Spring damping for bearing compartment
According to an aspect, a bearing compartment includes a housing integrally formed with a spring configured to deform in response to a force. The housing includes an overhang region that is supported by the spring during an additive manufacturing build process. The spring includes a plurality of struts that extend axially within the housing.
1. A bearing compartment comprising:
a housing including a lower portion and an upper portion extending from the lower portion, wherein the housing is integrally formed with a spring configured to deform in response to a force, wherein the lower portion includes the spring radially inward of the housing, wherein the upper portion comprises an overhang region that is supported by and integrally formed with the spring, the spring comprises a plurality of struts that extend axially within the housing, and the spring comprises a shell with an internal lattice structure within the struts.
2. The bearing compartment of claim 1 , wherein the spring is a squirrel cage spring, and a centerline of the struts extends axially in parallel to an axis of rotation defined within a central cavity of the bearing compartment.
3. The bearing compartment of claim 1 , wherein the shell comprises one of more weep holes that allow additive manufacturing powder to be removed from within the internal lattice structure.
4. The bearing compartment of claim 3 , wherein the internal lattice structure is a triply periodic minimal surfaces structure comprising a gyroid.
5. The bearing compartment of claim 1 , wherein two or more of the struts are canted.
6. The bearing compartment of claim 1 , wherein the spring comprises a keyway.
7. A gas turbine engine comprising:
a compressor section;
a turbine section;
a shaft coupled to the compressor section and the turbine section; and
a bearing system configured to support rotation of the shaft, the bearing system comprising a bearing compartment having a housing including a lower portion and an upper portion extending from the lower portion, wherein the housing is integrally formed with a spring configured to deform in response to a force, wherein the lower portion includes the spring radially inward of the housing, wherein the upper portion comprises an overhang region that is supported by and integrally formed with the spring, the spring comprises a plurality of struts that extend axially within the housing, and the spring comprises a shell with an internal lattice structure within the struts.
8. The gas turbine engine of claim 7 , wherein the spring is a squirrel cage spring, and a centerline of the struts extends axially in parallel to an axis of rotation of the shaft within a central cavity of the bearing compartment.
9. The gas turbine engine of claim 7 , wherein the shell comprises one of more weep holes that allow additive manufacturing powder to be removed from within the internal lattice structure.
10. The gas turbine engine of claim 9 , wherein the internal lattice structure is a triply periodic minimal surfaces structure comprising a gyroid.
11. The gas turbine engine of claim 7 , wherein two or more of the struts are canted.
12. The gas turbine engine of claim 7 , wherein the spring comprises a keyway to support positioning one or more other components of the bearing compartment.
13. A method of manufacturing a bearing compartment, the method comprising:
additively manufacturing a lower portion of a housing of the bearing compartment including a spring radially inward of the housing;
additively manufacturing a plurality of struts of the spring to extend axially within the housing; and
additively manufacturing an upper portion of the housing extending from the lower portion, the upper portion including an overhang region that is integrally formed with the spring, and the spring comprises a shell with an internal lattice structure within the struts.
14. The method of claim 13 , wherein the spring is additively manufactured as a squirrel cage spring, and a centerline of the struts extends axially in parallel to an axis of rotation defined within a central cavity of the bearing compartment.
15. The method of claim 13 , wherein the shell comprises one of more weep holes that allow additive manufacturing powder to be removed from within the internal lattice structure, and the internal lattice structure is a triply periodic minimal surfaces structure comprising a gyroid.
16. The method of claim 13 , wherein two or more of the struts are canted.
17. The method of claim 13 , wherein the spring comprises a keyway.