High temperature fuel manifold for gas turbine engines

1. A segment of a fluid manifold for a gas turbine engine comprising:

a flexible thermal shield with an insulation space defined inboard of the flexible thermal shield to provide thermal isolation from conditions external to the flexible thermal shield, wherein the flexible thermal shield includes a helically corrugated metal tube having opposed first and second ends; and

an outer collar threaded to a first end of the helically corrugated metal tube, wherein a vent is defined between the outer collar and the flexible thermal shield in venting communication with the insulation space.

2. A segment of a fluid manifold as recited in claim 1 , wherein the outer collar includes a crimped portion and an uncrimped portion, the uncrimped portion being spaced apart from the helically corrugated metal tube more than the crimped portion to define the vent between the outer collar and the helically corrugated metal tube in venting communication with the insulation space.

3. A segment of a fluid manifold as recited in claim 2 , wherein there are four crimped portions circumferentially alternating with four respective uncrimped portions to form four vents from the insulation space to an area outside the flexible thermal shield.

4. A segment of a fluid manifold as recited in claim 1 , further comprising a liner defining an internal fluid passage therethrough fluidly connecting a pair of hose fitting inserts, wherein the flexible thermal shield is outboard of the liner, and wherein the insulation space is defined between the liner and the flexible thermal shield.

5. A segment of a fluid manifold as recited in claim 4 , wherein the outer collar includes fitting threads engaged with threads on one of the hose fitting inserts, and wherein the fitting threads of the outer collar are structurally ovalized relative to the threads of the hose fitting insert engaged thereto to prevent unthreading of the outer collar.

6. A segment of a fluid manifold as recited in claim 4 , further comprising a lock wire connecting the outer collar to the hose fitting insert engaged thereto to prevent de-threading of the outer collar.

7. A segment of a fluid manifold as recited in claim 6 , further comprising a weld joining the lock wire to the outer collar and a weld joining the lock wire to the hose fitting insert engaged to the outer collar.

8. A segment of a fluid manifold as recited in claim 4 , further comprising a cable connecting the outer collar to the hose fitting insert engaged thereto to prevent de-threading of the outer collar.

9. A segment of a fluid manifold as recited in claim 4 , wherein the collar and the hose fitting insert engaged thereto include at least one staked portion that is locally deformed to prevent de-threading of the outer collar.

10. A segment of a fluid manifold as recited in claim 4 , further comprising at least one weld joining the outer collar to the hose fitting insert engaged to the outer collar.

11. A fuel manifold for distributing fuel to a gas turbine engine comprising:

a plurality of interconnected manifold segments, each manifold segment extending between a pair of fuel injector inlet fittings, wherein each manifold segment includes:

a flexible thermal shield with an insulation space is defined inboard of the flexible thermal shield to provide thermal isolation from conditions external to the flexible thermal shield, wherein the flexible thermal shield includes a helically corrugated metal tube having opposed first and second ends; and

an outer collar threaded to a first end of the helically corrugated metal tube, wherein a vent is defined between the outer collar and the flexible thermal shield in venting communication with the insulation space.

12. A fuel manifold as recited in claim 11 , wherein the outer collar includes a crimped portion and an uncrimped portion, the uncrimped portion being spaced apart from the corrugated helical metal tube more than the crimped portion to define the vent between the outer collar and the corrugated helical metal tube in venting communication with the insulation space.

13. A fuel manifold as recited in claim 12 , wherein there are four crimped portions circumferentially alternating with four respective uncrimped portions to form four vents from the insulation space to an area outside the flexible thermal shield.

14. A fuel manifold as recited in claim 11 , wherein each manifold segment includes a liner defining an internal fluid passage therethrough fluidly connecting a pair of hose fitting inserts, wherein the flexible thermal shield is outboard of the liner, and wherein the insulation space is defined between the liner and the flexible thermal shield.

15. A fuel manifold as recited in claim 14 , wherein the outer collar of each manifold segment includes fitting threads engaged with threads on one of the hose fitting inserts, and wherein the fitting threads of the outer collar are structurally ovalized relative to the threads of the hose fitting insert engaged thereto to prevent unthreading of the outer collar.

16. A fuel manifold as recited in claim 14 , further comprising a lock wire connecting the outer collar to the hose fitting insert engaged thereto to prevent de-threading of the outer collar.

17. A fuel manifold as recited in claim 16 , further comprising a weld joining the lock wire to the outer collar and a weld joining the lock wire to the hose fitting insert engaged to the outer collar.

18. A fuel manifold as recited in claim 14 , further comprising a cable connecting the outer collar to the hose fitting insert engaged thereto to prevent de-threading of the outer collar.

19. A fuel manifold as recited in claim 14 , wherein the collar and the hose fitting insert engaged thereto include at least one staked portion that is locally deformed to prevent de-threading of the outer collar.

20. A fuel manifold as recited in claim 14 , further comprising at least one weld joining the outer collar to the hose fitting insert engaged to the outer collar.