Zero-fastener flushmount balance weight system preserving rotor-blade tip with integral tuning weight retention feature
The present invention includes a balancing system that includes a weight box, mounted substantially within the rotor-blade spar, flush with a rotor-blade spar outer surface, operably accessible from a rotor-blade tip, and retained within the rotor-blade spar by a weight-box retention pin, one or more weight-box contact surfaces bonded to a rotor-blade-spar inner surface, or a weight-box lip providing a bearing contact with an edge of a spar rotor-blade spar cutout; and a weight package attached to the weight box, the weight package including a weight-box cover, two or more weight guide-rods attached to the weight-box cover, wherein one of the two or more weight guide-rods is positioned forward of a pitch change axis or center of twist and wherein one of the two weight guide-rods is positioned aft of the pitch change axis or center of twist, and one or more balance weights mounted on the weight guide-rods.
1. A balancing system, comprising:
a weight box, the weight box comprising a weight-box retention pin, the weight box mounted substantially within a rotor-blade spar, flush with a spar outer surface of the rotor-blade spar, operably accessible from a rotor-blade tip, and retained within the rotor-blade spar by:
the weight-box retention pin inserted through a forward wall of the rotor-blade spar, the weight box, and an aft wall of the rotor-blade spar,
one or more weight-box contact surfaces bonded to an upper inner surface of the rotor-blade spar or a lower inner surface of the rotor-blade spar, and
a weight-box lip positioned to provide a bearing contact with an edge of a spar cutout of the rotor-blade spar; and
a weight package attached to the weight box, the weight package comprising:
a weight-box cover attached to the weight box;
two or more weight guide-rods attached to the weight-box cover, wherein one of the two or more weight guide-rods is positioned forward of a pitch change axis or a center of twist and wherein one of the two or more weight guide-rods is positioned aft of the pitch change axis or the center of twist; and
one or more balance weights mounted on at least one of the two or more weight guide-rods.
2. The system of claim 1 , further comprising one or more weight-retention devices mounted on at least one of the two or more weight guide-rods to retain the one or more balance weights on the at least one of the two or more weight guide-rods.
3. The system of claim 2 , wherein the one or more weight-retention devices are interference-fit to the one or more balance weights.
4. The system of claim 1 , further comprising one or more pin spacers positioned near the weight-box retention pin and between the forward wall of the rotor-blade spar and the weight-box or the aft wall of the rotor-blade spar and the weight box.
5. The system of claim 1 , wherein the weight-box cover is attached to the weight box with one or more weight-package retention devices.
6. The system of claim 5 , wherein the one or more weight-package retention devices are interference-fit to the weight-box cover.
7. The system of claim 1 , wherein the two or more weight guide-rods, each weight guide-rod having a threaded tip portion and a non-threaded shank portion or is threaded for substantially its entire length.
8. The system of claim 1 , wherein the one or more balance weights comprise one or more span-balance weights or one or more dynamic-balance weights.
9. The system of claim 8 , wherein the one or more span-balance weights are mounted on the two or more weight guide-rods on an inboard side of the weight-box cover.
10. The system of claim 9 , wherein the one or more span-balance weights are shaped to substantially fill an interior space of the weight box from a weight-box upper inner surface to a weight-box lower inner surface and from a weight-box forward inner surface to a weight-box aft inner surface.
11. The system of claim 8 , wherein the one or more dynamic-balance weights are mounted on the two or more weight guide-rods on an outboard side of the weight-box cover.
12. The system of claim 1 , wherein the weight package further comprises one or more lightweight spacers mounted on at least one of the two or more weight guide-rods.
13. The system of claim 1 , wherein the one or more balance weights are operably configurable to substantially provide span balance or chord balance.
14. The system of claim 1 , wherein the weight-box retention pin locates or retains a leading-edge tuning weight.
15. The system of claim 1 , wherein the weight-box retention pin locates a blade core.
16. The system of claim 1 , wherein the rotor-blade spar is a main rotor-blade spar, a tail rotor-blade spar, a proprotor blade spar, a propeller blade spar, or a wind-turbine blade spar.
