Gas turbine engine with composite airfoil and method of forming
A gas turbine engine includes a fan section, a compressor section, combustor section, and turbine section in serial flow arrangement, and defines an engine centerline extending a forward to an aft. A composite airfoil, provided in one of the fan section, the compressor section, or the turbine section can have a balanced mass distribution. A woven core defines a first mass distribution. A set of plies coupled to the woven core collectively defines a second mass distribution, where the second mass distribution is nearer to the balanced mass distribution than the first mass distribution.
1 . A gas turbine engine comprising:
a fan section, a compressor section, a combustion section, and a turbine section in serial flow arrangement, and defining an engine centerline extending between a forward direction and an aft direction; and
at least one composite airfoil provided in one of the fan section, the compressor section, or the turbine section and rotatable about the engine centerline, the at least one composite airfoil having a balanced mass distribution defining a balanced center of mass aligned with a balanced center of rotation defined relative to the engine centerline, with the at least one composite airfoil comprising:
a woven core defining a first mass distribution having a first center of rotation;
a set of plies, coupled to the woven core, and defining a second mass distribution; and
a skin layer provided exterior of the set of plies and the woven core;
wherein the combination of the first mass distribution and the second mass distribution collectively defines a combined mass distribution that is nearer to the balanced center of rotation than the first center of rotation.
2 . The gas turbine engine of claim 1 , wherein the combined mass distribution defines a combined center of rotation that aligns with the balanced center of rotation.
3 . The gas turbine engine of claim 1 , wherein the woven core is made from a raw material that defines the first mass distribution differing from the balanced mass distribution.
4 . The gas turbine engine of claim 3 , wherein the raw material includes material properties defining the first mass distribution that differs from the balanced mass distribution.
5 . The gas turbine engine of claim 3 , wherein the at least one composite airfoil comprises multiple composite airfoils, and wherein the raw material defines the first mass distribution that is common among the multiple composite airfoils that commonly differ from the balanced mass distribution.
6 . The gas turbine engine of claim 1 , wherein the combined mass distribution defines a combined center of mass and a combined center of rotation, wherein the combined center of mass aligns with the balanced center of rotation relative to the engine centerline.
7 . The gas turbine engine of claim 6 , wherein the combined center of rotation is aligned with the balanced center of rotation.
8 . The gas turbine engine of claim 6 , wherein the combined center of mass is aligned with the balanced center of mass.
9 . The gas turbine engine of claim 1 , wherein the first mass distribution defines a first center of mass that corresponds to a first center of rotation relative to the engine centerline,
wherein the second mass distribution defines a second center of mass that corresponds to a second center of rotation relative to the engine centerline, and
wherein the first center of rotation is spaced from the second center of rotation.
10 . The gas turbine engine of claim 1 , wherein the woven core is a cured woven core that defines a cured mass distribution having a cured center of mass and a cured center of rotation.
11 . The gas turbine engine of claim 10 , wherein the cured mass distribution varies from the first mass distribution by a variation between the first center of mass and the cured center of mass or by a variation between the first center of rotation and the cured center of rotation.
12 . A composite airfoil for a gas turbine engine, the composite airfoil defining a balanced mass distribution including a balanced center of mass aligned with a balanced center of rotation, the composite airfoil comprising:
a woven core defining a first mass distribution having a first center of rotation;
a set of plies, coupled to the woven core, and defining a second mass distribution; and
a skin layer provided exterior of the set of plies and the woven core;
wherein the combination of the first mass distribution and the second mass distribution collectively defines a combined mass distribution that is nearer to the balanced center of rotation than the first center of rotation.
13 . The composite airfoil of claim 12 , wherein the combined mass distribution defines a combined center of rotation that aligns with the balanced center of rotation.
14 . The composite airfoil of claim 12 , wherein the woven core is made from a raw material that defines the first mass distribution differing from the balanced mass distribution.
15 . The composite airfoil of claim 12 , wherein the combined mass distribution defines a combined center of mass and a combined center of rotation, wherein the combined center of mass aligns with the balanced center of rotation.
16 . A method of forming a composite airfoil having a balanced mass distribution defining a balanced center of mass aligned with a balanced center of rotation arranged along a rotational axis for a gas turbine engine, the method comprising: forming a woven core defining a first mass distribution having a first center of rotation; and applying a set of plies to the woven core, the set of plies defining a second mass distribution; adding a skin layer exterior of the set of plies and the woven core, wherein the first mass distribution and the second mass distribution collectively define a combined mass distribution that is nearer to the balanced center of rotation than the first center of rotation.
17 . The method of claim 16 , wherein forming the woven core further comprises forming the woven core from a raw material defining the first mass distribution.
18 . The method of claim 17 , wherein the raw material includes material properties defining the first mass distribution that differs from the balanced mass distribution.
19 . The method of claim 16 , further comprising measuring the woven core to determine the first mass distribution.
20 . The method of claim 19 , further comprising comparing the first mass distribution to the balanced mass distribution to define an unbalanced mass distribution.