| 摘要 |
<p>The invention relates to an impingement baffle for a gas turbine engine, whereby the impingement baffle (1) is a one piece split impingement ring (2) with fastening elements (4,5) at both free ends (6a,6b) of the impingement ring (2) to enable the closing of the impingement ring (2). The invention relates further to a gas turbine engine comprising at least one such an impingement baffle (1).</p> |
