GB842540A - Rotary regenerative heat exchanger - Google Patents
Rotary regenerative heat exchangerInfo
- Publication number
- GB842540A GB842540A GB8951/59A GB895159A GB842540A GB 842540 A GB842540 A GB 842540A GB 8951/59 A GB8951/59 A GB 8951/59A GB 895159 A GB895159 A GB 895159A GB 842540 A GB842540 A GB 842540A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- diaphragm
- thermal
- passages
- march
- 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
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
- F28D19/04—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
842,540. Thermal regenerators. AIR PREHEATER CORPORATION. March 16, 1959 [March 26, 1958], No. 8951/59. Class 64(1) In a thermal regenerator of the rotary matrix type in which the rotor 10 is divided by diaphrams 16 into sectorshaped compartments for the heat transfer material (not shown), each diaphragm is hollow and fluid passages 36, 38 are provided therein on each side of a radially extending partition 34, the arrangement being such that some of the heating gas entering the regenerator through a duct 20 is directed through a port 46 and thence through the diaphragm passages before reentering the heating gas stream by way of a port 54 adjacent the cooled gas outlet duct 22. By this arrangement thermal distortion of the rotor with consequent reduction of the efficiency of the sealing means is said to be substantially eliminated. In the form shown, the diaphragm passages 36, 38 communicate with the ports 46, 54 through ducts 44, 52 formed in the rotor post 18.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US842540XA | 1958-03-26 | 1958-03-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB842540A true GB842540A (en) | 1960-07-27 |
Family
ID=22183779
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB8951/59A Expired GB842540A (en) | 1958-03-26 | 1959-03-16 | Rotary regenerative heat exchanger |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB842540A (en) |
-
1959
- 1959-03-16 GB GB8951/59A patent/GB842540A/en not_active Expired
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