Device for a rotating gland seal

1. A machine arranged to operate in explosive environments, comprising a rotatable shaft ( 16 ) extending through a stationary part ( 10 ) arranged between an interior side ( 12 ) and an exterior side ( 14 ) of said machine, a gland ( 20 ) which is mounted in said stationary part ( 10 ) and which is provided with a through hole in order to accommodate said rotatable shaft ( 16 ) such that a first flame path is provided between the rotatable shaft ( 16 ) and the gland ( 20 ), wherein the machine comprises dampening means ( 42 ) arranged between and separating the gland ( 20 ) and the stationary part ( 10 ) in the axial and radial directions such that a second flame path ( 50 , 56 ) is provided between the gland ( 20 ) and the stationary part ( 10 ), the dampening means ( 42 ) maintaining the existence of the second flame path ( 50 , 56 ), and the dampening means comprising an annular part ( 44 ) having discrete enlarged portions ( 46 ) arranged to contact the gland and stationary part, and permitting axial and radial movement of the gland ( 20 ) in relation to the stationary part ( 10 ) upon rotation of the rotatable shaft ( 16 ), said first and second flame paths extending from the interior side ( 12 ) to the exterior side ( 14 ).

2. The machine according to claim 1 , wherein the enlarged portions comprise a number of discrete resilient members ( 46 ) arranged against at least one surface of the gland ( 20 ) and at least one surface of the stationary part ( 10 ), which surfaces are facing in the axial direction of the rotatable shaft ( 16 ).

3. The machine according to claim 2 , wherein one set of resilient members ( 46 ) are arranged between a first surface of the gland ( 20 ) and a first surface of the stationary part ( 10 ), which first surfaces are facing each other, and that another set of resilient members are arranged between a second surface of the gland ( 20 ), facing in the opposite direction as the first surface of the gland ( 20 ) and a second surface of the stationary part ( 10 ), facing in the opposite direction as the first surface of the stationary part ( 10 ), which second surfaces are facing each other.

4. The machine according to claim 2 , wherein the discrete resilient members ( 46 ) are inter-connected and spaced at even intervals along a circumference around the rotatable shaft ( 16 ).

5. The machine according to claim 2 , wherein the discrete resilient members ( 46 ) are formed such that they provide point contacts with said surfaces of the gland ( 20 ) and the stationary part ( 10 ) or line contacts with said surfaces of the gland ( 20 ) and the stationary part ( 10 ).

6. The machine according to claim 1 , wherein the machine comprises a locking means ( 38 , 54 ) arranged to rotationally lock said gland ( 20 ) in relation to the stationary part ( 10 ) of the machine.

7. The machine according to claim 1 , wherein the gland ( 20 ) is arranged with a flange-shaped part ( 24 ) having at least one circumferential recess ( 40 ) for receiving said dampening means ( 42 ).

8. The machine according to claim 1 , wherein at least said second flame path is constituted by a gap dimensioned to prevent the passage of sparks or flame out of said machine.

9. The machine according to claim 1 , wherein each of said flame paths is constituted by a gap dimensioned to prevent the passage of sparks or flame out of said machine.