Invention Application
- Patent Title: Seal Air Buffer and Oil Scupper System and Method
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Application No.: US17085153Application Date: 2020-10-30
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Publication No.: US20220136407A1Publication Date: 2022-05-05
- Inventor: Enzo DiBenedetto
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Main IPC: F01D25/18
- IPC: F01D25/18 ; F02C7/28 ; F02C7/06

Abstract:
A turbine engine strut stage extends through gaspath upstream of a guide vane stage. A carbon seal system seals a bearing compartment and has: a carbon seal mounted to the case and a seal runner on the spool; and a seal carrier carrying the carbon seal. The engine passes buffer air along a buffer air supply path internally through one or more first struts of the stage of struts. The engine drains oil along an oil drain path internally through one or more second struts of the stage of struts.
Public/Granted literature
- US11459911B2 Seal air buffer and oil scupper system and method Public/Granted day:2022-10-04
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