Voronko I. Development of the pneumopulse mandrelling technology of the holes in aircraft structures made of titanium alloys using robotic workcells

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0419U003086

Applicant for

Specialization

  • 05.07.02 - Проектування, виробництво та випробування літальних апаратів

13-06-2019

Specialized Academic Board

Д 64.062.04

National Aerospace University "Kharkiv Aviation Institute"

Essay

The subject of research is the technology and air-impact tool for holes mandreling in aviation structures made of titanium alloys in robotic complexes; the objective of research is to develop the technology and modification of the air-impact tool for holes mandreling in aviation structures made of titanium alloys when used in RTC conditions; research methods – numerical methods for solving problems for processes of air-impact holes mandreling in aviation structures of titanium alloys; technological recommendations for air-impact holes mandreling in aviation structures made of titanium alloys were developed on the basis of experimental studies; the deformed state of the mandrelled samples was investigated by methods of macro- and microstructural metallography and electron microscopy; the results of research – technological recommendations for parameters selection of the pulse mandrelling process of the holes in aircraft structures made of titanium alloys are provided; pneumopulse mandrelling device for the use as a part of the robotic workcell is improved by performing constructive modification; novelty – for the first time, technological process of the pulse mandrelling of the holes in aircraft structures made of titanium alloys are developed, having provided increased durability by more than 15%; the method of determining rational parameters of pulse mandrelling of holes with titanium alloys in the CAD / CAE was further developed, namely, the properties of the working tool mandrel are given as a power function instead of an absolutely rigid body, which made it possible to reduce the error between numerical simulation and a field experiment from 15% to 10%; improved methodology for the development of technological processes for pulse mandrelling of holes in aircraft structures allowed the use of pneumopulse devices as a part of the robotic workcell; the degree of implementation – Antonov Company, National Aerospace University "Kharkiv Aviation Institute"; area of implementation – aviation industry.

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