Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

aircraft

A technology of aircraft and support parts, applied in the field of aircraft, can solve problems such as damage to sensing components, affect the execution of normal tasks of the aircraft, affect the perception accuracy of sensing components, and achieve the effect of eliminating vibration

Active Publication Date: 2018-07-24
SZ DJI TECH CO LTD
View PDF8 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In existing aircraft, the sensing components are generally fixed directly on the fuselage shell of the aircraft. However, since the aircraft will vibrate due to the rotation of the motor and propeller and / or encountering air flow during flight, this vibration will pass through the aircraft. The special body of the fuselage is transmitted to the sensing component, thereby affecting the sensing accuracy of the sensing component, further affecting the execution of normal tasks of the aircraft, and in severe cases, causing damage to the sensing component

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 more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • aircraft
  • aircraft
  • aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0021] see figure 1 and figure 2 , the aircraft 100 described in the embodiment of the present invention includes a fuselage 10 , a sensing assembly 20 , a support 23 and a shock absorber 24 .

[0022] The fuselage 10 is a load-bearing part of the aircraft 100, the outer surface and / or inside of the fuselage 10 are used to carry the functional modules of the aircraft 100, and the functional modules may include but not limited to the inertial measurement unit (not shown in the figure), image acquisition module (not shown in the figure), rotor assembly 30 , height sensor (not shown in the figure), temperature sensor (not shown in the figure), etc.

[0023] The fuselage 10 includes a main shell 11 , an arm shell 12 and a landing frame 13 . Both the main housing 11 and the support arm housing 12 adopt a structure in which the upper and lower parts are interlocked with each other, and only the lower half of the main housing 11 and the support arm housing 12 are shown in the figu...

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

No PUM Login to View More

Abstract

An aircraft, comprising a fuselage, a sensing assembly and a supporting part arranged in the fuselage, and the fuselage includes a main casing. The main casing includes a bottom wall and a side wall connected with the bottom wall, and the side wall and the bottom wall jointly enclose a receiving space. The sensing component and the support are accommodated in the accommodation space, the support is connected to the bottom wall, the sensing component is arranged on the support and has a gap with the side wall . The aircraft will use a support to arrange the sensing assembly on the bottom wall of the fuselage and keep a gap between the sensing assembly and the side wall of the fuselage, which can effectively reduce or eliminate the parallel motion of the sensing assembly. Vibration in the direction of the bottom wall.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to an aircraft with a sensing component. Background technique [0002] Sensing components, such as Inertial Measurement Unit (IMU), are important components of the aircraft, which are used to sense the flight attitude, orientation and other environmental information of the aircraft. In existing aircraft, the sensing components are generally fixed directly on the fuselage shell of the aircraft. However, since the aircraft will vibrate due to the rotation of the motor and propeller and / or encountering air flow during flight, this vibration will pass through the aircraft. The special body of the fuselage is transmitted to the sensing component, thereby affecting the sensing accuracy of the sensing component, further affecting the execution of normal tasks of the aircraft, and in severe cases, causing damage to the sensing component. Contents of the invention [0003] In view of this, it is n...

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
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/00
Inventor 冯建刚潘国秀石仁利
Owner SZ DJI TECH CO LTD
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com