Composite structure comprising a stringer with a pad embedded in the recess of a panel and method of transmitting forces
A composite structure including a panel and a stringer bonded to the surface of the panel, the stringer having an end surface and a pair of sides extending lengthwise along the stringer away from the end surface. The surface of the panel is formed with a first wall which engages the end surface of the stringer and a second wall which engages another part of the stringer. Compressive forces are transmitted from the panel to the stringer by a normal reaction between the first wall formed in the surface of the panel and the end surface of the stringer. Tensile forces are transmitted from the panel to the stringer by a normal reaction between the second wall formed in the surface of the panel and the other surface of the stringer.
1. A composite structure comprising:
a panel; and
a stringer bonded to a surface of the panel, the stringer having an end surface and a pair of sides extending lengthwise along the stringer away from the end surface, wherein the surface of the panel is formed with a first wall which abuts the end surface of the stringer and a second wall opposite to said first wall, said second wall abuts another part of the stringer.
2. The structure of claim 1 , wherein the stringer has a second end surface at an opposite end of the stringer to the first end surface, and wherein the second wall formed in the panel engages the second end surface of the stringer.
3. The structure of claim 1 wherein the first and second walls formed in the surface of the panel are oriented in substantially opposite directions.
4. The structure of claim 1 wherein the first and second walls formed in the surface of the panel extend across the width of the stringer, substantially at right angles to the length of the stringer.
5. An aircraft skin comprising the composite structure of claim 1 .
6. The structure of claim 1 , wherein the stringer comprises a base which is bonded to the surface of the panel and a pad which protrudes from the base and is embedded in a recess in the panel; and wherein the pad has a first end surface which engages a first end wall of the recess and a second end surface which engages a second end wall of the recess.
7. The structure of claim 6 wherein the pad has a first side surface which engages a first side wall of the recess and a second side surface which engages a second side wall of the recess.
8. The structure of claim 6 wherein the bond between the base of the stringer and the surface of the panel terminates at the pad.
9. A method of transmitting forces in the composite structure of claim 1 , the method comprising:
transmitting compressive forces from the panel to the stringer by a normal reaction between the first wall formed in the surface of the panel and the end surface of the stringer; and
transmitting tensile forces from the panel to the stringer by a normal reaction between the second wall formed in the surface of the panel and the other surface of the stringer.
10. The method of claim 9 wherein substantially no tensile forces are transmitted from the panel to the stringer between the first wall formed in the surface of the panel and the end surface of the stringer, and substantially no compressive forces are transmitted from the panel to the stringer between the second wall formed in the surface of the panel and the other surface of the stringer.