Hybrid composite flexbeam for a helicopter bearingless main rotor assembly

• US 5,431,538 A
• Filed: 07/01/1993
• Issued: 07/11/1995
• Est. Priority Date: 07/01/1993
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Schmaling, David N., Byrnes, Francis E.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): Lee, Michael S.
• Application Number:
  US08/087,826
• Time in Patent Office: 740 Days
• Field of Search: 416/134 A, 416/138, 416/141, 416/230
• US Class Current: 416/134.00A
• CPC Class Codes: B29C 70/202 arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC] B29C70/207 takes precedence
• CPC Class Codes: B64C 27/33 having flexing arms

Abstract

A hybrid composite flexbeam for a soft inplane bearingless main rotor assembly has eight spanwise regions: a hub attachment region; a first tapered region; a second tapered region; an inboard transition region; a pitch region having a cruciform configuration; an outboard transition region; a tapered outboard transition region; and a main rotor blade, torque tube attachment region. The pitch region is formed from unidirectional fiberglass plies, a 50/50 admixture of unidirectional fiberglass and graphite plies, and unidirectional graphite plies, all of which extend from root to tip of the hybrid flexbeam. Unidirectional fiberglass and graphite plies of varying lengths are interleaved in the second inboard tapered region. Fiberglass and graphite cross plies of varying lengths are interleaved in the first inboard tapered region. Fiberglass and graphite cross plies and unidirectional fiberglass plies of varying length are interleaved in the outboard tapered region. The ends of the plies of varying length form distributed ply drop-off arrangements in the first and second inboard tapered regions and the outboard tapered regions. The distributed arrangement of ply endings cause kick loads in the hybrid flexbeam to be distributed across the ply buildups. Fiberglass edge caps having a U-shaped configuration may be disposed in combination with the leading and trailing edges of the hybrid flexbeam, starting at the limits of the pitch region and extending inboardly and outboardly therefrom, respectively.

Claims

1. A hybrid composite flexbeam for a bearingless main rotor assembly, comprising:

a pitch region formed by a plurality of unidirectional fiberglass plies, a plurality of unidirectional fiberglass and graphite plies in interleaved combination, and a plurality of unidirectional graphite plies, said plurality of unidirectional graphite plies defining a cruciform configuration in cross section for said pitch region, and wherein said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, and said plurality of unidirectional graphite plies extend from root to tip of said hybrid composite flexbeam;

an inboard transition region comprised of unidirectional fiberglass plies in abutting relation with edges of said plurality of unidirectional graphite plies defining said cruciform configuration, said abutting unidirectional fiberglass plies extending inboardly to said root of said hybrid flexbeam;

a second inboard tapered region formed by a plurality of unidirectional fiberglass and graphite plies of varying lengths internally interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, and said plurality of abutting unidirectional fiberglass plies extending inboardly from said inboard transition region, said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths extending inboardly to said root of said hybrid composite flexbeam;

a first inboard tapered region formed by a plurality of fiberglass and graphite cross plies of varying lengths internally interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths, and said plurality of abutting unidirectional fiberglass plies extending inboardly from said second inboard tapered region, said plurality of internally interleaved fiberglass and graphite cross plies of varying lengths extending inboardly to said root of said hybrid composite flexbeam;

a hub attachment region formed by said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths, said plurality of internally interleaved fiberglass and graphite cross plies of varying lengths, and said plurality of abutting unidirectional fiberglass plies extending inboardly from said first inboard tapered region;

an outboard transition region comprised of unidirectional fiberglass plies in abutting relation with edges of said plurality of unidirectional graphite plies defining said cruciform configuration, said abutting unidirectional fiberglass plies extending outboardly to said tip of said hybrid flexbeam;

an outboard tapered region formed by a plurality of fiberglass and graphite cross plies and a plurality of unidirectional fiberglass plies of varying lengths interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, and said plurality of abutting unidirectional fiberglass plies extending outboardly from said outboard transition region, said plurality of internally interleaved fiberglass and graphite cross plies and said plurality of internally interleaved unidirectional fiberglass plies of varying lengths extending outboardly to said tip of said hybrid composite flexbeam; and

a torque tube, main rotor blade attachment region formed by said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, said plurality of internally interleaved fiberglass and graphite cross plies and said plurality of internally interleaved unidirectional fiberglass plies of varying lengths, and said plurality of abutting unidirectional fiberglass plies extending outboardly from said outboard tapered region.

