Invention Grant
- Patent Title: Fan assembly of a gas turbine engine with a tip shroud
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Application No.: US15812331Application Date: 2017-11-14
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Publication No.: US10584714B2Publication Date: 2020-03-10
- Inventor: Jason Husband , James Glaspey
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F01D5/22
- IPC: F01D5/22 ; F04D29/32 ; F02K3/06 ; F04D19/00 ; F04D29/66
Abstract:
A fan of a gas turbine engine is provided. The fan having: a plurality of fan blades secured to a rotor, each of the plurality of fan blades having an airfoil secured to the rotor at one end and a tip portion that is secured to a shroud that circumscribes the plurality of fan blades.
Public/Granted literature
- US10724535B2 Fan assembly of a gas turbine engine with a tip shroud Public/Granted day:2020-07-28
Information query
