Helicopter blade folding with blade droop
AssigneeDavis Aircraft Products Co., Inc.
InventorBruce T. Davis
Life of this patent
Estimating the term…
Abstract
Blade fold hinge units are attachable between each helicopter blade and its hub attachment point, while maintaining continuity of mechanical connection of each blade to its hub portion. A two portion hinge unit has a first portion for blade attachment and a second portion for hub attachment. The first and second portions are hinged via a transverse pin to enable blade drooping downward, before or after a blade is pivoted to an aft position for helicopter storage or shipment. Upon aft pivoting of a blade, undesired further pivoting or knuckling of the hinge unit relative to the hub is prevented by addition of a lock link. After blade folding, the blades may be suitably fixed in position adjacent the aft portion of the helicopter body.
Claims15
A blade fold hinge unit, usable with a helicopter blade attached to a blade support via two blade pins, to enable blade folding with removal of both said blade pins while retaining blade connection continuity, comprising:
- a first portion configured for pivotal attachment to the blade via a first pin positionable in alignable apertures in said first portion and the blade upon removal of one said blade pin;
- a second portion configured for pivotal attachment to the blade support via a second pin positionable in alignable apertures in said second portion and the blade support upon removal of said one blade pin;
- a hinge pin positioned in aligned apertures in said first and second portions to pivotally hinge the first portion to the second portion, the center line of the hinge pin extending transversely to the insertion axes of said first and second pins;
- and
- a restraining strut of length suitable for connection between apertures in said blade and said blade support after said other blade pin has been removed therefrom and subsequent to movement of the blade to a folded position;
- the blade fold hinge unit configured to enable attachment between the blade and blade support upon removal of said one blade pin and to maintain connection continuity of the blade to the blade support via said hinge unit upon removal of the other said blade pin for blade folding.
A blade fold hinge unit, usable with a helicopter blade attached to a blade support via two blade pins to enable blade folding with blade droop, comprising:
- a first portion configured for pivotal attachment to the blade via a first pin positionable in alignable apertures in said first portion and the blade upon removal of one said blade pin;
- a second portion configured for pivotal attachment to the blade support via a second pin positionable in alignable apertures in said second portion and the blade support upon removal of said one blade pin;
- a hinge pin positioned in aligned apertures in said first and second portions to pivotally hinge the first portion to the second portion, to permit the free end of the blade to move downward to a drooped position;
- a lock link of length suitable for contact with said second portion to restrain its pivotal displacement relative to the blade support subsequent to movement of the blade to a folded positions;
- and
- a lock link pin, insertable into the blade support in the former position of the other said blade pin after removal thereof, to maintain the lock link in position.
A method for folding and drooping a helicopter blade attached to a blade support via two blade pins, with removal of both said pins while retaining blade connection continuity, comprising the steps of:
- (a) removing one said blade pin from first apertures in the blade and first apertures in the blade support, so the blade can be rotated forward;
- (b) attaching a first portion of a hinge unit to the blade via a pin positioned in said first apertures in the blade;
- (c) attaching a second portion of the hinge unit to the blade support via a pin positioned in said first apertures in the blade support;
- (d) removing the other said blade pin from second apertures in the blade and second apertures in the blade support;
- (e) pivoting the blade to a folded position;
- (f) pivoting said first portion relative to said second portion to droop the free end of the blade downward;
- and
- (g) attaching a lock link, via a pin positioned in said second apertures in the blade support, to limit pivoting of said second portion relative to the blade support while the blade is in said folded position.
Dependencies are inferred from the claim text.