Double-walled pipe with integrated heating capability for an aircraft or spacecraft
US-2016312924-A1 · Oct 27, 2016 · US
US10400920B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10400920-B2 |
| Application number | US-201715430763-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 13, 2017 |
| Priority date | Mar 7, 2016 |
| Publication date | Sep 3, 2019 |
| Grant date | Sep 3, 2019 |
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A double skinned feed or scavenge pipe assembly comprises; an inner pipe ( 22 ) and an outer pipe ( 23 ) enclosing the inner pipe and defining an annular space ( 24 ) between the inner pipe and the outer pipe and a sleeve ( 28 ) configured to slip over the outer pipe ( 23 ). Complementary threads ( 29 ) are provided on an outer wall of the outer pipe ( 23 ) and an inner wall of the sleeve ( 28 ). A lock, for example in the form of a locking nut ( 31 ) is positioned over the outer pipe ( 23 ) when the complementary threads ( 29 ) of the outer pipe and sleeve are engaged. The configuration of the assembly is such that, in use, the sleeve ( 28 ) is slidable between a first position where the inner pipe ( 22 ) is accessible and a second position wherein the inner pipe ( 22 ) is completely enclosed.
Opening claim text (preview).
The invention claimed is: 1. A double skinned pipe assembly comprising: an inner pipe and an outer pipe enclosing the inner pipe and defining an annular space between the inner pipe and the outer pipe; a sleeve configured to slip over the outer pipe; complementary threads on an outer wall of the outer pipe and an inner wall of the sleeve; and a lock for locking the sleeve in position over the outer pipe when the complementary threads of the outer pipe and sleeve are engaged, wherein the configuration of the assembly is such that, in use, the sleeve is movable between a first position where the inner pipe may be accessed and a second position wherein the inner pipe is completely enclosed. 2. A double skinned pipe assembly as claimed in claim 1 wherein the lock comprises a locking nut which includes a thread which is complementary to the thread on the outer pipe and is arranged to be threaded onto the outer pipe after the sleeve has been threaded onto the outer pipe. 3. A double skinned pipe assembly as claimed in claim 2 wherein the lock further includes a tab washer arranged between the locking nut and the sleeve and receivable in a tab washer groove provided in a mid-portion of the thread, wherein once the sleeve and locking nut are arranged for locking, the tabs of the washer can be bent and engage with the nut and/or sleeve to restrict axial and/or rotational movement thereof. 4. A double skinned pipe assembly as claimed in claim 1 wherein the lock is incorporated into the sleeve and/or the outer pipe. 5. A double skinned pipe assembly as claimed in claim 4 wherein the lock comprises an anti-rotation feature on the outer pipe configured to engage with the sleeve when the sleeve is in the second position. 6. A double skinned pipe assembly as claimed in claim 1 wherein the outer pipe includes a stop against which the sleeve abuts when the sleeve is in the second position. 7. A double skinned pipe assembly as claimed in claim 6 wherein the stop comprises a flange. 8. A double skinned pipe assembly as claimed in claim 1 wherein the inner pipe is joined to a body into/out of which the inner pipe feeds or scavenges. 9. A double skinned pipe assembly as claimed in claim 8 wherein the inner pipe is welded to the body. 10. A double skinned pipe assembly as claimed in claim 8 wherein the body comprises a hub of a bearing chamber in a gas turbine engine. 11. A gas turbine engine incorporating a double skinned pipe assembly as claimed in claim 1 wherein the inner pipe is joined to and arranged to feed into or scavenge out of a hub of a bearing chamber. 12. A gas turbine engine incorporating a double skinned pipe assembly as claimed in claim 4 wherein the inner pipe is joined to and arranged to feed into or scavenge out of a hub of a bearing chamber.
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