Aircraft safe landing protection ball
A technology for safe landing and protection of the ball. It is applied to aircraft landers and other directions. It can solve problems such as inability to adjust the use, damage to the aircraft circuit, and inconvenience in use, and achieve a variety of functions.
Inactive Publication Date: 2021-01-05
福州力佳达智能科技有限公司
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Problems solved by technology
[0002] With the development of science and technology, remote control aircraft has come into people's sight. The structural feature of the aircraft is that each of its four corners is equipped with a rotor, which is driven by a motor respectively. The blades can rotate forward or reverse. In order to keep the aircraft The aircraft is equipped with 3-direction gyroscopes and 3-axis acceleration sensors to form an inertial navigation module. It also uses electronic controllers to ensure its fast flight. The existing aircraft is in direct contact with the ground during flight and landing. , easy to produce a large impact force, the impact force will cause damage to the internal circuit of the aircraft, long-term use will cause damage to the equipment, and it is inconvenient to use. The existing equipment cannot be adjusted for different positions where the aircraft falls, and it is inconvenient to use. Single function
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[0024] As a preferred embodiment of the present invention, the installation rod 10 is installed on the fixed hanging lug 8 through the rotating shaft 11 , and the top of the electric push rod 1 is installed on the connecting lug 12 through the rotating shaft 1 .
[0025] As a preferred embodiment of the present invention, the number of the movable plates 2 is 6, and elastic plates 6 are installed between the movable plates 2, and the elastic plates 6 are made of rubber.
[0026] As a preferred embodiment of the present invention, a base 13 is installed on the bottom of the mounting seat 1 , a support column 14 is installed on the base 13 , a roller 15 is installed on the support column 14 , and the roller 15 is connected with the installation The inner wall of the seat 1 is matched.
[0027] As a preferred embodiment of the present invention, a fixed seat 16 is welded on the support column 14, the second electric push rod 17 is installed on the fixed seat 16, and the movable r...
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The invention discloses an aircraft safe landing protection ball comprising a protection ball body; the protection ball body comprises an installation seat and an intelligent system; the intelligent system comprises an infrared sensor, a control box, an intelligent processor, a control switch, a power supply device, a direct current motor, a first electric push rod and a second electric push rod,and a movable plate is mounted on the installation seat; the movable plate is mounted on the installation seat through a fixing shaft, a groove is formed in the movable plate, a hollow rubber ball isplaced in the groove, and the infrared sensor is mounted at one end of the movable plate. The aircraft safe landing protection ball detects the position of an aircraft through an infrared sensor; theintelligent processor controls the motor to rotate, so that the direction of the second electric push rod is changed, the second electric push rod conducts left-right fine adjustment on the position of the installation seat through a movable rod, adjustment and use are conducted according to the position of the aircraft, and functions are diversified.
Description
technical field [0001] The invention relates to the field of aircraft equipment, in particular to an aircraft safety landing protection ball. Background technique [0002] With the development of science and technology, the remote control aircraft has come into people's sight. The structure of the aircraft is characterized by a rotor on each of its four corners, which is driven by the motor respectively. The blades can rotate forward or reverse. In order to keep the aircraft The aircraft is equipped with 3-direction gyroscopes and 3-axis acceleration sensors to form an inertial navigation module. It also uses an electronic controller to ensure its fast flight. The existing aircraft is in direct contact with the ground during flight and landing. , It is easy to generate a large impact force, the impact force will cause damage to the internal circuit of the aircraft, and long-term use will cause damage to the equipment, which is inconvenient to use. Single function. SUMMARY...
Claims
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IPC IPC(8): B64D45/06
CPCB64D45/06
Inventor 林建斌
Owner 福州力佳达智能科技有限公司