Attitude adjusting and docking system with wide-range movement and automatic navigation
A technology for automatic navigation and automatic navigation vehicles, which is applied in aircraft component testing, aircraft assembly and other directions, and can solve the problems of poor versatility, low positioning accuracy, and poor scalability of fixed attitude adjustment and docking systems.
Active Publication Date: 2018-08-07
AVIC BEIJING AERONAUTICAL MFG TECH RES INST
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Problems solved by technology
[0004] The existing fixed attitude adjustment and docking system is fixed in a special assembly workshop, which occupies the use space. For some attitude adjustment and docking systems that are not used frequently, the workshop space is wasted
The fixed attitude adjustment and docking system has poor versatility, and only assembles specific parts in a dedicated area, which has poor scalability
At the same time, the automatic navigation mobile vehicle has low positioning accuracy due to air cushion drive or omnidirectional wheel drive.
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[0032] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0033] The invention relates to a large-scale mobile and automatic navigation attitude adjustment docking system, which is used for large-scale movement of parts such as aircraft, missiles or rockets in the aerospace field, automatic navigation to the relative position of the target part, and adjustment with the target part. The digitized and automated partial assembly or final assembly assembly process of postural docking.
[0034] Such as Figure 1-2 As shown, the attitude adjustment and docking system for large-scale movement and automatic navigation of the present invention includes an attitude adjustment mechanism 1, a measurement system 2 and an integrated control system; the m...
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The invention discloses an attitude adjusting and docking system with wide-range movement and automatic navigation. The system comprises an automatic navigation vehicle, an attitude adjusting mechanism, a measurement system and an integrated control system. The measurement system is in communication connection with the integrated control system, and the attitude adjusting mechanism is controllablyconnected to the integrated control system; the attitude adjusting mechanism is arranged on a bed body of the automatic navigation vehicle, and strut positioning mechanisms are arranged on the bed body of the automatic navigation vehicle and used for positioning and supporting the attitude adjusting mechanism. By adopting the autonomous navigation type attitude adjusting and docking system, the purposes of long-distance transportation and close-range precise adjustment, positioning and docking of product parts are achieved, and the problems of long-distance automatic navigation transportationand close-range precise attitude adjustment, positioning and docking are solved.
Description
technical field [0001] The invention relates to the technical field of automated assembly of aerospace vehicles, in particular to an attitude-adjusting docking system and method for large-scale movement and automatic navigation. Background technique [0002] Chinese patent CN201010545364.X discloses a patent called an aircraft component attitude adjustment and docking system and method based on four numerical control positioners, an attitude adjustment platform and a moving bracket. The invention relates to an aircraft component attitude adjustment and docking system and method for an attitude platform and a mobile bracket. The system includes: mobile bracket, attitude adjustment platform, CNC positioner, guide rail of CNC positioner group, upper computer, ball joint connection and laser tracker. The invention relates to an attitude-adjusting docking system in the form of a three-coordinate numerical control locator fixed on the foundation. [0003] The attitude adjustment...
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IPC IPC(8): B64F5/10B64F5/60
Inventor 荆道艳薛贵军杜兆才李光丽
Owner AVIC BEIJING AERONAUTICAL MFG TECH RES INST