22. The hybrid composite flexbeam of claim 1 further comprising:

a plurality of edge caps having a U-Shaped configuration disposed in combination the leading and trailing edges of said hybrid composite flexbeam, respectively, said plurality of edge caps including

a first edge cap disposed in combination with the leading edge of said hybrid composite flexbeam from the inboard limit of said pitch region into said first inboard tapered region;

a second edge cap disposed in combination with the trailing edge of said hybrid composite flexbeam from the inboard limit of said pitch region into said first inboard tapered region;

a third edge cap disposed in combination with the leading edge of said hybrid composite flexbeam from the outboard limit of said pitch region into said outboard tapered region; and

a fourth edge cap disposed in combination with the trailing edge of said hybrid composite flexbeam from the outboard limit of said pitch region into said outboard tapered region.

23. The hybrid composite flexbeam of claim 22 wherein said plurality of edge caps are formed from fiberglass.

24. The hybrid composite flexbeam of claim 23 wherein said fiberglass edge caps have fiber orientations of ±

45°

.

2. A hybrid composite flexbeam for a bearingless main rotor assembly, comprising:

a pitch region formed by a plurality of unidirectional fiberglass plies, a plurality of unidirectional fiberglass and graphite plies in interleaved combination, and a plurality of unidirectional graphite plies, said plurality of unidirectional graphite plies defining a cruciform configuration in cross section for said pitch region, and wherein said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, and said plurality of unidirectional graphite plies extend from root to tip of said hybrid composite flexbeam;

an inboard transition region comprised of unidirectional fiberglass plies in abutting relation with edges of said plurality of unidirectional graphite plies defining said cruciform configuration, said abutting unidirectional fiberglass plies extending inboardly to said root of said hybrid flexbeam;

a second inboard tapered region formed by a plurality of unidirectional fiberglass and graphite plies of varying lengths internally interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, and said plurality of abutting unidirectional fiberglass plies extending inboardly from said inboard transition region, said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths extending inboardly to said root of said hybrid composite flexbeam;

a first inboard tapered region formed by a plurality of fiberglass and graphite cross plies of varying lengths internally interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths, and said plurality of abutting unidirectional fiberglass plies extending inboardly from said second inboard tapered region, said plurality of internally interleaved fiberglass and graphite cross plies of varying lengths extending inboardly to said root of said hybrid composite flexbeam;

a hub attachment region formed by said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths, said plurality of internally interleaved fiberglass and graphite cross plies of varying lengths, and said plurality of abutting unidirectional fiberglass plies extending inboardly from said first inboard tapered region;

an outboard transition region comprised of unidirectional fiberglass plies in abutting relation with edges of said plurality of unidirectional graphite plies defining said cruciform configuration, said abutting unidirectional fiberglass plies extending outboardly to said tip of said hybrid flexbeam;

an outboard tapered region formed by a plurality of fiberglass and graphite cross plies and a plurality of unidirectional fiberglass plies of varying lengths interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, and said plurality of abutting unidirectional fiberglass plies extending outboardly from said outboard transition region, said plurality of internally interleaved fiberglass and graphite cross plies and said plurality of internally interleaved unidirectional fiberglass plies of varying lengths extending outboardly to said tip of said hybrid composite flexbeam;

a torque tube, main rotor blade attachment region formed by said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, said plurality of internally interleaved fiberglass and graphite cross plies and said plurality of internally interleaved unidirectional fiberglass plies of varying lengths, and said plurality of abutting unidirectional fiberglass plies extending outboardly from said outboard tapered region; and

a plurality of fiberglass edge caps having a U-shaped configuration disposed in combination the leading and trailing edges of said hybrid composite flexbeam, respectively, said plurality of fiberglass edge caps having fiber orientations of ±

45°

, and wherein said plurality of fiberglass edge caps include

a first fiberglass edge cap disposed in combination with the leading edge of said hybrid composite flexbeam from the outboard limit of said inboard transition region into said first inboard tapered region,

a second fiberglass edge cap disposed in combination with the trailing edge of said hybrid composite flexbeam from the outboard limit of said inboard transition region into said first inboard tapered region,

a third fiberglass edge cap disposed in combination with the leading edge of said hybrid composite flexbeam from the inboard limit of said outboard transition region into said outboard tapered region, and

a fourth fiberglass edge cap disposed in combination with the trailing edge of said hybrid composite flexbeam from the inboard limit of said outboard transition region into said outboard tapered region.

