BURNER

The gas turbine burner (100) has a combustion air duct (104) in which are several spin-generating elements (108) forming spin-generators (109) in the form of spin blade rings. The ring consists of first (108A) and second (108B) blades. An extra pilot burner (106) stabilizes the mixture of fuel and c...

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Bibliographische Detailangaben
1. Verfasser:	HEIN, OLAF
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR AIR SUPPLY BLASTING CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES COMBUSTION APPARATUS COMBUSTION PROCESSES DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS DRAUGHT-INDUCING GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS WEAPONS
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Beschreibung
Zusammenfassung:	The gas turbine burner (100) has a combustion air duct (104) in which are several spin-generating elements (108) forming spin-generators (109) in the form of spin blade rings. The ring consists of first (108A) and second (108B) blades. An extra pilot burner (106) stabilizes the mixture of fuel and combustion air emerging from the combustion air duct.