GB621368A - Improvements relating to heat interchange apparatus - Google Patents
Improvements relating to heat interchange apparatusInfo
- Publication number
- GB621368A GB621368A GB524947A GB524947A GB621368A GB 621368 A GB621368 A GB 621368A GB 524947 A GB524947 A GB 524947A GB 524947 A GB524947 A GB 524947A GB 621368 A GB621368 A GB 621368A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tubes
- casing
- cooling
- baffles
- fluid
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/22—Arrangements for directing heat-exchange media into successive compartments, e.g. arrangements of guide plates
Abstract
621,368. Tubular heat-exchangers; cooling radiators for aircraft. SERCK RADIATORS, Ltd., MARTIN, A. M., and MONTGOMERIE, G. A. Feb. 22, 1947, No. 5249. [Class 64(iii)] Relates to apparatus of the kind comprising an assembly of tubes 3 arranged parallel with each other in concentric rings in a casing 1 in which one fluid is caused by means of transverse baffles 4, 5 (see Fig. 2, in which four tubes only are indicated) to flow radially alternately towards and away from the central axis of the tube assembly through the spaces between the tubes while the other fluid flows through the tubes. According to the invention, the circumferential spacing of the tubes increases from the outer ring 10 to the inner ring 11 of the assembly. The spacing of the tubes in two or more successive rings may be equal and the tubes may be staggered, e.g. as shown in Fig. 1. Alternate baffles 5 contact with the casing 1 at their peripheries and are formed with central holes 6 while the remaining baffles 4 provide passages for the one fluid at their peripheries and may be supplied with supporting spacers 7. The ends of the tubes 3 are expanded into the plates 2 of the casing. The apparatus may be used on aircraft for cooling the engine jacket water or warming or cooling the lubricating oil.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB524947A GB621368A (en) | 1947-02-22 | 1947-02-22 | Improvements relating to heat interchange apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB524947A GB621368A (en) | 1947-02-22 | 1947-02-22 | Improvements relating to heat interchange apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
GB621368A true GB621368A (en) | 1949-04-07 |
Family
ID=9792532
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB524947A Expired GB621368A (en) | 1947-02-22 | 1947-02-22 | Improvements relating to heat interchange apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB621368A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3044164A1 (en) * | 1979-11-23 | 1981-09-03 | Chemetics International Ltd., Vancouver, British Columbia | HEAT EXCHANGER |
-
1947
- 1947-02-22 GB GB524947A patent/GB621368A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3044164A1 (en) * | 1979-11-23 | 1981-09-03 | Chemetics International Ltd., Vancouver, British Columbia | HEAT EXCHANGER |
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