Aerodynamic/hydrodynamic profile with a composite reinforced oblong foam core

Patent metadata

Field	Value
Publication number	US-11124285-B2
Application number	US-201816037269-A
Country	US
Kind code	B2
Filing date	Jul 17, 2018
Priority date	Jul 18, 2017
Publication date	Sep 21, 2021
Grant date	Sep 21, 2021

Abstract

An aerodynamic profile including a skin defining the outer surface of the aerodynamic profile, a leading edge, a trailing edge and a central portion representing at least 50% of the chord of the profile. The profile includes a hollow core of composite material reinforced with a textile having unidirectional fibers. The hollow core has, in cross section, an oblong shape that is rounded, in particular at each of its ends. The skin bears against the hollow core over the length of the central portion of the aerodynamic profile, both on the pressure side and on the suction side of the profile. The reinforcement with a textile having unidirectional fibers permits an ideal orientation of reinforcing fibers in order to optimize mechanical properties in certain directions. The shape of the hollow core, elongate along the chord of the profile and rounded, lends it great resistance to deformation.

First claim

The invention claimed is:

1. A profile for aerodynamic or hydrodynamic applications, the profile comprising:
a skin defining an outer surface of the profile;
a leading edge;
a trailing edge;
a central portion representing at least 50% of a chord of the profile;
a hollow core comprising composite material, which comprises a matrix and a textile having unidirectional fibers, the hollow core having, in cross section, an oblong shape that is rounded at each of its ends; and
a transverse hollow beam, which has an essentially rectangular cross-section, arranged in the hollow core, the hollow beam extending transversely in a thickness of the profile and being made of composite material;
wherein the skin bears against the hollow core over a length of the central portion of the profile, both on a pressure side of the profile and on a suction side of the profile; and
wherein the profile is a profile selected from the group consisting of: a wing, an aileron, a wingtip winglet, an empennage, a fairing, a flap, and a foil.

2. The profile according to claim 1 , wherein the skin comprises a composite material or a composite material covered with a metallic outer layer.

3. The profile according to claim 2 , wherein the composite material of the skin comprises a matrix and a textile having unidirectional fibers.

4. The profile according to claim 1 , wherein the matrix is a polymer matrix.

5. The profile according to claim 1 , wherein the hollow core comprises at least one planar outer surface.

6. The profile according to claim 1 , wherein the hollow core has a suction-side wall, a pressure-side wall, and two connecting walls between the suction-side wall and the pressure-side wall, and wherein fibers of the suction-side wall and of the pressure-side wall are predominantly oriented parallel to the skin, along a reference direction that is inclined relative to the chord of the profile.

7. The profile according to claim 6 , wherein:
the skin comprises a composite material or a composite material covered with a metallic outer layer;
the composite material of the skin comprises a matrix and a textile having unidirectional fibers; and
the fibers of the skin are oriented at an angle with respect to the reference direction.

8. The profile according to claim 7 , wherein the angle is 45° or 135°.

9. The profile according to claim 6 , wherein the reference direction is perpendicular to the chord of the profile.

10. The profile according to claim 9 , wherein fibers of the connecting walls are oriented at an angle of 45° or approximately 135° with respect to the reference direction.

11. The profile according to claim 9 , wherein:
the skin comprises a composite material or a composite material covered with a metallic outer layer;
the composite material of the skin comprises a matrix and a textile having unidirectional fibers; and
the fibers of the skin are oriented at an angle of 45° or 135° with respect to the reference direction.

12. The profile according to claim 1 , wherein at least one of a first internal volume, which is defined by the hollow core over the length of the central portion in which the hollow beam is arranged, is filled with a first foam and/or a second internal volume, which is defined by the skin at the leading edge and the trailing edge, is filled with a second foam.

13. The profile according to claim 12 , wherein the second foam has a density that is greater than a density of the first foam.

14. The profile according to claim 1 , wherein the foil is a boat foil for the hydrodynamic application.

15. The profile according to claim 1 , wherein:
the hollow core has a suction-side wall, a pressure-side wall, and two connecting walls between the suction-side wall and the pressure-side wall;
fibers of the suction-side wall and of the pressure-side wall are predominantly oriented parallel to the skin, along a reference direction perpendicular to the chord of the profile;
fibers of the connecting walls are oriented at an angle of 45° or 135° with respect to the reference direction;
the skin comprises a composite material or a composite material covered with a metallic outer layer;
the composite material of the skin comprises a matrix and a textile having unidirectional fibers; and
the fibers of the skin are oriented at an angle of 45° or 135° with respect to the reference direction.

16. The profile according to claim 1 , wherein the hollow core extends over all of the central portion of the profile.

17. The profile according to claim 1 , wherein at least one of a first volume, which is defined by the hollow core over the length of the central portion in which the hollow beam is arranged, a second volume defined by the volume of the hollow beam, a third volume defined by the leading edge, and a fourth volume defined by the trailing edge are filled with foam, some or all of the first, second, third, and fourth volumes being filled with a same foam.

Assignees

• Airbus Operations Sas
• Airbus Sas

Inventors

• Trouve Rodolphe
• Lacombe Jean-Claude
• Rodes Julien
• Schutz Thomas

Classifications

• B64C3/20

  Integral or sandwich constructions · CPC title

• B29D99/0025 Primary

  Producing blades or the like, e.g. blades for turbines, propellers, or wings · CPC title

• B64C3/185

  Spars · CPC title

• B29L2031/3085

  Wings · CPC title

• B64C3/26 Primary

  Construction, shape, or attachment of separate skins, e.g. panels · CPC title