Rotor containment structure
A shroud reinforcement is provided for a shroud that is coaxial with and partially surrounds a rotor and that includes tubular and flange sections and a transition section axially interposed between the tubular and flange sections. The shroud reinforcement includes first fiber-reinforced polymer-matrix composite reinforcement elements with fibers extending along an axial dimension of the rotor and being disposed to reinforce the transition section and second fiber-reinforced polymer-matrix composite reinforcement elements with fibers extending along a circumferential dimension of the rotor and being disposed to reinforce the transition section.
1 . A shroud reinforcement assembly, comprising:
a shroud, which is formed of one or more of metallic and alloy materials, the shroud being coaxial with and partially surrounding a rotor and comprising tubular and flange sections and a transition section axially interposed between the tubular and flange sections; and
a shroud reinforcement comprising:
first fiber-reinforced polymer-matrix composite reinforcement elements with fibers extending along an axial dimension of the rotor and being disposed to reinforce the transition section; and
second fiber-reinforced polymer-matrix composite reinforcement elements with fibers extending along a circumferential dimension of the rotor and being disposed to reinforce the transition section,
wherein the first fiber-reinforced polymer-matrix composite reinforcement elements abut with an external surface of the transition section.
2 . The shroud reinforcement assembly according to claim 1 , wherein at least one of:
the first fiber-reinforced polymer-matrix composite reinforcement elements extend along a full axial length of the transition section and do not overlap with one another,
the first fiber-reinforced polymer-matrix composite reinforcement elements extend along the full axial length of the transition section and partially overlap with one another, and
the first fiber-reinforced polymer-matrix composite reinforcement elements extend along the full axial length of the transition section and partially overlap with one another and comprise additional first fiber-reinforced polymer-matrix composite reinforcement elements that extend along a partial axial length of the transition section.
3 . The shroud reinforcement assembly according to claim 1 , wherein:
the shroud comprises an additional part surrounding the transition section and the first fiber-reinforced polymer-matrix composite reinforcement elements and defines treads on which the second fiber-reinforced polymer-matrix composite reinforcement elements are seated, and
the treads are at least one of flat cylindrical steps, linearly self-locking cylindrical steps, convex self-locking cylindrical steps and concave self-locking cylindrical steps.
4 . The shroud reinforcement assembly according to claim 1 , wherein:
the shroud comprises an additional part surrounded by the transition section and the first fiber-reinforced polymer-matrix composite reinforcement elements and defines treads on which the second fiber-reinforced polymer-matrix composite reinforcement elements are seated, and
the treads are at least one of flat cylindrical steps, linearly self-locking cylindrical steps, convex self-locking cylindrical steps and concave self-locking cylindrical steps.
5 . The shroud reinforcement assembly according to claim 1 , wherein the first and second composite reinforcement elements comprise thermoset polymers or thermoplastic polymers reinforced by one or more of organic fibers, carbon fibers and glass fibers.
6 . A rotor assembly, comprising:
a shroud, which is formed of one or more of metallic and alloy materials, the shroud being coaxial with and partially surrounding a rotor and comprising tubular and flange sections and a transition section axially interposed between the tubular and flange sections; and
shroud reinforcement comprising:
first fiber-reinforced polymer-matrix composite reinforcement elements extending along an axial dimension of the rotor and being disposed to reinforce the transition section; and
second fiber-reinforced polymer-matrix composite reinforcement elements extending along a circumferential dimension of the rotor and being disposed to reinforce the transition section,
wherein the first fiber-reinforced polymer-matrix composite reinforcement elements extend along a full axial length of the transition section and do not overlap with one another.
7 . The rotor assembly according to claim 6 , wherein at least one of:
the first fiber-reinforced polymer-matrix composite reinforcement elements extend along a full axial length of the transition section and do not overlap with one another,
the first fiber-reinforced polymer-matrix composite reinforcement elements extend along the full axial length of the transition section and partially overlap with one another, and
the first fiber-reinforced polymer-matrix composite reinforcement elements extend along the full axial length of the transition section and partially overlap with one another and comprise additional first fiber-reinforced polymer-matrix composite reinforcement elements that extend along a partial axial length of the transition section.
