Aircraft pipework assembly
An aircraft pipework assembly is disclosed including an aircraft structure; pipework; a fixture arrangement between the pipework and the aircraft structure; a tie rod connecting the pipework to the aircraft structure; a first tie rod bearing which connects the tie rod to the pipework; and a second tie rod bearing which connects the tie rod to the aircraft structure. The fixture arrangement includes a spherical bearing, the spherical bearing comprising a ball mounted to the pipework, and a housing coupled to the aircraft structure. The ball includes a convex spherical bearing surface; and the housing comprises a concave spherical bearing surface which mates with the convex spherical bearing surface of the ball. The fixture arrangement is configured to enable the pipework to translate relative to the ball in an axial direction aligned with a longitudinal axis of the pipework.
1. An aircraft pipework assembly comprising: an aircraft structure; pipework; a fixture arrangement between the pipework and the aircraft structure; a tie rod; a first tie rod bearing which connects the tie rod to the pipework; and a second tie rod bearing which connects the tie rod to the aircraft structure; wherein the fixture arrangement comprises a spherical bearing, the spherical bearing comprising a ball mounted to the pipework and a housing coupled to the aircraft structure; the ball comprises a convex spherical bearing surface; the housing comprises a concave spherical bearing surface which mates with the convex spherical bearing surface of the ball; and the fixture arrangement is configured to enable the pipework to translate relative to the ball in an axial direction aligned with a longitudinal axis of the pipework.
2. An aircraft pipework assembly according to claim 1 , wherein the spherical bearing is configured to enable the pipework to rotate relative to the aircraft structure about three perpendicular axes.
3. An aircraft pipework assembly according to claim 1 , wherein the spherical bearing is configured to transmit radial load between the pipework and the aircraft structure, and the radial load is normal to the spherical bearing surfaces.
4. An aircraft pipework assembly according to claim 1 , wherein the concave spherical bearing surface contacts the convex spherical bearing surface of the ball.
5. An aircraft pipework assembly according to claim 1 , wherein the fixture arrangement further comprises an axial bearing, the axial bearing comprising an inner bearing surface of the ball which mates with an outer surface of the pipework, and wherein the axial bearing is configured to enable the pipework to translate relative to the ball in the axial direction.
6. An aircraft pipework assembly according to claim 5 , wherein the inner bearing surface of the ball contacts the outer surface of the pipework.
7. An aircraft pipework assembly according to claim 1 , wherein the first tie rod bearing is configured to enable the tie rod to rotate relative to the pipework about two or three perpendicular axes.
8. An aircraft pipework assembly according to claim 1 , wherein the second tie rod bearing is configured to enable the tie rod to rotate relative to the aircraft structure about two or three perpendicular axes.
9. An aircraft pipework assembly according to claim 1 , wherein the ball comprises an assembly of two or more ball parts which are distributed around a circumference of the pipework.
10. An aircraft pipework assembly according to claim 1 , wherein the housing comprises an assembly of two or more housing parts which are distributed around a circumference of the pipework.
11. An aircraft pipework assembly according to claim 1 , wherein the tie rod extends along a tie rod axis between the first tie rod bearing and the second tie rod bearing, and the tie rod axis extends at an acute angle to the axial direction.
12. An aircraft pipework assembly according to claim 1 , wherein the pipework comprises a pipe assembly, the pipe assembly comprising two or more pipe parts which are distributed in the axial direction and/or distributed radially orthogonal to the axial direction.
13. An aircraft pipework assembly according to claim 1 , wherein the pipework comprises a double-walled pipe assembly, the double-walled pipe assembly comprising an inner pipe within an outer pipe.
14. An aircraft wing comprising an aircraft pipework assembly according to claim 1 .
15. An aircraft wing according to claim 14 , further comprising a wing box with upper and lower covers, and ribs joined to the upper and lower covers, wherein the aircraft structure is one of the ribs.
16. An aircraft wing comprising: a wing rib; pipework; a fixture arrangement between the pipework and the wing rib; and a tie rod connecting the pipework to the wing rib, wherein the fixture arrangement is configured to enable the pipework to rotate relative to the wing rib about three perpendicular axes; and the fixture arrangement is configured to enable the pipework to translate relative to the fixture arrangement in an axial direction aligned with a longitudinal axis of the pipework.