Title:
WING DEPLOYMENT MECHANISM
Document Type and Number:
WIPO Patent Application WO/2020/022972
Kind Code:
A3
Abstract:
Invention relates to a wing folding mechanism for a pair of wings comprising a lower wing (5) and a co-operative upper wing (6) extending opposite to each other in a deployment position and approach each other when rotated from respective remote ends to a resting position. According to the invention, a spherical rolling element slots (10) is adapted to receive a number of uniform spherical rolling elements provided at a corresponding lower wing root (20) and a upper wing root (21) so that allowing lower wing (5) and upper wing (6) extending symmetrical to each other; plurality of spherical rolling elements (3) are disposed at the spherical rolling element slot (10); an alignment element(2) is positioned in coaxially with a wing pin hole (18) and linear energy storage element (4) arranged in a such manner that release the stored energy accrued during the folding of the wings and disposed around the alignment element (2) to exert a pressing force to the upper wing (6).
Inventors:
UZUN CAN (TR)
Application Number:
PCT/TR2018/000124
Publication Date:
February 27, 2020
Filing Date:
December 24, 2018
Export Citation:
Assignee:
ROKETSAN ROKET SANAYII TICARET A S (TR)
International Classes:
B64C3/56; B64C11/28; B64C39/02
Domestic Patent References:
| WO2016196277A1 | 2016-12-08 |
Foreign References:
| US20120280080A1 | 2012-11-08 | |||
| CN105799915A | 2016-07-27 |
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