Anti-vibration vertical take-off and landing aircraft
A vertical take-off and landing, aircraft technology, applied in the field of unmanned aerial vehicles, can solve problems such as data deviation
Inactive Publication Date: 2021-09-03
LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
View PDF8 Cites 0 Cited by
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
[0004] The purpose of the present invention is to provide an anti-vibration vertical take-off and landing aircraft, which can meet the anti-vibration requirements, thereby solving the problem of data deviation caused by the vibration of the angle and acceleration sensors
Method used
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View moreImage
Smart Image Click on the blue labels to locate them in the text.
Smart ImageViewing Examples
Examples
Experimental program
Comparison scheme
Effect test
Embodiment Construction
[0037] Next, the technical solutions in the embodiments of the present invention will be apparent from the embodiment of the present invention, and it is clearly described, and it is understood that the described embodiments are merely embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, there are all other embodiments obtained without making creative labor without making creative labor premises.
[0038] The core of the present invention is to provide a rigid vertical start-off aircraft, which can meet the resistance requirements, so that the angle and acceleration sensor can cause data deviation due to vibration.
[0039]In order to better understand the present invention, the present invention will be described in detail below with reference to the drawings and specific embodiments.
[0040] It should be noted that orientation as defined by the "upper end, lower end, left, right" as defined below.
[0041] Please r...
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More PUM
Login to View More Abstract
The invention discloses an anti-vibration vertical take-off and landing aircraft, which comprises an aircraft body, an anti-vibration module and a sensor assembly are arranged in the aircraft body, and the anti-vibration module comprises a carrying table and a three-axis moving vibration buffering structure; the three-axis moving vibration buffering structure comprises an X-axis moving vibration buffering assembly and a Y-axis moving vibration buffering assembly, wherein the X-axis moving vibration buffering assembly is connected with the carrying table in a matched mode and enables the carrying table to move in the X-axis direction to achieve vibration buffering, and the Y-axis moving vibration buffering assembly is connected with the carrying table in a matched mode and enables the carrying table to move in the Y-axis direction to achieve vibration buffering. the Z-axis moving vibration buffering assembly is connected with the X-axis moving vibration buffering assembly and the Y-axis moving vibration buffering assembly in a matched mode and enables the X-axis moving vibration buffering assembly and the Y-axis moving vibration buffering assembly to move in the Z-axis direction so as to achieve vibration buffering. According to the anti-vibration vertical take-off and landing aircraft, the anti-vibration requirements of the aircraft in different working environments can be met, so that the situation of data deviation caused by vibration of the angle sensor and the acceleration sensor can be improved, and the accuracy of data detected by the angle sensor and the acceleration sensor can be improved.
Description
Technical field [0001] The present invention relates to the field of drone, and in particular, to a resistant vertical start-off aircraft. Background technique [0002] UAVs are generalized for remote control aircraft without boarding, including remote control, guiding, and automatic driving, usually divided into military and civil drones according to the use. The drone is widely used, whether it is remotely controlled or automatic flight, vertical start-down drones have been widely used due to unreachable restrictions, including empty beats, logistics, exploration or Military activities, etc. However, in the existing drone, the sensor assembly (angle and acceleration sensor) is located inside the flight controller, and the drone occurs during flight, so that the data deviation of the sensor assembly inside the flying controller is caused. [0003] Therefore, how to avoid data deviations of sensor components in the flight controller due to vibration during flight, is a technical ...
Claims
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More Application Information
Patent Timeline
Login to View More Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00B64C29/00F16F15/02
CPCB64D47/00B64C29/00F16F15/02
Inventor 徐开明李佳鹏高大鹏冯国涛许可吴志刚陈辅政陈敏尹欣繁时广轶吴天祥
Owner LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT