Study of Manufacturing Process of Holes in Aeroengine Heat Shield

<div>Comparing photos (<svg height="8.94669pt" id="M131" style="vertical-align:-0.2063894pt" version="1.1" viewbox="-0.0498162 -8.7403 58.0016 8.94669" width="58.0016pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M41 650V615C111 608 121 602 121 516V134C121 48 111 42 32 35V0H289C413 0 518 27 592 83C668 141 717 229 717 351C717 446 678 517 628 564C564 625 467 650 341 650H41ZM255 540C255 569 257 586 265 595C272 602 292 609 328 609C397 609 450 589 491 547C537 502 566 426 566 331C566 152 474 43 340 43C270 43 255 68 255 140V540Z"></path></g><g transform="matrix(.013,0,0,-0.013,13.525,0)"><path d="M535 323V373H52V323H535ZM535 138V188H52V138H535Z"></path></g><g transform="matrix(.013,0,0,-0.013,24.788,0)"><path d="M241 635C89 635 35 457 35 312C35 153 89 -12 240 -12C390 -12 443 166 443 312C443 466 390 635 241 635ZM238 602C329 602 354 454 354 312C354 172 330 22 240 22C152 22 124 173 124 313S148 602 238 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International Journal of Aerospace Engineering

Study of Manufacturing Process of Holes in Aeroengine Heat Shield

Figure 4