Invention Grant
- Patent Title: Flared anti-vortex tube rotor insert
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Application No.: US15927659Application Date: 2018-03-21
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Publication No.: US10774742B2Publication Date: 2020-09-15
- Inventor: Konstantinos Panagiotis Giannakopoulos , Erica J. Harvie
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F04D29/32
- IPC: F04D29/32 ; F02C6/08 ; F01D5/08

Abstract:
A compressor rotor includes a first disk and a conical section connected to the first disk. The conical section includes at least one flow hole. A bore cavity is defined between the conical section and the first disk. The bore cavity is arranged in fluid communication with the at least one flow hole. An anti-vortex tube is disposed within the at least one flow hole of the conical section and includes at least one feature arranged in contact with a surface of the conical section to restrict movement of the anti-vortex tube out of engagement with the conical section.
Public/Granted literature
- US20190292981A1 FLARED ANTI-VORTEX TUBE ROTOR INSERT Public/Granted day:2019-09-26
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