Pipe having an upstream core having a sharp curvature

Patent metadata

Field	Value
Publication number	US-9341082-B2
Application number	US-201214003180-A
Country	US
Kind code	B2
Filing date	Mar 2, 2012
Priority date	Mar 4, 2011
Publication date	May 17, 2016
Grant date	May 17, 2016

Abstract

A turbine engine pipe having a longitudinal axis, which, at an upstream end thereof, includes an outer wall and a core, only an upstream portion of which is surrounded by the outer wall. The boundary between the upstream portion and a downstream portion is defined by the intersection between the core and the surface formed by bisectors of acute angles formed by straight lines perpendicular to the outer wall and straight lines perpendicular to an outer surface of the core passing through the downstream end of the outer wall. The outer surface of the downstream portion of the core has a sharply curved convex region close to the boundary, the region having a radius of curvature in a radial plane of less than 30 times the radius of the core at the boundary, and a first slightly curved region between the boundary and the sharply curved convex region.

First claim

The invention claimed is:

1. A turbine engine pipe, in which a working fluid circulates during normal operation from upstream to downstream, comprising:
at a downstream end, an outer wall and a core, an upstream part of the core surrounded by the outer wall and a downstream part of the core extends the upstream part downstream from the outer wall,
a border between the upstream part and the downstream part being defined by an intersection between the core and a surface formed by bisectors of acute angles formed by straight lines perpendicular to the outer wall and passing through the downstream end of the outer wall and straight lines perpendicular to an outer face of the core and passing through the downstream end of the outer wall,
a space between the outer wall and the upstream part of the core defining an annular tunnel having a longitudinal axis, a portion of the surface which extends between the outer face and the outer wall constitutes a downstream orifice of the annular tunnel,
wherein the outer face of the downstream part of the core includes, downstream from the border, a sharply curved convex region at each point of which the radius of curvature, in the longitudinal radial plane, is smaller than a first radius equal to 30 times a radius of curvature of the core in a transverse plane at a point of intersection of the border and the longitudinal radial plane,
the sharply curved convex region being situated within 33% of the downstream part of the core that is furthest upstream, and a first convex region with a smaller curvature, between the border and the sharply curved convex region, at each point of which the radius of curvature in the longitudinal radial plane is greater than a second radius equal to 10 times the first radius.

2. The pipe according to claim 1 , wherein, at each point of the sharply curved convex region, its radius of curvature is less than half of the first radius.

3. The pipe according to claim 1 , wherein the first region with a smaller curvature has a length smaller than 0.02 times the radius of curvature of the core.

4. The pipe according to claim 3 , wherein the first region with a smaller curvature has a length not greater than 0.8 times the radius of curvature of the core.

5. The pipe according to claim 3 , wherein the first region with a smaller curvature has a length not greater than 0.55 times the distance between the border and a downstream end of the core in the direction of the longitudinal axis.

6. The pipe according to claim 1 , wherein the sharply curved convex region has a length not less than 1.9 times the radius of curvature of the core.

7. The pipe according to claim 6 , wherein the sharply curved convex region has a length not greater than 2.7 times the radius of curvature of the core.

8. The pipe according to claim 1 , wherein the outer face of the downstream part of the core includes, downstream from the sharply curved convex region, a second convex region with a smaller curvature at each point of which any radius of curvature in a longitudinal radial plane is greater than a second radius equal to 10 times the first radius.

9. The pipe according to claim 1 , wherein the downstream end of the core is truncated.

Assignees

• Bensilum Stephane Emmanuel Daniel
• Bertucchi Jean
• Gaillot Mathieu
• Snecma

Inventors

• Bensilum Stephane Emmanuel Daniel
• Bertucchi Jean
• Gaillot Mathieu

Classifications

• B64D33/04 Primary

  of exhaust outlets or jet pipes · CPC title

• F05D2250/711

  convex · CPC title

• F02K1/00 Primary

  Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K9/97) · CPC title

• F01D25/24 Primary

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic