Claims
- 1. In a regeneratively cooled rocket combustor comprising a wall having a hot-side surface for defining the interior of said combustor, and a plurality of longitudinally extending, spaced apart coolant channels formed within said combustor wall, said coolant channels being substantially rectangular in cross-sectional shape with the long axis of the rectangle oriented radially with respect to the axis of said combustor, each of said coolant channels having interior surfaces and a roof, said roof being formed by the portion of said combustor wall situated between said hot-side surface and said coolant channel; wherein the improvement comprises at least one keel-rib formed within each coolant channel, each said keel-rib extending a minor fraction of the way into said coolant channel from said roof and being bounded by longitudinally extending arcuate flutes for providing smooth and continuous surface transition between said keel-rib and adjoining interior surfaces of said coolant channel, each said keel-rib extending said minor fraction for substantially the entire length of each said coolant channel.
- 2. The combustor wall as set forth in claim 1 wherein said keel-rib is parabolic in cross-sectional shape.
- 3. The combustor wall as set forth in claim 1 wherein said keel-rib is formed by convergently tapered walls extending from said roof.
- 4. The combustor wall as set forth in claim 1 wherein said keel-rib is formed by parallel walls extending from said roof.
Parent Case Info
This application is a continuation of application Ser. No. 481,550 filed 04/04/83, now abandoned.
US Referenced Citations (1)
Number |
Name |
Date |
Kind |
3154914 |
Stockel |
Nov 1964 |
|
Foreign Referenced Citations (1)
Number |
Date |
Country |
459924 |
Jan 1937 |
GBX |
Continuations (1)
|
Number |
Date |
Country |
Parent |
481550 |
Apr 1983 |
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