SU565193A1 - Device for pressing capillary-porous material to thermal pipe wall - Google Patents
Device for pressing capillary-porous material to thermal pipe wallInfo
- Publication number
- SU565193A1 SU565193A1 SU7301874085A SU1874085A SU565193A1 SU 565193 A1 SU565193 A1 SU 565193A1 SU 7301874085 A SU7301874085 A SU 7301874085A SU 1874085 A SU1874085 A SU 1874085A SU 565193 A1 SU565193 A1 SU 565193A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- porous material
- pipe wall
- thermal pipe
- capillary
- pressing
- Prior art date
Links
Description
1one
Изобретение предназначено дл улучшени структуры капилл рного сло в тепловой трубе .The invention is intended to improve the structure of a capillary layer in a heat pipe.
Известны устройства дл нрижати капилл рно-пористого материала к стеике корпуса тепловой трубы, выполненные в виде перфорированной трубки.There are known devices for pressing capillary-porous material to a heat pipe body steak, made in the form of a perforated tube.
Дл повышени надежности трубы в предлагаемом устройстве трубка ио образующей имеет разъем, в котором установлена клиновидна полоса.In order to increase the reliability of the pipe in the proposed device, the tube which generates has a connector in which a wedge-shaped strip is installed.
На фиг. 1 схематично изображена теплова труба с описываемым устройством; на фиг. 2- узел I на фиг. 1.FIG. 1 schematically shows a heat pipe with the described device; in fig. 2- node I in FIG. one.
Теилова труба содержит герметичный корпус 1 с капилл рно-пористым материалом 2 внутри и перфорированной трубкой 3 дл прижати материала. Трубка разрезана ио образующей и в разъеме установлена клиновидна полоса 4. В данном случае проход дл полосыThe teil tube comprises a hermetic body 1 with a capillary-porous material 2 inside and a perforated tube 3 to press the material. The tube is cut by the IO generator and a wedge-shaped strip 4 is installed in the connector. In this case, the strip pass
ооразуетс из цилиндрической части корнуса сеткодержател и вниз отогнутых « зычков, полученных в результате коротких разрезов держател , выполненных в плоскости чертежа и расположенных равномерно ио длине трубы.It is rotated from the cylindrical part of the mesh holder's corn and downwardly bent tabs, obtained as a result of short cuts of the holder, made in the plane of the drawing and spaced evenly over the length of the pipe.
На держатель с вынутой клиновидной иолосой наматывают слои сетки, полученное вставл ют в корпус тепловой трубы, а затем в проход вставл ют клпновпдную полосу.Layers of mesh are wound onto the holder with the wedge-shaped and hair removed, the resulting material is inserted into the heat pipe body, and then the control strip is inserted into the passage.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU7301874085A SU565193A1 (en) | 1973-01-18 | 1973-01-18 | Device for pressing capillary-porous material to thermal pipe wall |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU7301874085A SU565193A1 (en) | 1973-01-18 | 1973-01-18 | Device for pressing capillary-porous material to thermal pipe wall |
Publications (1)
Publication Number | Publication Date |
---|---|
SU565193A1 true SU565193A1 (en) | 1977-07-15 |
Family
ID=20539898
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU7301874085A SU565193A1 (en) | 1973-01-18 | 1973-01-18 | Device for pressing capillary-porous material to thermal pipe wall |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU565193A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4931905A (en) * | 1989-01-17 | 1990-06-05 | Grumman Aerospace Corporation | Heat pipe cooled electronic circuit card |
-
1973
- 1973-01-18 SU SU7301874085A patent/SU565193A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4931905A (en) * | 1989-01-17 | 1990-06-05 | Grumman Aerospace Corporation | Heat pipe cooled electronic circuit card |
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