Claims
- 1. A fluidic device for an aircraft comprising:
a passage block defining an internal space; an internal body, an outer surface of the internal body being liquid tightly fitted to the internal space; an actuator having a portion and a cylinder chamber; and a fluid-controlled valve; wherein the passage block defines:
first fluid passages communicating the internal space with the cylinder chamber of the actuator, second fluid passages communicating the internal space with the fluid-controlled valve, and third fluid passages, by which fluid is supplied to and discharged from the internal space, the internal body defines grooves by which the first, second and third fluid passages are communicated, the grooves extending along the outer surface of the internal body.
Priority Claims (1)
Number |
Date |
Country |
Kind |
P. HEI. 11-347184 |
Dec 1999 |
JP |
|
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This application is a continuation of pending U.S. patent application Ser. No. 10/163,438, filed Jun. 4, 2002, which is a divisional of U.S. Pat. No. 6,435,205 B1.
Divisions (1)
|
Number |
Date |
Country |
Parent |
09528638 |
Mar 2000 |
US |
Child |
10163438 |
Jun 2002 |
US |
Continuations (1)
|
Number |
Date |
Country |
Parent |
10163438 |
Jun 2002 |
US |
Child |
10322561 |
Dec 2002 |
US |