199
RIKEN Accel. Próg. Rep. 24 (1990)
3000
Points of aeasureaent |
(D |
<D |
© |
© | |
22. 539 m |
♦ |
* |
* |
» |
• |
radius |
27.8 |
44.6 |
50.0 |
44.5 |
27.8 |
Chaaber 1 |
16.8 |
27.0 |
30.2 |
26.7 |
16.1 |
Chaaber 2 |
22.6 |
35.8 |
40.7 |
36.4 |
22.7 |
Chaaber 3 |
22 . 1 |
35.3 |
39.7 |
35.3 |
22.1 |
« calculated valu«?
A circulating electron beam in a storage ring reduces electromagnetic fields in vacuum system components such as chamber, bellows, and gate valve. When a straight chamber is used in a bending magnet section, the break of symmetri-cal electromagnetic fields might drive a trans-verse instability for an electron beam, because a curved beam causes an offset in respect to the center of the beam chambers transversally. Therefore chambers in the bending magnet section should be curved along beam orbits.
To ascertain the feasibility of bending the complicated chamber to be used in bending magnet section of the SPring-8 storage ring, we built a bending magnet chamber by means of stretch forming. Figurę 1 shows the schematics of a stretch former, and Fig. 2 the photograph of a bending test. In this test we used an existing forming błock of 23-m curvature radius for an another chamber to save the building cost of the bending magnet chamber.
Hydraulic strcch cylinder
Fig. 1. Schematic diagram of a stretch former.
Fig. 3. Bending radius of the chamber after stretch forming.
I
I
r-4 |
H H N C |
* JUL | 5 2_aj |
iĄ co co | ||
No |
Section A |
No |
Soction A |
Section B | |
i |
-0.10 |
0.0 |
20 |
+0.01 |
0.0 |
2 |
+ 0.05 |
+ 0.14 |
21 |
-0.10 |
-0.40 |
3 |
-0.10 |
♦ 0.10 |
22 |
-0.02 |
-0.01 |
4 |
0.0 |
-0.20 |
23 |
+ 0.02 |
-0.02 |
5 |
-0.10 |
-0.10 |
24 |
-0.10 |
-0.50 |
6 |
-0.10 |
0.0 |
25 |
40.01 |
-0.04 |
7 |
+ 0.10 |
0.0 |
26 |
-0.20 |
-0.50 |
8 |
4-0.07 |
40.04 |
27 |
-0.30 |
-0.70 |
9 |
0.0 |
+0.60 |
28 |
-0.30 |
-0.60 |
10 |
♦ 0.06 |
+ 0.12 |
29 |
+ 0.08 |
-0.12 |
1 1 |
-0.03 |
40.03 |
30 |
-0.20 |
-0.60 |
12 |
0.0 |
0.0 |
31 |
4*0.02 |
+0.08 |
13 |
♦ 0.03 |
+ 0.05 |
32 |
♦ 0.03 |
-0.05 |
14 |
0.0 |
♦ 0.03 |
33 |
-0.10 |
-0.30 |
16 |
+ 0.10 |
0.0 |
34 |
-0.01 |
-0.02 |
16 |
0.0 |
+ 0.02 |
35 |
-0.09 |
-0.01 |
17 |
0.0 |
♦ 0.06 |
36 |
0.0 |
-0.20 |
18 |
0.0 |
-0.10 |
37 |
+0.02 |
-0.02 |
19 |
4-0 . Ob |
+0.06 |
Fig. 4. Deformations of the cross-sections of the chamber.
i
Fig. 2. Photograph of the test.
*
Ishikawajima-Harima Heavy Industries Co., Ltd.