A device for a combustion chamber of a gas turbine

Details A device for a combustion chamber of a gas turbine A device for a combustion chamber of a gas turbine

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/26 (2006.01) F23R 3/28 (2006.01) F23R 3/30 (2006.01) F23R 3/34 (2006.01) F23R 3/60 (2006.01)

Patent

CA 2467334

The invention relates to a device for a combustion chamber (1) in a gas turbine for controlling the intake of gas to the combustion zone (10, 11) of the combustion chamber. The device comprises a control element (12) which is arranged outside the combustion chamber and which in turn comprises a means (13) for covering at least one inlet to the combustion zone, the cover means being displaceable in relation to the combustion chamber. The device further comprises a means (16) connected to the cover means for supporting the control element. The means of support (16) is accommodated in a structure (4) at the rear of the combustion chamber (1).

L'invention concerne un dispositif conçu pour la chambre à combustion (1) d'une turbine à gaz servant à commander l'admission de gaz dans la zone de combustion (10, 11) de cette chambre de combustion. Ce dispositif comprend un élément de régulation (12) situé à l'extérieur de la chambre de combustion et comprenant, à son tour, des moyens (13) servant à recouvrir au moins une entrée de la zone de combustion et pouvant être déplacés par rapport à la chambre de combustion. Ce dispositif comprend, de plus, des moyens (16) reliés aux moyens de couverture afin de supporter l'élément de régulation. Ces moyens de support (16) logent dans une structure (4) située à l'arrière de la chambre de combustion (1).

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