Aircraft assembly
An aircraft assembly including: an aircraft structure; a pipe assembly; a fixture arrangement attached to the aircraft structure, the fixture arrangement contacting the pipe assembly via a curved bearing surface having curvature in two orthogonal directions; the curved bearing surface configured to enable the pipe assembly to rotate relative to the fixture arrangement about three perpendicular axes; wherein the pipe assembly comprises a stop member adjacent the fixture arrangement, a contact surface of the stop member configured to abut a contact surface of the fixture arrangement so as to restrict axial movement of the pipe assembly relative to the fixture arrangement, and wherein a distance between the contact surface of the fixture arrangement and the contact surface of the stop member increases radially from the longitudinal pipe axis.
1 . An aircraft assembly comprising:
an aircraft structure;
a pipe assembly with a bearing surface and a longitudinal pipe axis; and
a fixture arrangement attached to the aircraft structure, the fixture arrangement contacting the pipe assembly via a curved bearing surface having curvature in two orthogonal directions, wherein the curved bearing surface contacts the bearing surface of the pipe assembly, and the curved bearing surface is configured to enable the pipe assembly to rotate relative to the fixture arrangement about three perpendicular axes; and
a stop member adjacent the fixture arrangement, wherein a contact surface of the stop member is configured to abut a contact surface of the fixture arrangement to restrict axial movement of the pipe assembly relative to the fixture arrangement,
wherein a gap between the contact surface of the fixture arrangement and the contact surface of the stop member increases radially from the longitudinal pipe axis.
2 . The aircraft assembly of claim 1 , wherein the gap between the contact surface of the fixture arrangement and the contact surface of the stop member increases exponentially.
3 . The aircraft assembly of claim 1 , wherein the contact surface of the stop member is angled relative to a plane normal to the longitudinal pipe axis.
4 . The aircraft assembly of claim 1 , wherein the contact surface of the fixture arrangement lies on a plane normal to the longitudinal pipe axis.
5 . The aircraft assembly of claim 1 , wherein the contact surface of the stop member is curved in two orthogonal directions.
6 . The aircraft assembly of claim 1 , wherein a curvature of the curved bearing surface matches a curvature of the contact surface of the stop member.
7 . The aircraft assembly of claim 1 , wherein the curved bearing surface is on the fixture arrangement.
8 . The aircraft assembly of claim 7 , wherein the bearing surface of the pipe assembly is a cylindrical bearing surface and the curved bearing surface contacts the cylindrical bearing surface of the pipe assembly.
9 . The aircraft assembly of claim 1 , wherein the aircraft structure is a wing rib, fairing rib, or fuselage frame.
10 . An aircraft comprising the aircraft assembly of claim 1 .
11 . The aircraft assembly of claim 1 , wherein the stop member is adjacent a sidewall of the fixture arrangement, the contact surface of the stop member abuts a contact surface on the sidewall of the fixture arrangement to restrict the axial movement of the pipe assembly relative to the fixture arrangement, and the sidewall of the fixture arrangement extends radially outward beyond the bearing surface of the fixture arrangement in a direction perpendicular to the longitudinal pipe axis.
12 . The aircraft assembly of claim 1 , wherein the curved bearing surface has a convex curvature along a direction parallel to the longitudinal pipe axis.
13 . An aircraft assembly comprising:
an aircraft structure;
a pipe assembly; and
a fixture arrangement attached to the aircraft structure, the fixture arrangement contacting the pipe assembly via a curved bearing surface having curvature in two orthogonal directions, wherein the curved bearing surface is configured to enable the pipe assembly to rotate relative to the fixture arrangement about three perpendicular axes, and
a stop member adjacent the fixture arrangement, wherein a contact surface of the stop member is configured to abut a contact surface of the fixture arrangement to restrict axial movement of the pipe assembly relative to the fixture arrangement,
wherein a gap between the contact surface of the fixture arrangement and the contact surface of the stop member increases radially from the longitudinal pipe axis, and
wherein the stop member is formed of two or more parts that interconnect circumferentially.
14 . The aircraft assembly of claim 13 , wherein axial movement of the pipe assembly relative to the fixture arrangement is restricted by the first and second stop members with axial movement no greater than 10 mm.
15 . The aircraft assembly of claim 13 , wherein axial movement of the pipe assembly relative to the fixture arrangement is restricted by the first and second stop members with axial movement of at least 2 mm.
16 . The aircraft assembly of claim 13 , wherein the pipe assembly comprises an inner pipe within an outer pipe.
17 . The aircraft assembly of claim 16 , comprising a cryogenic fuel in the inner pipe.
18 . The aircraft assembly of claim 17 , wherein the cryogenic fuel is liquid hydrogen.
19 . The aircraft assembly of claim 16 , comprising a vacuum pressure between the inner pipe and the outer pipe.
20 . An aircraft assembly comprising:
an aircraft structure;
a pipe assembly;
a fixture arrangement attached to the aircraft structure, the fixture arrangement contacting the pipe assembly via a curved bearing surface having curvature in two orthogonal directions, wherein the curved bearing surface is configured to enable the pipe assembly to rotate relative to the fixture arrangement about three perpendicular axe, and
a stop member adjacent the fixture arrangement, wherein a contact surface of the stop member is configured to abut a contact surface of the fixture arrangement to restrict axial movement of the pipe assembly relative to the fixture arrangement;
wherein a gap between the contact surface of the fixture arrangement and the contact surface of the stop member increases radially from the longitudinal pipe axis;
wherein the pipe assembly comprises a second stop member adjacent the fixture arrangement such that the fixture arrangement is between the first and second stop members,
wherein a contact surface of the second stop member is configured to abut a second contact surface of the fixture arrangement to restrict axial movement of the pipe assembly relative to the fixture arrangement, and
wherein a gap between the contact surface of the fixture arrangement and the contact surface of the second stop member increases radially from the longitudinal pipe axis.
21 . The aircraft assembly of claim 20 , wherein the pipe assembly has a plane of symmetry that lies between the first and second stop members.
22 . The aircraft assembly of claim 20 , wherein the first and second stop members are connected by a collar, the collar includes the bearing surface in contact with the fixture arrangement at the curved bearing surface, and the collar is a component of the pipe assembly.