Double-jet film cooling structure and method for manufacturing same

Patent metadata

Field	Value
Publication number	US-9945233-B2
Application number	US-201514944503-A
Country	US
Kind code	B2
Filing date	Nov 18, 2015
Priority date	May 22, 2013
Publication date	Apr 17, 2018
Grant date	Apr 17, 2018

Abstract

A double-jet film cooling structure includes: an injection port, formed on a wall surface facing a high-temperature gas passage; a main passage as a straight round hole to supply cooling medium to the injection port; a pair of branch passages as straight round holes; and communication passages connecting the main passage to the branch passages. The main passage and the branch passages have same constant inner diameters. Each communication passages has an envelope surface obtained by continuously arranging straight round holes each passing a branch point and having the constant inner diameter. Transverse injection angles of the branch passages relative to gas flow along the wall surface are oriented in opposite directions. An angle between axial direction of the main passage and the wall surface is greater than an angle formed between axial direction of branch passage and the wall surface.

First claim

What is claimed is:

1. A double-jet film cooling structure comprising:
an injection port, formed on a wall surface facing a passage of a high-temperature gas, to inject a cooling medium toward a downstream side of the passage;
a main passage in the form of a straight round hole formed in the wall to supply the cooling medium to the injection port;
a pair of branch passages formed in the wall, branching from a branch point on the main passage, each in the form of a straight round hole having the injection port as an outlet; and
communication passages formed in the wall that allow the main passage to communicate with respective branch passages and have the injection port as an outlet,
wherein injection directions of cooling medium components injected from the pair of branch passages are inclined with respect to a flow direction of the high-temperature gas so as to form respective swirl flows of the cooling medium components oriented in directions to push each other against the wall surface,
the main passage and the branch passages have transverse cross-sections having the same constant inner diameters,
each of the communication passages has an envelope surface obtained by continuously arranging straight round holes each of which passes the branch point and has a transverse cross-section having the constant inner diameter,
transverse injection angles β of the injection directions from the pair of branch passages with respect to the flow direction of the high-temperature gas, along the wall surface, are set to be oriented in opposite directions from each other with respect to the flow direction, and
a main longitudinal angle α 1 formed between an axial direction of the main passage and the wall surface is set to be greater than a branch longitudinal angle α 2 formed between an axial direction of each branch passage and the wall surface.

2. The double-jet film cooling structure as claimed in claim 1 , wherein an angular difference δ between the main longitudinal angle α 1 and the branch longitudinal angle α 2 is within a range of 3 to 15 degrees.

3. The double-jet film cooling structure as claimed in claim 1 , wherein a rear surface portion of the envelope surface forming the communication passages is a flat surface.

4. The double-jet film cooling structure as claimed in claim 1 , wherein a ratio Lc/H of a height Lc of a branch point of each of the branch passages to a height H of the main passage in a direction orthogonal to the wall surface is within a range of 0.3 to 0.9.

5. The double-jet film cooling structure as claimed in claim 1 , wherein the transverse injection angle β from each of the branch passages is within a range of 10 to 45 degrees.

6. The double-jet film cooling structure as claimed in claim 1 , wherein the main longitudinal angle α 1 of the main passage is within a range of 10 to 45 degrees.

7. The double-jet film cooling structure as claimed in claim 1 , wherein a distance W, along the wall surface, between outlets of the pair of branch passages is set within a range of 1.0D to 5.0D with respect to a constant inner diameter D of the main passage.

8. A method of forming the double-jet film cooling structure as claimed in claim 1 by electric-discharge machining, comprising:
forming the main passage having the constant inner diameter in the wall surface facing the passage of the high-temperature gas, by use of a cylindrical machining electrode having a predetermined outer diameter; and
performing discharging with the machining electrode being inclined with respect to an axis of the main passage to continuously form the passages from the communication passages to the branch passages.

Assignees

• Kawasaki Heavy Ind Ltd
• B&B Agema Gmbh

Inventors

• Tanaka Ryozo
• Sugimoto Takao
• Kazari Masahide
• Taniguchi Tomoki
• Kusterer Karsten
• Bohn Dieter
• Tekin Nurettin

Classifications

• F05D2240/11

  Shroud seal segments · CPC title

• B23H1/04

  Electrodes specially adapted therefor or their manufacture (B23H9/00 takes precedence) · CPC title

• F01D5/186 Primary

  Film cooling (F01D5/187 takes precedence) · CPC title

• F05D2240/81

  Cooled platforms · CPC title

• F05D2250/14

  elliptical · CPC title