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JPS54150561A - Rotary servo-actuator - Google Patents

Rotary servo-actuator

Info

Publication number
JPS54150561A
JPS54150561A JP5845878A JP5845878A JPS54150561A JP S54150561 A JPS54150561 A JP S54150561A JP 5845878 A JP5845878 A JP 5845878A JP 5845878 A JP5845878 A JP 5845878A JP S54150561 A JPS54150561 A JP S54150561A
Authority
JP
Japan
Prior art keywords
pipe line
actuator
pressurized oil
housing
output shaft
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
Application number
JP5845878A
Other languages
Japanese (ja)
Inventor
Koyo Saeki
Katsuhiko Yoshihara
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Metal Corp
Original Assignee
Mitsubishi Metal Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Metal Corp filed Critical Mitsubishi Metal Corp
Priority to JP5845878A priority Critical patent/JPS54150561A/en
Publication of JPS54150561A publication Critical patent/JPS54150561A/en
Pending legal-status Critical Current

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  • Servomotors (AREA)

Abstract

PURPOSE: To simplify the conbination of a plurality of actuators, by constructing a pressurized oil feed pipe line, a pressurized oil outlet pipe line and a drain unit in an arm part of the housing to make the opening in the outer wall face.
CONSTITUTION: In both end parts of a housing 1 is provided an arm part 24, 25 facing each other, and a pressurized oil feed pipe line 26 and a pressurized oil outlet pipe line 27 are constructed penetrating through the arm part 24, with the opening provided in a wall face of the housing. The other end of the pipe line 27 is made opening to the ring-shape groove 12 of an output shaft 3, and the other end of the pipe line 27 is made opening to the ring-shape groove 11 of the output shaft 3. In the armpart 25 is constructed a drain pipe line 28. In case of combination use of a plurality of actuators, each pipe line of one actuator can be linked to the corresponding pipe line of another actuator by means of engaging the output shaft 3 of the actuator to the manifold.
COPYRIGHT: (C)1979,JPO&Japio
JP5845878A 1978-05-17 1978-05-17 Rotary servo-actuator Pending JPS54150561A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5845878A JPS54150561A (en) 1978-05-17 1978-05-17 Rotary servo-actuator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5845878A JPS54150561A (en) 1978-05-17 1978-05-17 Rotary servo-actuator

Publications (1)

Publication Number Publication Date
JPS54150561A true JPS54150561A (en) 1979-11-26

Family

ID=13084971

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5845878A Pending JPS54150561A (en) 1978-05-17 1978-05-17 Rotary servo-actuator

Country Status (1)

Country Link
JP (1) JPS54150561A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4825754A (en) * 1986-11-26 1989-05-02 S.A.M.M.-Societe D'applications Des Machines Motrices Vane-type rotary hydraulic actuator device intended for driving an aircraft control surface

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4825754A (en) * 1986-11-26 1989-05-02 S.A.M.M.-Societe D'applications Des Machines Motrices Vane-type rotary hydraulic actuator device intended for driving an aircraft control surface

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