COMBUSTOR PANEL MOUNTING SYSTEMS AND METHODS

Combustors of gas turbine engines having a combustor shell (330; 430; 530; 630; 730; 830; 930; 1030) having a first end (342; 942) and a second end (344; 1044) opposite the first end, a first securing element (346; 946) positioned at the first end of the combustor shell, a second securing element (3...

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Bibliographische Detailangaben
1. Verfasser:	KRAMER, Stephen K
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	Combustors of gas turbine engines having a combustor shell (330; 430; 530; 630; 730; 830; 930; 1030) having a first end (342; 942) and a second end (344; 1044) opposite the first end, a first securing element (346; 946) positioned at the first end of the combustor shell, a second securing element (348; 1048) positioned at the second end of the combustor shell, a plurality of high temperature material panels (340; 440; 540; 640; 740; 840; 940; 1040) fixedly secured by the first securing element (346; 946) at the first end (342; 942) and the second securing element (348; 1048) at the second, wherein a panel gap (454; 554; 654) is formed between edges of adjacent high temperature material panels of the plurality of high temperature material panels, and a seal divider (450; 550; 650) extending from the first end (342; 942) to the second end (344; 1044) and positioned on the combustor shell and arranged to seal the panel gap (454; 554; 654) between adjacent first and second high temperature material panels.