Invention Application
- Patent Title: VORTEX TUBE PARTICLE SEPARATORS WITH COATINGS FOR REBOUND CONTROL
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Application No.: US18371812Application Date: 2023-09-22
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Publication No.: US20250101914A1Publication Date: 2025-03-27
- Inventor: James C. Loebig
- Applicant: Rolls-Royce North American Technologies Inc.
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee Address: US IN Indianapolis
- Main IPC: F02C7/052
- IPC: F02C7/052 ; B01D45/16 ; B04C3/00

Abstract:
A vortex particle separator adapted for use with a gas turbine engine includes a vortex tube, a plurality of swirl vanes, and an outlet tube. The vortex tube receives atmospheric air laden with particles. The plurality of swirl vanes are arranged within the vortex tube and separate the atmospheric air into a first flow of air having the particles and a second flow of air that is relatively free of the particles. The outlet tube extends into the vortex tube to define a scavenge passageway between the outlet tube and the vortex tube that receives the first flow of air. The outlet tube defines an intake passageway that receives the second flow of air. The vortex particle separator further includes a layer of material having a low coefficient of restitution on at least one of an interior surface of the vortex tube and a surface of the swirl vanes.
Public/Granted literature
- US12258903B1 Vortex tube particle separators with coatings for rebound control Public/Granted day:2025-03-25
Information query
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