8 . The rotor assembly according to claim 6 , wherein the shroud comprises an additional part surrounding the transition section and the first fiber-reinforced polymer-matrix composite reinforcement elements and defines treads on which the second fiber-reinforced polymer-matrix composite reinforcement elements are seated.
9 . The rotor assembly according to claim 8 , wherein the treads are at least one of flat cylindrical steps, linearly self-locking cylindrical steps, convex self-locking cylindrical steps and concave self-locking cylindrical steps.
10 . The rotor assembly according to claim 6 , wherein the shroud comprises an additional part surrounded by the transition section and the first fiber-reinforced polymer-matrix composite reinforcement elements and defines treads on which the second fiber-reinforced polymer-matrix composite reinforcement elements are seated.
11 . The rotor assembly according to claim 10 , wherein the treads are at least one of flat cylindrical steps, linearly self-locking cylindrical steps, convex self-locking cylindrical steps and concave self-locking cylindrical steps.
12 . The rotor assembly according to claim 6 , wherein the shroud comprises one or more of metallic or alloy materials, polymers and reinforced polymers.
13 . The rotor assembly according to claim 6 , wherein the first and second fiber-reinforced polymer-matrix composite reinforcement elements comprise thermoset polymers or thermoplastic polymers reinforced by one or more of organic fibers, carbon fibers and glass fibers.
14 . A method of assembling a shroud for a rotor assembly, the method comprising:
forming a shroud, which is formed of one or more of metallic and alloy materials, to be coaxial with and partially surround a rotor and comprising tubular and flange sections and a transition section axially interposed between the tubular and flange sections; and
forming a shroud reinforcement,
the forming of the shroud reinforcement comprising:
arranging first fiber-reinforced polymer-matrix composite reinforcement elements to extend along an axial dimension of the rotor and to be disposed to reinforce the transition section; and
arranging second fiber-reinforced polymer-matrix composite reinforcement elements to extend along a circumferential dimension of the rotor and to be disposed to reinforce the transition section,
wherein the arranging of the first fiber-reinforced polymer-matrix composite reinforcement elements is executed such that the first fiber-reinforced polymer-matrix composite reinforcement elements abut with an external surface of the transition section.
15 . The method according to claim 14 , wherein:
the shroud comprises one or more of metallic or alloy materials, polymers and reinforced polymers,
the first and second composite reinforcement elements comprise thermoset polymers or thermoplastic polymers reinforced by one or more of organic fibers, carbon fibers and glass fibers, and
the method further comprises one or more of curing the thermoset polymers, solidifying the thermoplastic polymers and adhering the thermoset polymers or the thermoplastic polymers.
16 . The method according to claim 14 , wherein the arranging of the first fiber-reinforced polymer-matrix composite reinforcement elements comprises at least one of:
arranging the first fiber-reinforced polymer-matrix composite reinforcement elements to extend along a full axial length of the transition section and not to overlap with one another,
arranging the first fiber-reinforced polymer-matrix composite reinforcement elements to extend along the full axial length of the transition section and to partially overlap with one another, and
arranging the first fiber-reinforced polymer-matrix composite reinforcement elements to extend along the full axial length of the transition section and to partially overlap with one another and to comprise additional first fiber-reinforced polymer-matrix composite reinforcement elements that extend along a partial axial length of the transition section.
17 . The method according to claim 14 , wherein:
the method further comprises surrounding the transition section with an additional part defining treads, and
the arranging of the second fiber-reinforced polymer-matrix composite reinforcement elements comprises seating the second fiber-reinforced polymer-matrix composite reinforcement elements on the treads.
18 . The method according to claim 17 , wherein the treads are at least one of flat cylindrical steps, linearly self-locking cylindrical steps, convex self-locking cylindrical steps and concave self-locking cylindrical steps.
19 . The method according to claim 14 , wherein:
the method further comprises surrounding an additional part by the transition section and the first fiber-reinforced polymer-matrix composite reinforcement elements, the additional part defining treads on which the second fiber-reinforced polymer-matrix composite reinforcement elements are seated.
20 . The method according to claim 19 , wherein the treads are at least one of flat cylindrical steps, linearly self-locking cylindrical steps, convex self-locking cylindrical steps and concave self-locking cylindrical steps.