JPS6392002U - - Google Patents
Info
- Publication number
 - JPS6392002U JPS6392002U JP18724286U JP18724286U JPS6392002U JP S6392002 U JPS6392002 U JP S6392002U JP 18724286 U JP18724286 U JP 18724286U JP 18724286 U JP18724286 U JP 18724286U JP S6392002 U JPS6392002 U JP S6392002U
 - Authority
 - JP
 - Japan
 - Prior art keywords
 - wall portion
 - circumferential wall
 - blade tip
 - rotor
 - inner circumferential
 - 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
- 230000002093 peripheral effect Effects 0.000 claims description 3
 - 230000001154 acute effect Effects 0.000 claims 1
 - 239000000919 ceramic Substances 0.000 claims 1
 
Landscapes
- Supercharger (AREA)
 
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title | 
|---|---|---|---|
| JP18724286U JPS6392002U (en, 2012) | 1986-12-04 | 1986-12-04 | 
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title | 
|---|---|---|---|
| JP18724286U JPS6392002U (en, 2012) | 1986-12-04 | 1986-12-04 | 
Publications (1)
| Publication Number | Publication Date | 
|---|---|
| JPS6392002U true JPS6392002U (en, 2012) | 1988-06-14 | 
Family
ID=31137542
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date | 
|---|---|---|---|
| JP18724286U Pending JPS6392002U (en, 2012) | 1986-12-04 | 1986-12-04 | 
Country Status (1)
| Country | Link | 
|---|---|
| JP (1) | JPS6392002U (en, 2012) | 
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| CN100447373C (zh) * | 2001-10-19 | 2008-12-31 | 三菱重工业株式会社 | 透平涡形管道和动翼的构造 | 
- 
        1986
        
- 1986-12-04 JP JP18724286U patent/JPS6392002U/ja active Pending
 
 
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| CN100447373C (zh) * | 2001-10-19 | 2008-12-31 | 三菱重工业株式会社 | 透平涡形管道和动翼的构造 |