3. A hybrid composite flexbeam for a bearingless main rotor assembly, comprising:

a pitch region formed by a plurality of unidirectional fiberglass plies, a plurality of unidirectional fiberglass and graphite plies in interleaved combination, and a plurality of unidirectional graphite plies, said plurality of unidirectional graphite plies defining a cruciform configuration in cross section for said pitch region, and wherein said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, and said plurality of unidirectional graphite plies extend from root to tip of said hybrid composite flexbeam;

a second inboard tapered region formed by a plurality of unidirectional fiberglass and graphite plies of varying lengths internally interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, and said plurality of unidirectional graphite plies extending inboardly from said pitch region, said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths extending inboardly to said root of said hybrid composite flexbeam;

a first inboard tapered region formed by a plurality of fiberglass and graphite cross plies of varying lengths internally interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, and said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths extending inboardly from said second inboard tapered region, said plurality of internally interleaved fiberglass and graphite cross plies of varying lengths extending inboardly to said root of said hybrid composite flexbeam;

a hub attachment region formed by said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, aid plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths, and said plurality of internally interleaved fiberglass and graphite cross plies of varying lengths extending inboardly from said first inboard tapered region;

an outboard tapered region formed by a plurality of fiberglass and graphite cross plies and a plurality of unidirectional fiberglass plies of varying lengths interleaved in combination with said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, and said plurality of unidirectional graphite plies extending outboardly from said pitch region, said plurality of internally interleaved fiberglass and graphite cross plies and said plurality of internally interleaved unidirectional fiberglass plies of varying lengths extending outboardly to said tip of said hybrid composite flexbeam; and

a torque tube, main rotor blade attachment region formed by said plurality of unidirectional fiberglass plies, said plurality of unidirectional fiberglass and graphite plies, said plurality of unidirectional graphite plies, and said plurality of internally interleaved fiberglass and graphite cross plies and said plurality of internally interleaved unidirectional fiberglass plies of varying lengths extending outboardly from said outboard tapered region.

4. The hybrid composite flexbeam of claim 3 wherein said pitch region comprises:

a base zone formed from said plurality of unidirectional fiberglass plies, said base zone having a rectangular configuration of predetermined width in cross section;

upper and lower internal zones formed from said interleaved plurality of unidirectional fiberglass and graphite plies, said upper and lower internal zones being contiguous with said base zone;

upper and lower, left and right side zones formed from said unidirectional fiberglass plies, said upper and lower, left and right side zones being contiguous with said base zone and disposed in abutting relation with said upper and lower internal zones, respectively;

wherein said upper and lower internal zones and said upper and lower, left and right side zones in combination have a rectangular configuration of said predetermined width in cross section; and

upper and lower external zones formed from said interleaved plurality of unidirectional graphite plies, said upper and lower external zones being contiguous with said upper and lower internal zones, respectively, and wherein said upper and lower external zones have a width less than said predetermined width.

5. The hybrid composite flexbeam of claim 4 wherein said upper and lower external zones have edges defining said width thereof, and wherein said edges have a parabolic fillet configuration.

6. The hybrid composite flexbeam of claim 5 further comprising an inboard transition region intermediate said pitch region and said second inboard tapered region, said inboard transition region being formed from unidirectional fiberglass plies to define upper and lower, left and right transition zones contiguous with said upper and lower, left and right side zones and said upper and lower internal zones, respectively, said upper and lower, left and right transition zones having edges having a configuration complementary to parabolic fillet edges of said upper and lower external zones wherein said edges of said upper and lower, left and right transition zones butt against said parabolic fillet edges of said upper and lower external zones, respectively.

7. The hybrid composite flexbeam of claim 6 wherein said second inboard tapered region further comprises first and second pluralities of full width plies of unidirectional fiberglass superposed upon the upper and lower external surfaces, respectively, of said second inboard tapered region, to form upper and lower surface zones, respectively, that effectively bury said upper and lower external zones and said upper and lower, left and right transition zones, respectively, said first and second superposed pluralities of full width unidirectional fiberglass plies extending inboardly to said root of said hybrid composite flexbeam.

8. The hybrid composite flexbeam of claim 5 further comprising an outboard transition region intermediate said pitch region and said second inboard tapered region, said outboard transition region being formed from unidirectional fiberglass plies to define upper and lower, left and right transition zones contiguous with said upper and lower, left and right side zones and said upper and lower internal zones, respectively, said upper and lower, left and right transition zones having edges having a configuration complementary to said parabolic fillet edges of said upper and lower external zones wherein said edges of said upper and lower, left and right transition zones butt against said parabolic fillet edges of said upper and lower external zones, respectively.

