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Mechanical arm for automatically tightening bolts of aero-engine disc-drum structural parts and its working method

A technology for aero-engines and structural parts, which is applied in manipulators, program-controlled manipulators, metal processing, etc. It can solve the problems of inability to quantitatively evaluate the bolt tightening effect, the inability to connect and use the robot arm, and the insufficient compact structure of the device to achieve the tightening effect. , small mass, easy to control the effect

Active Publication Date: 2019-04-19
NORTHEASTERN UNIV LIAONING
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

For example, in Chinese patent applications such as CN201210229080.9, CN201610211363.9, CN201610723895.0, CN201610382080.0, CN201610213153.3, CN201010113070.X, 201410600722.0 and other Chinese patent applications, but the automation of several or more types of bolts is disclosed, The bolt tightening effect cannot be quantitatively evaluated, and the structure of the device is not compact enough, it takes up a large space, and cannot be adjusted actively. It still needs to be operated by workers during the tightening process, and it cannot be connected with the robot arm widely used in the industry at present. , not suitable for occasions with complex forms such as drum structures with multiple sets of complex bolt holes

Method used

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  • Mechanical arm for automatically tightening bolts of aero-engine disc-drum structural parts and its working method
  • Mechanical arm for automatically tightening bolts of aero-engine disc-drum structural parts and its working method
  • Mechanical arm for automatically tightening bolts of aero-engine disc-drum structural parts and its working method

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Embodiment Construction

[0035] Specific embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0036] Mechanical arm for automatically tightening bolts of aero-engine disc drum structural parts, including clamping device 4, bolt tightening head 12, bolt fixing sleeve 10, transmission gear 1, transmission gear 2 9, servo motor 5, cylinder 6, rotation angle sensor 2 and torque Sensor 13; the upper part of the clamping device 4 has a long axis through it, and the lower part has a left clamping arm and a right clamping arm; the two ends of the long axis are positioned by bearings, one end of the long axis is connected to the output shaft of the servo motor 5, and the long axis The other end is connected with the angle sensor 2, and the end of the angle sensor 2 is connected with the transmission gear-1 axis; the bolt tightening head 12 is housed on the left clamp arm, and the bolt fixing sleeve 10 is housed on the right clamp arm; the bolt t...

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Abstract

The invention discloses an automatic tightening mechanical arm for bolts of an aeroengine drum structure component, which includes a clamping device, a bolt tightening head, a bolt fixing sleeve, a first transmission gear, a second transmission gear, a servo motor, a cylinder, a rotation angle sensor and a torque sensor; The upper part of the clamping device has a long axis running through it, one end is connected to the output shaft of the servo motor, and the other end is connected to the rotation angle sensor; the lower part of the clamping device is equipped with a bolt tightening head and a bolt fixing sleeve, and the bolt tightening head is connected to the torque sensor. , the torque sensor is connected to the two axes of the transmission gear. The torque sensor and the rotation angle sensor control the servo motor in real time, and use the output value as the input signal of the servo motor to perform negative feedback excitation to achieve automatic tightening. The invention can not only tighten the bolts, but also control the servo motor in real time through the torque sensor and the rotation angle sensor, so as to achieve the best tightening effect and a high degree of automation.

Description

technical field [0001] The invention belongs to the technical field of aviation automation assembly, and in particular relates to a robot arm for automatically tightening bolts of a disc drum structure part of an aero engine. Background technique [0002] As an important part of an aero-engine, the disc-drum structural part is an important factor affecting the stability and safety of the engine operation. It is usually composed of a disc, a cylinder and a taper sleeve. The above three parts are connected by detachable bolts. Parts are pressed and connected to form a whole rotor structure, and the bolts are evenly distributed on the pressing surface of the disc, and the torque is transmitted by the friction force of the pressing surface. Since the disc drum structure is a rotatable drum at the wheel rim, the rigidity of the structure is better; and the centrifugal force is borne by the wheel disc, so the strength of the structure is higher. In view of these advantages, disc-...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P19/06B25J9/16B25J13/08
CPCB23P19/06B25J9/1687B25J13/085
Inventor 李晖陈延炜吴怀帅哈泽坤闻邦椿
Owner NORTHEASTERN UNIV LIAONING