Invention Grant
- Patent Title: Stress reducing holes
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Application No.: US15756777Application Date: 2016-09-13
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Publication No.: US10703468B2Publication Date: 2020-07-07
- Inventor: Krzysztof Kopanski , Justin Thomas
- Applicant: Sikorsky Aircraft Corporation
- Applicant Address: US CT Stratford
- Assignee: SIKORSKY AIRCRAFT CORPORATION
- Current Assignee: SIKORSKY AIRCRAFT CORPORATION
- Current Assignee Address: US CT Stratford
- Agency: Cantor Colburn LLP
- International Application: PCT/US2016/051459 WO 20160913
- International Announcement: WO2017/048683 WO 20170323
- Main IPC: B64C27/473
- IPC: B64C27/473

Abstract:
A blade includes a blade body having a surface and a hole extending through the surface of the blade body. The hole defines a hole axis and a plane perpendicular to the hole axis. The hole has an elongated hole perimeter within the plane. The hole perimeter includes a plurality of non-linear perimeter sections to minimize stress concentration around the elongated hole perimeter while maximizing the usable opening area. A rotor system includes a rotor hub and a blade as recited above. The blade extends radially outward from the rotor hub. The blade defines a root end proximate to the rotor hub, a tip end opposite the root end.
Public/Granted literature
- US20180237133A1 STRESS REDUCING HOLES Public/Granted day:2018-08-23
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