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Titanium nail riveting device based on lateral ultrasonic energy field assistance and forming method thereof

A riveting device and field-assisted technology, which is applied in the field of aircraft assembly, can solve the problems of large riveting force, cracking of titanium nails, uneven deformation of titanium nails, etc., and achieve the goals of safe and convenient use, improved shaping, fatigue strength and service life Effect

Active Publication Date: 2019-10-22
江苏航浦国创复材研究院有限公司
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  • Abstract
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  • Claims
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Problems solved by technology

[0003] The present invention provides a titanium nail riveting device and its forming method based on the assistance of the lateral ultrasonic energy field, which can effectively solve the problems of excessive riveting force, cracking of the titanium nail, and deformation of the titanium nail in the traditional titanium nail riveting process proposed in the above-mentioned background technology. Inhomogeneity, which limits the application of titanium nail riveting connection method in the aerospace industry

Method used

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  • Titanium nail riveting device based on lateral ultrasonic energy field assistance and forming method thereof
  • Titanium nail riveting device based on lateral ultrasonic energy field assistance and forming method thereof
  • Titanium nail riveting device based on lateral ultrasonic energy field assistance and forming method thereof

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Embodiment

[0042] Example: such as Figure 1-2 As shown, the present invention provides a technical solution, a titanium nail riveting device assisted by a lateral ultrasonic energy field, including a frame 1 for support, wherein the frame 1 is composed of a column and an iron plate, and the iron plate adopts The A3 iron plate has good rigidity, and the force that the frame 1 bears is greater than 50KN, which improves the stability of the device. The top of the frame 1 is equipped with a fixture tooling module 2 for fixing objects, and one side of the fixture tooling module 2 is installed with a vertical installation frame 6, and the bottom end of the vertical mounting frame 6 is connected to the frame 1, the ultrasonic auxiliary module 3 is installed laterally on the vertical mounting frame 6, and the power module 4 is installed on the top of the vertical mounting frame 6, between the ultrasonic auxiliary module 3 and the power module 4 A data acquisition module 5 for collecting data is...

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Abstract

The invention discloses a titanium nail riveting device based on lateral ultrasonic energy field assistance and a forming method thereof. The titanium nail riveting device comprises a rack used for supporting; a clamp tooling module used for fixing objects is erected at the top end of the rack; a vertical mounting frame is arranged at one side of the clamp tooling module; the bottom end of the vertical mounting frame is connected with the rack; and the vertical mounting frame is laterally provided with an ultrasonic assistant module. The titanium nail riveting device based on the lateral ultrasonic energy field assistance is scientific and reasonable in structure and safe and convenient to use; through laterally arranging the ultrasonic assistant module, an ultrasonic generator can work normally under the riveting force of a titanium rivet instead of being abnormal under the excessive riveting force, and the maximum riveting force can be increased up to 30 KN to improve the riveting quality; and the ultrasonic energy field assistant riveting is generated through the action of the ultrasonic assistant module, and the volume effect and the surface area effect under the ultrasonic energy field are fully utilized to reduce the deformation resistance during riveting, so that the uniformity of the interference amount of riveting is effectively improved, and the riveting quality is improved.

Description

technical field [0001] The invention relates to the technical field of aircraft assembly, in particular to a titanium nail riveting device assisted by a lateral ultrasonic energy field and a forming method thereof. Background technique [0002] With the continuous growth and development of the aviation industry, the aircraft gradually expands the application of the overall structure, titanium alloy structure and composite material structure, and the requirements for the variety and quality of riveted joints are greatly improved. In order to meet some special requirements for riveted parts, domestic and foreign developed Some special rivets, such as ring groove rivets, blind rivets, threaded hollow rivets, high shear rivets, titanium nails, high lock bolts and other riveting process equipment; among them, blind rivets and high lock bolts are currently widely used in aircraft assembly , but due to its high cost and the potential corrosion problem between the laminated structur...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B21J15/12B21J15/20
CPCB21J15/12B21J15/20
Inventor 陈文亮王星星齐振超刘勇肖叶鑫杨景岚
Owner 江苏航浦国创复材研究院有限公司
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