Casing assembly
There is provided a casing assembly for a gas turbine engine comprising: a casing and electrically conductive intumescent material extending around the casing. The intumescent material is being activatable in response to electrical current to expand. The casing assembly comprises an electrical activation line extending around the casing to activate the intumescent material. The activation line extends in a pattern such that an activation area which circumscribes the activation line has an axial extent of at least 50% of the casing and a circumferential extent of at least 50%, to thereby activate the intumescent material at multiple locations over a corresponding area of the casing.
1. A casing assembly for a gas turbine engine comprising:
a casing having a circular annular cross-sectional profile extending in an axial direction and configured for surrounding components of the gas turbine engine;
electrically conductive intumescent material extending around the casing, the intumescent material being activatable in response to electrical current to expand; and
an electrical activation line extending around the casing to activate the intumescent material, the activation line extending in a pattern such that an activation area which circumscribes the activation line has an axial extent of at least 50% of an axial length of the casing and a circumferential extent of at least 50% of a circumference of an outer surface of the circular annular cross-sectional profile,
wherein the electrical activation line comprises two activation lines in a side by side relationship, the two activation lines being electrically coupled to each other via the electrically conductive intumescent material to thereby activate the intumescent material at multiple locations over a corresponding area of the casing.
2. A casing assembly according to claim 1 , wherein the activation line extends in a helical pattern.
3. A casing assembly according to claim 1 , wherein each of the two activation lines comprises a plurality of line portions arranged in side by side relationship.
4. A casing assembly according to claim 3 , wherein for each of the two activation lines, the respective line portions are joined in series by connecting turns of the activation line.
5. A casing assembly according to claim 3 , wherein the line portions are electrically coupled in parallel relationship.
6. A casing assembly according to claim 1 , wherein the activation line is coupled to an activation control system comprising a temperature sensor and a controller configured to selectively direct electric current through the activation line when an output of the temperature sensor is indicative of a fire or excessive heat event.
7. The casing assembly of claim 6 , wherein the controller is configured to selectively pass a current through the electrically conductive intumescent material via the two activation lines.
8. A casing assembly according to claim 1 , wherein a layer of resin surrounds the intumescent material and the electrical activation line.
9. A casing assembly according to claim 8 , wherein the resin layer comprises frangible portions.
10. The casing assembly of claim 1 , wherein the two activation lines are of opposing polarity, further comprising a controller configured to selectively direct current in the two activation lines.
11. The casing assembly of claim 1 , wherein the two activation lines are arranged to pass a current through the electrically conductive intumescent material.
12. A casing assembly for a gas turbine engine comprising:
a casing having a circular annular cross-sectional profile extending in an axial direction and configured for surrounding components of the gas turbine engine;
electrically conductive intumescent material extending around the casing, the intumescent material being activatable in response to electrical current to expand; and
an electrical activation line extending around the casing and electrically coupled to the electrically conductive intumescent material to activate the intumescent material, the activation line extending in a pattern such that an activation area which circumscribes the activation line has an axial extent of at least 50% of an axial length of the casing and a circumferential extent of at least 50% of a circumference of an outer surface of the circular annular cross-sectional profile, to thereby activate the intumescent material at multiple locations over a corresponding area of the casing;
wherein the activation line comprises two lines of opposing polarity in side by side relationship.
13. A casing assembly according to claim 12 , wherein the activation line extends in a helical pattern.
14. A casing assembly according to claim 12 , wherein each of the two lines comprises a plurality of line portions arranged in side by side relationship.
15. A casing assembly according to claim 14 , wherein for each of the two lines, the respective line portions are joined in series by connecting turns of the activation line.
16. A casing assembly according to claim 14 , wherein the line portions are electrically coupled in parallel relationship.
17. A gas turbine engine comprising:
a casing having a circular annular cross-sectional profile extending in an axial direction and configured for surrounding components of the gas turbine engine;
electrically conductive intumescent material extending around the casing, the intumescent material being activatable in response to electrical current to expand; and
an electrical activation line extending around the casing and electrically coupled to the electrically conductive intumescent material to activate the intumescent material, the activation line extending in a pattern such that an activation area which circumscribes the activation line has an axial extent of at least 50% of an axial length of the casing and a circumferential extent of at least 50% of a circumference of an outer surface of the circular annular cross-sectional profile, to thereby activate the intumescent material at multiple locations over a corresponding area of the casing.
18. The gas turbine engine of claim 17 , wherein the activation line comprises two activation lines of opposing polarity in side by side relationship, and wherein the gas turbine engine comprises a controller configured to selectively direct current in the two activation lines.
19. The gas turbine engine of claim 18 , wherein each of the two activation lines comprises a plurality of line portions arranged in side by side relationship, the line portions joined by connecting turns of the respective activation lines.