JPS63157202U - - Google Patents
Info
- Publication number
- JPS63157202U JPS63157202U JP4983287U JP4983287U JPS63157202U JP S63157202 U JPS63157202 U JP S63157202U JP 4983287 U JP4983287 U JP 4983287U JP 4983287 U JP4983287 U JP 4983287U JP S63157202 U JPS63157202 U JP S63157202U
- Authority
- JP
- Japan
- Prior art keywords
- support ring
- pin
- fixed
- movable wing
- attached
- 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.)
- Pending
Links
- 239000010409 thin film Substances 0.000 claims description 3
- 210000003746 feather Anatomy 0.000 claims description 2
- 239000012141 concentrate Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
Landscapes
- Vaporization, Distillation, Condensation, Sublimation, And Cold Traps (AREA)
Description
第１図は本考案の一実施例を示す支持リングと
可動翼およびストツパーの取付状況を示す部分拡
大平面図、第２図は同じく一部断面側面図、第３
図は遠心薄膜蒸発器の全体図、第４図および第５
図は従来の支持リングと可動翼の取付状を示す平
面図および側面図である。
１……加熱胴、２……原料入口、３……可動翼
、４……蒸発物出口、５……濃縮物出口、６……
支持リング、７……ボス、８……ストツパー、９
……ストレート羽根、１０……胴体内壁、１１…
…ナツト、１２……ピン。
Fig. 1 is a partially enlarged plan view illustrating an embodiment of the present invention showing how the support ring, movable blade, and stopper are attached; Fig. 2 is a partially sectional side view;
The figure shows the overall view of the centrifugal thin film evaporator, Figures 4 and 5.
The figures are a plan view and a side view showing how a conventional support ring and movable blade are attached. 1... Heating cylinder, 2... Raw material inlet, 3... Movable blade, 4... Evaporated material outlet, 5... Concentrate outlet, 6...
Support ring, 7... Boss, 8... Stopper, 9
...Straight feather, 10...Inner body wall, 11...
...Natsuto, 12...Pin.
Claims (1)
動翼の先端を胴体内壁に摺動させる遠心薄膜蒸発
器において、ストレート羽根をボスに固着して可
動翼を形成し、前記可動翼のボスをピンを介して
支持リングに回動可能に取付けると共に、前記ス
トレート羽根と係合してこれを係止するストツパ
ーを前記ピンを介して支持リングの外側面に固定
したことを特徴とする遠心薄膜蒸発器の羽根の構
造。 In a centrifugal thin film evaporator in which the tip of a movable wing attached to a support ring fixed to a rotating shaft is slid against the inner wall of the fuselage, the straight vane is fixed to a boss to form a movable wing, and the boss of the movable wing is attached to a pin. A centrifugal thin film evaporator characterized in that the stopper is rotatably attached to the support ring via the pin, and a stopper that engages and locks the straight blade is fixed to the outer surface of the support ring via the pin. Structure of the feather.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4983287U JPS63157202U (en) | 1987-04-03 | 1987-04-03 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4983287U JPS63157202U (en) | 1987-04-03 | 1987-04-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63157202U true JPS63157202U (en) | 1988-10-14 |
Family
ID=30872650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4983287U Pending JPS63157202U (en) | 1987-04-03 | 1987-04-03 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63157202U (en) |
-
1987
- 1987-04-03 JP JP4983287U patent/JPS63157202U/ja active Pending