Methods and apparatus for reducing noise in reinforced skin structures

• US 9,016,628 B2
• Filed: 06/12/2012
• Issued: 04/28/2015
• Est. Priority Date: 06/12/2012
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Christenson, Justin, Hoffman, Herbert L., Chewning, Gary R., Lin, Juhn-Shyue
• Primary Examiner(s): Canfield, Robert
• Assistant Examiner(s): GITLIN, MATTHEW J
• Application Number:
  US13/494,083
• Publication Number:
  US 20130327588A1
• Time in Patent Office: 1,050 Days
• Field of Search: 521/677, 521/678, 521/679, 521/673, 528/43, 528/46, 528/47, 526/93, 526/96, 244/117.R, 244/119, 181/207, 181/210, 181/290, 181/292
• US Class Current: 244/119
• CPC Class Codes: B64C 1/061 Frames
• CPC Class Codes: B64C 1/064 Stringers; Longerons
• CPC Class Codes: B64C 1/40 Sound or heat insulation , e.g. using insulation blankets
• CPC Class Codes: F16F 9/306 of the constrained layer type, i.e. comprising one or more constrained viscoelastic layers
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y10T 29/49826 Assembling or joining

Abstract

Assemblies, methods, and an apparatus for damping vibrational energy induced to a reinforced skin structure are disclosed. The reinforced skin structure includes an outer wall and at least one stringer coupled to the outer wall. The method includes providing a damping apparatus that includes a stiffening member configured to adjust at least one of a bending mode and a torsional twisting mode of the stringer and an energy dissipation member configured to dissipate vibrational energy of the stringer. The stiffening member includes at least two elongated members that are spaced a distance apart and at least one truss member that extends obliquely between the at least two elongated members. The damping apparatus is attached to the at least one stringer. The damping apparatus may be configured to dampen vibration in the range of between about 200-600 Hz.

Claims

1. A method for damping vibrational energy induced to a reinforced skin structure, wherein the reinforced skin structure includes an outer wall and at least one stringer coupled to the outer wall and having a length that extends between a pair of adjacent frame members, said method comprising:

attaching a damping apparatus to the at least one stringer, the damping apparatus configured to dampen vibration of the at least one stringer, wherein the damping apparatus includes a stiffening member configured to adjust at least one of a bending mode and a torsional twisting mode of the stringer and an energy dissipation member configured to dissipate vibrational energy of the stringer, the stiffening member including at least two elongated members that are spaced a distance apart, and that are oriented substantially parallel to one another, wherein the stiffening member further includes at least one truss member that extends obliquely between the at least two elongated members; and

orienting the damping apparatus such that the at least two elongated members extend the length of the at least one stringer and such that the torsional twisting mode of the at least one stringer is adjusted.

2. A method in accordance with claim 1, wherein the energy dissipation member includes a viscoelastic material member.

3. A method in accordance with claim 1, further comprising:

disposing the energy dissipation member on at least one surface of each of the at least two elongated members; and

attaching the at least two elongated members to the at least one stringer such that the energy dissipation member is positioned between the at least two elongated members and the stringer.

4. A method in accordance with claim 3, further comprising disposing the energy dissipation member substantially continuously across an entire length of at least one surface of each of the at least two elongated members.

5. A method in accordance with claim 1, further comprising providing the damping apparatus substantially continuously across an entire length of the at least one stringer.

6. A method in accordance with claim 1, wherein the at least one truss member defines a plurality of equilateral triangular-shaped apertures between the at least two elongated members.

7. A reinforced skin structure comprising:

an outer wall;

a pair of adjacent frame members coupled to said outer wall;

at least one stringer coupled to said outer wall and having a length extending between said pair of adjacent frame members; and

a vibration damping apparatus coupled to said stringer, said vibration damping apparatus comprising;

a stiffening member configured to adjust at least one of a bending mode and a torsional twisting mode of said stringer and extending along at least a portion of said at least one stringer, said stiffening member comprising at least two elongated members spaced a distance apart, extending the length of the at least one stringer such that the torsional twisting mode is adjusted, and oriented substantially parallel to one another and at least one truss member extending obliquely between said at least two elongated members; and

an energy dissipation member coupled to said stiffening member, said energy dissipation member configured to dissipate vibrational energy of the stringer.

8. A reinforced skin structure in accordance with claim 7, wherein said energy dissipation member comprises a viscoelastic material member on at least one surface of each of said at least two elongated members.

9. A reinforced skin structure in accordance with claim 7, wherein said energy dissipation member has a thickness between about 0.005 inches and about 0.02 inches.

10. A reinforced skin structure in accordance with claim 7, wherein said energy dissipation member extends substantially continuously across an entire length of at least one surface of each of said two elongated members.

11. A reinforced skin structure in accordance with claim 7, wherein each of said at least two elongated members extends substantially continuously across an entire length of said at least one stringer.

12. A reinforced skin structure in accordance with claim 7, wherein said at least one stringer comprises:

a cross-member for coupling said at least one stringer to said outer wall;

a first leg member and an opposing second leg member, each of said leg members extending substantially perpendicularly from opposite ends of said cross-member; and

a first flange and a second flange, said first flange extending substantially perpendicularly from said first leg member, said second flange extending substantially perpendicularly from said second leg member.

13. A reinforced skin structure in accordance with claim 12, wherein said at least two elongated members are coupled to each of said first and second flanges.

14. A reinforced skin structure in accordance with claim 7, wherein said at least one truss member defines a plurality of triangular-shaped apertures between said at least two elongated members.

15. An apparatus for damping vibrational energy of a reinforced skin structure that includes an outer wall and, a pair of adjacent frame members coupled to the outer wall, and at least one stringer coupled to the outer wall and having a length extending between the pair of adjacent frame members, said apparatus comprising:

a stiffening member configured to adjust at least one of a bending mode and a torsional twisting mode of a reinforced skin structure, said stiffening member comprising;

at least two elongated members spaced a distance apart, each sized to extend the length of the at least one stringer such that the torsional twisting mode is adjusted, and oriented substantially parallel to one another; and

at least one truss member extending obliquely between said at least two elongated members; and

an energy dissipation member coupled to said stiffening member, said energy dissipation member configured to dissipate vibrational energy of the reinforced skin structure.

16. An apparatus in accordance with claim 15, wherein said energy dissipation member comprises a viscoelastic material member on at least one surface of each of said at least two elongated members.

17. An apparatus in accordance with claim 15, wherein said energy dissipation member extends substantially continuously across an entire length of at least one surface of each of said two elongated members.

18. An apparatus in accordance with claim 15, wherein said energy dissipation member comprises one of acrylic, urethane, and silicon.

19. An apparatus in accordance with claim 15, wherein said energy dissipation member has a thickness between 0.005 inches and 0.02 inches.

20. An apparatus in accordance with claim 15, wherein said vibration damping apparatus comprises one or more of aluminum, steel, titanium, and graphite.