COMBUSTOR LINER

PROBLEM TO BE SOLVED: To provide a combustor having a combustion zone formed inside. SOLUTION: The combustor 1 includes: an annular liner 10 having a first mixing hole 11 formed therein at a first axial position 14; a flow sleeve 20 having a second mixing hole 21 formed therein at a second axial pos...

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Bibliographische Detailangaben
Hauptverfasser:	CHILA RONALD JAMES, DAVIS LEWIS BERKELY JR
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a combustor having a combustion zone formed inside. SOLUTION: The combustor 1 includes: an annular liner 10 having a first mixing hole 11 formed therein at a first axial position 14; a flow sleeve 20 having a second mixing hole 21 formed therein at a second axial position 24 and forming a first flow space 30 at an exterior of the liner 10; a port 40 connected to the flow sleeve 20 at the second axial position 24 and removing air from the first flow space 30 via the second mixing hole 21; and a shield 50 having a third mixing hole 51 formed therein at the second axial position 24, protecting the liner 10 and arranged to form a second flow space 60 within the liner 10, leading to the combustion zone 2 via the third mixing hole 51 and to the first flow space 30 via the first mixing hole 11. COPYRIGHT: (C)2011,JPO&INPIT