IP Library Granted Patent US 9,188,259
Granted Patent B2
US 9,188,259 · App. 13/984,615 · Granted Nov 17, 2015

Reduced pressure-drop pipe element

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Quick Facts
Patent No.
US 9,188,259
App. No.
13/984,615
Granted
Nov 17, 2015
Kind
B2
Abstract

A duct element configured to be used as a shapeable coupling element in a fluid flow line in any industrial application, for example within a rocket engine. The duct element includes a deformable tubular covering in a form of a bellows including inwardly projecting annular projections; and a protective sleeve including an end segment fastened in the tubular covering and including a free end that projects towards an inside of the tubular covering. The protective sleeve includes a plurality of other segments engaged in part one within another, each of the other segments including at a periphery of an outside surface thereof at least one attachment element fastened to the outside surface and that co-operates with at least one annular projection.

Claims (19)

1. A duct element comprising:

a deformable tubular covering in a form of a bellows including inwardly projecting annular projections; and

a protective sleeve including an end segment fastened in the tubular covering and including a free end that projects towards an inside of the tubular covering,

wherein the protective sleeve further includes a plurality of other segments engaged in part one within another, each of the other segments including at a periphery of an outside surface thereof at least one attachment element that is fastened to the outside surface, that co-operates with at least one annular projection, and that enables the segment to rock relative to the at least one annular projection,

wherein the bellows of the tubular covering include a sealing sheath,

wherein the tubular covering includes a central ring presenting an annular projection that projects inwards,

wherein the sealing sheath is subdivided into first and second portions which are arranged on either side of the central ring, and first ends of the first and second portions of the sealing sheath are engaged with ends of the central ring, and

wherein the annular projection of the central ring engages the attachment element of a central segment, a length of the central segment being longer than a length of the central ring.

2. A duct element according to claim 1 , wherein each of the other segments includes a band of metal strip rolled up with partial overlap and defining the outside surface.

3. A duct element according to claim 1 , wherein the attachment element is in a form of a tab that engages against at least one annular projection.

4. A duct element according to claim 3 , wherein a profile of the tab is generally U-shaped, or is U-shape with diverging branches.

5. A duct element according to claim 1 , wherein the attachment element co-operates with only one annular projection.

6. A duct element according to claim 1 , wherein each of the other segments includes a plurality of attachment elements, or at least three attachment elements.

7. A duct element according to claim 1 , wherein an end segment is fastened in the tubular covering by welding.

8. A duct element according to claim 1 , wherein an end segment is fastened to the tubular covering at a fluid inlet end thereof.

9. A duct element according to claim 1 , wherein the attachment element is fastened to the outside surface by welding.

10. A duct element according to claim 1 , wherein the sealing sheath is made of a single piece.

11. A duct element according to claim 1 , wherein the sealing sheath is made of two or more sheets that are shaped together.

12. A duct element according to claim 1 , further comprising a reinforcing ring mounted on the sealing sheath, the reinforcing ring including an annular projection projecting inwards and engaging an outside of the annular projection of the bellows.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 23, 2013
From: FIOLEK, MICHEL; DESCHAMPS, MIKAEL
To: SNECMA
Reel/Frame 031460/0741 →