Holding device of a cooling tube for a turbojet casing
View Patent ↗A holding device of a cooling tube for a turbojet casing, the holding device including a first plate configured to be arranged in integral contact with a turbojet casing; a second plate, the first and second plates having a gap therebetween; a first spacer and the second spacer which are arranged between the first plate and the second plate and defining the gap between the first and second plates, the first and second spacers having a spacing therebetween suitable for passing the cooling tube.
1. A holding device of a cooling tube for a turbojet casing, the holding device comprising:
a first plate configured to be arranged in integral contact with a turbojet casing;
a second plate, the first and second plates having a gap therebetween, and
a first spacer and a second spacer which are arranged between the first plate and the second plate and define the gap between the first and second plates, the first and second spacers having a spacing therebetween suitable for passing the cooling tube.
2. The holding device according to claim 1 , wherein:
the first plate includes a first runner configured to position the cooling tube against the first plate, and/or
the second plate includes a second runner configured to position the cooling tube against the second plate.
3. The holding device according to claim 1 , further comprising a pad configured to dampen a contact between the cooling tube on the one hand, and the first plate and/or the second plate on the other hand.
4. The holding device according to claim 3 , wherein the pad comprises:
a first part arranged on the first plate, and/or
a second part arranged on the second plate.
5. The holding device according to claim 1 , wherein the first plate includes a first side tab and a second side tab, the first and second side tabs being configured to position the first plate on the turbojet casing.
6. The holding device according to claim 1 , wherein the first plate, the first spacer and the second spacer form a single piece part.
7. The holding device according to claim 1 , further comprising:
a first connecting device securing the first spacer to the second plate, and
a second connecting device securing the second spacer to the second plate.
8. The holding device according to claim 7 , wherein the second plate includes:
a first oblong hole for mounting the first connecting device, and
a second oblong hole for mounting the second connecting device.
9. A cooling device for turbojet casing including:
a holding device of a cooling tube according to claim 1 , and
the cooling tube,
the cooling device including a sheath configured to dampen the contact between the cooling tube on the one hand, and the first and second plates on the other hand, the sheath surrounding a part of the cooling tube.
10. A turbojet casing comprising a cooling device according to claim 9 , wherein the turbojet casing forms a single piece part with the first plate.
11. The holding device according to claim 1 , wherein the first and second spacers are individual elements that are separately arranged between the first plate and the second plate and separately secured to the second plate by a respective first and second connecting device.
12. The holding device according to claim 1 , wherein the first plate, the first spacer and the second spacer form a single piece part, and wherein said single piece part is secured to said second plate only via said first and second spacers.
13. The holding device according to claim 1 , wherein more than a third of a lower surface of the first plate is in contact with the turbojet casing.
14. The holding device according to claim 1 , wherein the first plate includes a first runner configured to position the cooling tube against the first plate.