17. A rotor system, comprising:
at least one rotor blade;
a rotor-blade spar inside the at least one rotor blade;
a weight box, the weight box comprising a weight-box retention pin, the weight box mounted substantially within the rotor-blade spar, flush with a spar outer surface of the rotor-blade spar, operably accessible from a rotor-blade tip, and retained within the rotor-blade spar by:
the weight-box retention pin inserted through a forward wall of the rotor-blade spar, the weight box, and an aft wall of the rotor-blade spar,
one or more weight-box contact surfaces bonded to an upper inner surface of the rotor-blade spar or a lower inner surface of the rotor-blade spar, and
a weight-box lip positioned to provide a bearing contact with an edge of a spar cutout of the rotor-blade spar; and
a weight package attached to the weight box, the weight package comprising:
a weight-box cover attached to the weight box;
two or more weight guide-rods attached to the weight-box cover, wherein one of the two or more weight guide-rods is positioned forward of a pitch change axis or a center of twist and wherein one of the two or more weight guide-rods is positioned aft of the pitch change axis or the center of twist; and
one or more balance weights mounted on at least one of the two or more weight guide-rods.
18. The rotor system of claim 17 , further comprising one or more weight-retention devices mounted on at least one of the two or more weight guide-rods to retain the one or more balance weights on the at least one of the two or more weight guide-rods.
19. A method of balancing weights in a rotor system, comprising:
inserting a weight box substantially within a rotor-blade spar of a rotor blade, flush with a spar outer surface of the rotor-blade spar, and operably accessible from a rotor-blade tip;
retaining the weight box within the rotor-blade spar by:
bonding one or more weight-box contact surfaces to an upper inner surface of the rotor-blade spar or a lower inner surface of the rotor-blade spar,
using a bearing contact between a weight-box lip of the weight box and an edge of a spar cutout, and
inserting a weight-box retention pin through a forward wall of the rotor-blade spar, the weight box, and an aft wall of the rotor-blade spar;
arranging one or more balance weights in a weight package;
retaining the one or more balance weights in the weight package; and
attaching the weight package to the weight box.
20. The method of claim 19 , wherein the weight package comprises a weight-box cover; and
the arranging the one or more balance weights in the weight package further comprises:
attaching two or more weight guide-rods to the weight-box cover, attaching one of the two or more weight guide-rods forward of a pitch change axis or a center of twist and attaching one of the two or more weight guide-rods aft of the pitch change axis or the center of twist; and
arranging the one or more balance weights on the two or more weight guide-rods.
21. The method of claim 19 , further comprising arranging the one or more balance weights, wherein the one or more balance weights comprise one or more span-balance weights.
22. The method of claim 19 , further comprising arranging the one or more balance weights, wherein the one or more balance weights comprise one or more dynamic-balance weights.
23. The method of claim 19 , further comprising retaining the one or more balance weights in the weight package with one or more retention devices interference-fit to the one or more balance weights.
24. The method of claim 19 , further comprising attaching the weight package to the weight box with one or more retention devices interference-fit to the weight.
25. The method of claim 19 , wherein the arranging the one or more balance weights in the weight package comprises arranging the one or more balance weights for span balancing the rotor system or arranging the one or more balance weights for chord balancing the rotor blade.
26. The method of claim 19 , further comprising locating or retaining a leading-edge tuning weight with the weight-box retention pin.
27. The method of claim 19 , further comprising locating a blade core with the weight-box retention pin.
28. The method of claim 19 , further comprising inserting the weight box and the weight package substantially inside the rotor-blade spar, wherein the rotor-blade spar is a main rotor-blade spar, a tail rotor-blade spar, a proprotor blade spar, a propeller blade spar, or a wind-turbine blade spar.
29. A rotorcraft, comprising:
a fuselage;
one or more engines coupled to the fuselage; and
one or more rotor systems coupled to the one or more engines, each rotor system of the one or more rotor systems comprising at least one rotor blade comprising:
a rotor-blade spar inside the at least one rotor blade;
a weight box, the weight box comprising a weight-box retention pin, the weight box mounted substantially within the rotor-blade spar, flush with a spar outer surface of the rotor-blade spar, operably accessible from a rotor-blade tip, and retained within the rotor-blade spar by:
the weight-box retention pin inserted through a forward wall of the rotor-blade spar, the weight box, and an aft wall of the rotor-blade spar,
one or more weight-box contact surfaces bonded to an upper inner surface of the rotor-blade spar or a lower inner surface of the rotor-blade spar, and
a weight-box lip positioned to provide a bearing contact with an edge of a spar cutout of the rotor-blade spar; and
a weight package attached to the weight box, the weight package comprising:
a weight-box cover attached to the weight box;
two or more weight guide-rods attached to the weight-box cover, wherein one of the two or more weight guide-rods is positioned forward of a pitch change axis or a center of twist and wherein one of the two or more weight guide-rods is positioned aft of the pitch change axis or the center of twist; and
one or more balance weights mounted on at least one of the two or more weight guide-rods.
30. The rotorcraft of claim 29 , further comprising one or more weight-retention devices mounted on at least one of the two or more weight guide-rods to retain the one or more balance weights on the at least one of the two or more weight guide-rods.