JPH0228999U - - Google Patents
Info
- Publication number
- JPH0228999U JPH0228999U JP10475388U JP10475388U JPH0228999U JP H0228999 U JPH0228999 U JP H0228999U JP 10475388 U JP10475388 U JP 10475388U JP 10475388 U JP10475388 U JP 10475388U JP H0228999 U JPH0228999 U JP H0228999U
- Authority
- JP
- Japan
- Prior art keywords
- steering
- shaft
- flying body
- fuselage
- fixed
- 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
- 239000012528 membrane Substances 0.000 claims 1
Landscapes
- Toys (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10475388U JPH0228999U (de) | 1988-08-08 | 1988-08-08 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10475388U JPH0228999U (de) | 1988-08-08 | 1988-08-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0228999U true JPH0228999U (de) | 1990-02-23 |
Family
ID=31336750
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP10475388U Pending JPH0228999U (de) | 1988-08-08 | 1988-08-08 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0228999U (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2301359A1 (es) * | 2006-05-16 | 2008-06-16 | Airbus España, S.L. | Sistema de sellado de hueco existente entre el fuselaje y el timon de altura de un avion con estabilizador horizontal orientable. |
JP2011502882A (ja) * | 2007-11-16 | 2011-01-27 | ザ・ボーイング・カンパニー | マルチセグメント・フラップフェンスのための方法及び装置 |
-
1988
- 1988-08-08 JP JP10475388U patent/JPH0228999U/ja active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2301359A1 (es) * | 2006-05-16 | 2008-06-16 | Airbus España, S.L. | Sistema de sellado de hueco existente entre el fuselaje y el timon de altura de un avion con estabilizador horizontal orientable. |
JP2011502882A (ja) * | 2007-11-16 | 2011-01-27 | ザ・ボーイング・カンパニー | マルチセグメント・フラップフェンスのための方法及び装置 |