Invention Grant
- Patent Title: Composite blade root structure
- Patent Title (中): 复合叶片根结构
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Application No.: US12397833Application Date: 2009-03-04
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Publication No.: US07972114B2Publication Date: 2011-07-05
- Inventor: Neil Gupta , Abe Karem
- Applicant: Neil Gupta , Abe Karem
- Applicant Address: US CA Lake Forest
- Assignee: Karem Aircraft, Inc.
- Current Assignee: Karem Aircraft, Inc.
- Current Assignee Address: US CA Lake Forest
- Agency: Fish & Associates, PC
- Main IPC: B64C11/24
- IPC: B64C11/24

Abstract:
A spar of a rotor blade having moderate depth transitions to a relatively much deeper shank over a relatively short distance. This rapid transition enables a low-weight blade root that is structurally efficient, offers a high moment capability, and enables high Mach number axial flow. A transition could advantageously reduce section depth by at least 15%, 20%, 30%, or even 40% over at most 5%, 6%, 10%, or 12% of a total length of the rotor blade. Such a transition could advantageously be accomplished using a cuff, which has interfaces with each of the spar and the shank. The rotor blade shank has a generally circular cross-section which allows for a rotary attachment to a hub, where the attachment may advantageously comprise a mechanical or elastomeric bearing. Preferred embodiments have a spar with a generally rectangular cross-section.
Public/Granted literature
- US20090226325A1 Composite Blade Root Structure Public/Granted day:2009-09-10
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