Stowed blade active restraint
US-2021094683-A1 · Apr 1, 2021 · US
US11814153B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11814153-B2 |
| Application number | US-202117552052-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 15, 2021 |
| Priority date | Dec 15, 2021 |
| Publication date | Nov 14, 2023 |
| Grant date | Nov 14, 2023 |
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Official abstract text for this publication.
A system for retaining a folded proprotor blade in flight. The system includes a mounting plate, a first arm coupled to the mounting plate at an acute angle relative to the mounting plate, and a first deformable pad affixed to the first arm and adapted to contact the folded proprotor blade.
Opening claim text (preview).
What is claimed is: 1. A system for retaining a folded proprotor blade in flight, the system comprising: a mounting plate; a first arm coupled to the mounting plate at an acute angle relative to the mounting plate; and a first deformable pad affixed to the first arm and adapted to contact the folded proprotor blade. 2. The system of claim 1 , wherein the first deformable pad is preloaded to facilitate proprotor blade retention. 3. The system of claim 1 , wherein the first deformable pad is contoured to mate with the folded proprotor blade. 4. The system of claim 1 , wherein the first deformable pad comprises at least one of TEFLON, open-cell foam, closed-cell foam, rubber, and NEOPRENE. 5. The system of claim 1 , comprising a second arm positioned opposite the first arm in a beamwise direction and coupled to the mounting plate at an acute angle relative to the mounting plate. 6. The system of claim 5 , comprising a second deformable pad affixed to the second arm and adapted to contact the folded proprotor blade. 7. The system of claim 6 , wherein the first arm and the second arm are symmetrical about a chordwise-direction axis. 8. A system for retaining a folded proprotor blade in flight, the system comprising: a mounting plate; a first pair of opposing arms coupled to the mounting plate; and a deformable roller rotatably coupled to each of the first pair of opposing arms and adapted to rollably contact the folded proprotor blade. 9. The system of claim 8 , wherein the deformable rollers are spring-loaded to facilitate proprotor blade retention. 10. The system of claim 9 , wherein the deformable rollers are spring-loaded by the mounting plate. 11. The system of claim 8 , wherein the deformable rollers comprise at least one of TEFLON, open-cell foam, closed-cell foam, rubber, and NEOPRENE. 12. The system of claim 8 , comprising a second pair of opposing arms coupled to the mounting plate and to the deformable rollers at an opposite end of the deformable rollers. 13. The system of claim 12 , wherein each of the first pair of opposing arms and the second pair of opposing arms comprises a tapered surface on a leading edge thereof. 14. The system of claim 8 , wherein each of the first pair of opposing arms has an adjustment slot formed therein to adjust the deformable rollers in a chordwise direction. 15. A system for retaining a folded proprotor blade in flight, the system comprising: a mounting plate; a first arm coupled to at least one of the mounting plate at a first acute angle relative to the mounting plate; a second arm coupled to at least one of the mounting plate at a second acute angle relative to the mounting plate; a first deformable pad affixed to the first arm and adapted to contact a first side of the folded proprotor blade; a second deformable pad affixed to the second arm and adapted to contact a second side of the folded proprotor blade; and wherein the first side and the second side are on opposite sides of the folded proprotor blade in a beamwise direction. 16. The system of claim 15 , wherein the first deformable pad and the second deformable pad are preloaded to facilitate proprotor blade retention. 17. The system of claim 15 , wherein the first deformable pad and the second deformable pad are contoured to mate with the folded proprotor blade. 18. The system of claim 15 , wherein the first deformable pad and the second deformable pad comprise at least one of TEFLON, open-cell foam, closed-cell foam, rubber, and NEOPRENE. 19. The system of claim 15 , wherein each of the first arm and the second arm has an adjustment slot formed therein to adjust the first deformable pad and the second deformable pad in a chordwise direction. 20. The system of claim 15 , wherein the first acute angle is different from the second acute angle.
Collapsible or foldable blades · CPC title
Blade mountings · CPC title
with forward-propulsion propellers pivotable to act as lifting rotors · CPC title
the propellers being tiltable relative to the fuselage · CPC title
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