System and method for fastening structures

Patent metadata

Field	Value
Publication number	US-9676469-B2
Application number	US-201414249486-A
Country	US
Kind code	B2
Filing date	Apr 10, 2014
Priority date	Apr 10, 2014
Publication date	Jun 13, 2017
Grant date	Jun 13, 2017

Abstract

A system includes an outer band, inner band, and a fastener. The outer band covers at least a portion of a first structure and has a first edge opposite a second edge. The second edge forms a first load redistribution ramp corresponding to a bend in the first structure. The inner band is positioned beneath a second structure and has a first surface opposite a second surface. The second surface forms a second load redistribution ramp corresponding to the bend in the first structure. A portion of the inner band adjacent to the second surface forms a curve around an edge of the second structure such that the second load redistribution ramp forms a wedge between the first structure and the second structure. The fastener couples the outer band, first structure, second structure, and inner band.

First claim

What is claimed is:

1. An apparatus, comprising:
an outer band covering at least a portion of a first structure, the outer band having a first edge opposite a second edge, the second edge forming a first load redistribution ramp corresponding to a bend in the first structure;
an inner band positioned beneath a second structure, the inner band having a first surface opposite a second surface, the second surface forming a second load redistribution ramp corresponding to the bend in the first structure, wherein a portion of the inner band adjacent to the second surface forms a curve around an edge of the second structure such that the second load redistribution ramp forms a wedge between the first structure and the second structure; and
a fastener coupling together the outer band, the first structure, the second structure, and the inner band, a portion of the fastener extending through an aperture in each of the outer band, the first structure, the second structure, and the inner band.

2. The apparatus of claim 1 , wherein the first structure comprises a composite structure and the second structure comprises a non-composite structure.

3. The apparatus of claim 1 , wherein the first structure is selected from the group consisting of a radome, a nose cone, a control surface, an access panel, an exhaust nozzle of an aircraft, an exhaust nozzle of a rocket, and an exhaust nozzle of a missile.

4. The apparatus of claim 1 , wherein an angle of the first load redistribution ramp and an angle of the second load redistribution ramp are each between fifteen and forty-five degrees.

5. The apparatus of claim 1 , wherein the aperture in the first structure is adapted to prevent the fastener from contacting the first structure.

6. The apparatus of claim 1 , wherein the inner band and the outer band comprise one of high-temperature steel and titanium.

7. The apparatus of claim 1 , wherein the first structure is removable.

8. The apparatus of claim 1 , the outer band adapted to prevent movement of the first structure in a first direction and the inner band adapted to prevent movement of the first structure in a second direction that is opposite from the first direction.

9. An apparatus, comprising:
a first structure;
a second structure; and
a system for fastening the first structure to the second structure so that the first structure is removable from the second structure, the system comprising:
an outer band covering at least a portion of the first structure and adapted to prevent the first structure from moving in a first direction, the outer band comprising:
a first edge proximate to the second structure; and
a second edge proximate to the first structure, the second edge forming a first load redistribution ramp corresponding to a bend in the first structure;

an inner band positioned beneath a portion of the second structure and adapted to prevent the first structure from moving in a second direction that is opposite from the first direction, the inner band comprising:
a first surface proximate to the second structure; and
a second surface proximate to the first structure, the second surface forming a second load redistribution ramp corresponding to the bend in the first structure, wherein a portion of the inner band adjacent to the second surface forms a curve around an edge of the second structure such that the second load redistribution ramp forms a wedge between the first structure and the second structure; and

a fastener coupling together the outer band, the first structure, the second structure, and the inner band, a portion of the fastener extending through an aperture in each of the outer band, the first structure, the second structure, and the inner band, the aperture in the first structure being adapted to prevent the fastener from contacting the first structure.

10. The apparatus of claim 9 , wherein an angle of the first load redistribution ramp and an angle of the second load redistribution ramp are each between fifteen and forty-five degrees.

11. The apparatus of claim 9 , wherein the first structure is selected from the group consisting of a radome, a nose cone, a control surface, an access panel, an exhaust nozzle of an aircraft, an exhaust nozzle of a rocket, and an exhaust nozzle of a missile.

12. The apparatus of claim 9 , wherein the first edge of the outer band and an edge of the first structure are adapted to correspond to a bend in the second structure.

13. The apparatus of claim 9 , wherein the first structure comprises a composite structure and the second structure comprises a non-composite structure.

14. A method for attaching two structures comprising:
positioning an outer band over a first structure, the outer band covering at least a portion of the first structure and having a first edge proximate to a second structure, and a second edge proximate to the first structure, the second edge forming a first load redistribution ramp corresponding to a bend in the first structure;
positioning an inner band beneath the second structure, the inner band having a first surface proximate to the second structure and opposite a second surface proximate to the first structure, the second surface forming a second load redistribution ramp corresponding to the bend in the first structure, wherein a portion of the inner band adjacent to the second surface forms a curve around an edge of the second structure such that the second load redistribution ramp forms a wedge between the first structure and the second structure; and
attaching the outer band, the first structure, the second structure, and the inner band to each other with a fastener, a portion of the fastener passing through an aperture in each of the outer band, the first structure, the second structure, and the inner band, the aperture of the first structure adapted to prevent the fastener from bearing directly against the first structure.

15. The method of claim 14 , wherein the first structure comprises a composite structure and the second structure comprises a non-composite structure.

16. The method of claim 15 , wherein the first structure is selected from the group consisting of a radome, a nose cone, a control surface, an access panel, an exhaust nozzle of an aircraft, an exhaust nozzle of a rocket, and an exhaust nozzle of a missile.

17. The method of claim 14 , wherein an angle of the first load redistribution ramp and an angle of the second load redistribution ramp are each between fifteen and forty-five degrees.

18. The method of claim 14 , wherein the inner band and the outer band comprise one of high-temperature steel and titanium.

19. The method of claim 14 , wherein the first structure is removable.

20. The method of claim 14 , the outer band adapted to prevent movement of the first structure in a first direction and the inner band adapted to prevent movement of the first structure in a second direction that is opposite from the first direction.

Assignees

• Benner Kent W
• Lockheed Corp

Inventors

• Benner Kent W

Classifications

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• F05D2300/6033

  Ceramic matrix composites [CMC] · CPC title

• Y02T50/672

  Cross-Sectional Technologies · mapped topic

• F16B5/0012

  a tongue on the edge of one sheet, plate or panel co-operating with a groove in the edge of another sheet, plate or panel · CPC title

• F02C7/00

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title