of the damping spring after absorbing pressure is inhibited so that when the aircraft steers and decelerates, the impact of the inertia of a load on the aircraft body can be reduced, and the aircraft can stably fly.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a composite aircraft of solar energy and air energy. Background technique [0002] At present, with the continuous development of science and technology, aircraft technology has been greatly improved in recent years, and many intelligent and multi-functional unmanned aerial vehicles have appeared. In response to the needs of transmitting information and monitoring in some small areas, unmanned aerial vehicles have received more and more attention. It is a new concept aircraft in rapid development, which has the advantages of flexible maneuverability, quick response, unmanned flight, and low operation requirements. By carrying multiple types of sensors, the aircraft can realize real-time image transmission and detection of high-risk areas, which is a beneficial supplement to satellite remote sensing and traditional aerial remote sensing. At present, the scope of use of unmanned...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D9/00B64C15/14F16F15/067
CPCB64D9/00B64C15/14F16F15/067B64U50/19
Inventor 周启凤
Owner CHONGQING NORMAL UNIVERSITY
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