Compensation assembly for a damper of a gas turbine
View Patent ↗The present invention relates to dampers for gas turbines and, for example, to a compensation assembly for a damper of a gas turbine for reducing the pulsations occurring in the combustion chamber. The damper can include a resonator cavity with a neck tube in flow communication with the interior of the combustion chamber, wherein the compensation assembly includes a spherical joint associated to the neck tube and configured to allow relative rotation between the combustion chamber and the resonator cavity, and having a bulb portion disposed around the neck tube and a spherical socket configured to internally host the bulb portion, wherein the spherical socket can have a top collar portion and a bottom collar portion connected to each other.
1. A compensation assembly for a damper of a combustion chamber of a gas turbine, the damper having a resonator cavity with a neck tube in flow communication with an interior of the combustion chamber, the compensation assembly comprising:
a spherical joint associated to a neck tube and configured to allow relative rotation between a combustion chamber and a resonator cavity, the spherical joint including:
a bulb portion configured as a collar element for disposal around the neck tube;
a spherical socket configured to internally host said bulb portion, wherein the spherical socket has a top collar portion and a bottom collar portion, the top and bottom collar portions being connected to each other by a joint; and
a sliding part formed directly on the spherical socket and configured to be air-tightly fitted into a groove of the resonator cavity in a direction traversing a longitudinal axis of the neck tube between said sliding part and the groove,
wherein said collar element is internally shaped for relative radial displacement of the neck tube along the longitudinal axis of the neck tube.
2. The compensation assembly according to claim 1 , in combination with a damper having the resonator cavity with the neck tube, wherein said bulb portion is inserted on the neck tube.
3. The compensation assembly according to claim 2 , wherein said collar element defines internally a cylindrical surface.
4. The compensation assembly according to claim 1 , wherein said bottom and top collar portions are connected by complementary threaded portions as the joint.
5. The compensation assembly according to claim 1 , wherein said sliding part is formed directly on said top collar portion.