9. The hybrid composite flexbeam of claim 4 wherein said upper and lower internal zones have edges having a parabolic fillet configuration, and further wherein said upper and lower, left and right side zones have edges having a configuration complementary to said parabolic fillet configuration of said upper and lower internal zones wherein said edges of said upper and lower, left and right side zones butt against said parabolic fillet edges of said upper and lower internal zones, respectively.

10. The hybrid composite flexbeam of claim 4 wherein said interleaved plurality of unidirectional fiberglass and graphite plies forming said upper and lower internal zones are interleaved in an alternating arrangement of unidirectional fiberglass and graphite plies.

11. The hybrid composite flexbeam of claim 3 wherein said internally interleaved unidirectional fiberglass and graphite plies forming the second inboard tapered region comprise:

left and right spanwise side strips of unidirectional fiberglass; and

central spanwise strips of unidirectional fiberglass and unidirectional graphite;

said left and right spanwise side strips butting against said corresponding central spanwise strips.

12. The hybrid composite flexbeam of claim 11 wherein said central spanwise strips of unidirectional fiberglass and unidirectional graphite are interleaved in an alternating arrangement of unidirectional fiberglass and unidirectional graphite.

13. The hybrid composite flexbeam of claim 3 wherein said first inboard tapered region includes first, second, and third transition segments wherein fiberglass cross plies of said plurality of internally interleaved fiberglass cross plies are uniformly internally interleaved in said first transition segment, fiberglass and graphite cross plies of said plurality of internally interleaved fiberglass and graphite cross plies are uniformly internally interleaved in said second transition segment, and first and second sets of graphite cross plies of said plurality of internally interleaved graphite cross plies are uniformly internally interleaved in distinct portions of said third transition segment.

14. The hybrid composite flexbeam of claim 13 wherein:

ply endings of said fiberglass cross plies uniformly internally interleaved in said first transition segment form a distributed ply drop-off arrangement therein;

ply endings of said fiberglass and graphite cross plies uniformly internally interleaved in said second transition segment form a distributed ply drop-off arrangement therein; and

ply endings of said first and second sets of said graphite cross plies uniformly interleaved in said distinct portions of said third transition segment form first and second distributed ply drop-off arrangements therein, respectively.

15. The hybrid composite flexbeam of claim 3 wherein said outboard tapered region includes fourth, fifth, sixth, and seventh transition segments wherein fiberglass cross plies of said plurality of internally interleaved fiberglass cross plies are uniformly internally interleaved in said fourth transition segment, fiberglass and graphite cross plies of said plurality of internally interleaved fiberglass and graphite cross plies are uniformly internally interleaved in said fifth transition segment, graphite cross plies of said plurality of internally interleaved graphite cross plies are uniformly internally interleaved in said six transition segment, and said plurality of internally interleaved unidirectional fiberglass plies are uniformly internally interleaved in said fifth transition segment.

16. The hybrid composite flexbeam of claim 3 wherein said hub attachment region comprises a substantially 50/50 admixture of unidirectional plies and cross plies of fiberglass and graphite.

17. The hybrid composite flexbeam of claim 16 wherein:

ply endings of said fiberglass cross plies uniformly internally interleaved in said fourth transition segment form a distributed ply drop-off arrangement therein;

ply endings of said fiberglass and graphite cross plies uniformly internally interleaved in said fifth transition segment form a distributed ply drop-off arrangement therein;

ply endings of said graphite cross plies uniformly internally interleaved in said sixth transition segment form a distributed ply drop-off arrangement therein; and

ply endings of said plurality of unidirectional fiberglass plies internally interleaved in said seventh transition segment form a distributed ply drop-off arrangement therein.

18. The hybrid composite flexbeam of claim 3 wherein said torque tube, main rotor blade attachment region comprises a substantially 50/50 admixture of unidirectional plies and cross plies of fiberglass and graphite.

19. The hybrid composite flexbeam of claim 3 wherein ply endings of said plurality of internally interleaved unidirectional fiberglass and graphite plies of varying lengths of said second inboard tapered region form a distributed ply drop-off arrangement therein.

20. The hybrid composite flexbeam of claim 3 wherein ply endings of said plurality of internally interleaved fiberglass and graphite cross plies of varying lengths of said first inboard tapered region form first, second, third, and fourth distributed ply drop-off arrangements therein.

21. The hybrid composite flexbeam of claim 3 wherein ply endings said internally interleaved plurality of fiberglass and graphite cross plies and said internally interleaved plurality of unidirectional fiberglass plies of varying length of said outboard tapered region form first, second, third, and fourth distributed ply drop-off arrangements therein.