DocumentCode
3552707
Title
Improved reliability of TWT´s through the use of a new lightweight heat removal device
Author
Basiulis, A. ; Starr, M.C.
Author_Institution
Hughes Aircraft Co., Torrance, Calif.
Volume
13
fYear
1967
fDate
1967
Firstpage
110
Lastpage
110
Abstract
It has been demonstrated that "heat pipe" cooling techniques can be applied to TWT\´s. Since the "heat pipe" will reduce operating temperatures and the temperature drop along the vacuum barrel, improved reliability can be attained. In addition, design flexibility is increased and the overall TWT weight may be reduced. On a specific radially focussed TWT design, the fol lowing improvements were obtained: 1. The radial temperature gradient between the vacuum barrel and th tube housing was reduced to less than 10°C. 2. The axial temperature gradient in the 10-inch long vacuum barrel was reduced to less than 6°C for a heat flux density variation from 10 watts per linear inch to 100 watts per linear inch. 3. The collector\´s cooling capacity was improved by reducing its axial and radial-temperature gradients.
Keywords
Cooling; Electron tubes; Temperature;
fLanguage
English
Publisher
ieee
Conference_Titel
Electron Devices Meeting, 1967 International
Type
conf
DOI
10.1109/IEDM.1967.187870
Filename
1474951
Link To Document