Combustion liner for gas turbine having liner stops

In a gas turbine combustion system, liner stops mount a combustion liner within a flow sleeve. The liner stops are mounted on the outer surface of the combustion liner and the inner surface of the flow sleeve in a symmentrical array of liner stops. The liner stops have inclined contacting surfaces t...

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Bibliographische Detailangaben
Hauptverfasser:	CALABRESE SALVADORE, DINC SAIM, LAWEN, JR. JAMES L
Format:	Patent
Sprache:	eng
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:	In a gas turbine combustion system, liner stops mount a combustion liner within a flow sleeve. The liner stops are mounted on the outer surface of the combustion liner and the inner surface of the flow sleeve in a symmentrical array of liner stops. The liner stops have inclined contacting surfaces that support the liner within the sleeve, and provide rubbing contact between the two. These inclined surfaces are on a post of a male liner stop that fits into a channel of a female liner stop.