IT1207151B - Eccentric actuator for aircraft controls - Google Patents

Eccentric actuator for aircraft controls

Info

Publication number
IT1207151B
IT1207151B IT8050109A IT5010980A IT1207151B IT 1207151 B IT1207151 B IT 1207151B IT 8050109 A IT8050109 A IT 8050109A IT 5010980 A IT5010980 A IT 5010980A IT 1207151 B IT1207151 B IT 1207151B
Authority
IT
Italy
Prior art keywords
beam member
actuator
eccentric revolution
actuators
supported
Prior art date
Application number
IT8050109A
Other languages
Italian (it)
Other versions
IT8050109A0 (en
Inventor
Robert G Musgrove
Original Assignee
Vought Corp Ora Ltv Aerospace
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
Priority claimed from US06/092,970 external-priority patent/US4286761A/en
Application filed by Vought Corp Ora Ltv Aerospace filed Critical Vought Corp Ora Ltv Aerospace
Publication of IT8050109A0 publication Critical patent/IT8050109A0/en
Application granted granted Critical
Publication of IT1207151B publication Critical patent/IT1207151B/en

Links

Landscapes

  • Transmission Devices (AREA)
  • Actuator (AREA)

Abstract

The actuator for effecting relative pivotal movement between two structures (12,14) includes a bent beam member (18) having a first portion (20) rotatably secured to one structure. A second portion (22) is supported for rotation and eccentric revolution by a housing (42) grounded to the other structure. Index gears (64,66) assure eccentric revolution of the beam member (18) in an opposite direction in response to rotation of the bent beam member to produce relative pivotal movement between the beam members (20,22). The actuators can incorporate internal hydraulic or electric drives. The actuators can instead employ various planetary type gear arrangements to achieve even greater mechanical advantage. Both portions of the bent beam member of the actuator are then driven and supported for eccentric revolution.
IT8050109A 1979-11-09 1980-11-07 Eccentric actuator for aircraft controls IT1207151B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/092,970 US4286761A (en) 1978-08-15 1979-11-09 Eccentric actuator

Publications (2)

Publication Number Publication Date
IT8050109A0 IT8050109A0 (en) 1980-11-07
IT1207151B true IT1207151B (en) 1989-05-17

Family

ID=22236026

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8050109A IT1207151B (en) 1979-11-09 1980-11-07 Eccentric actuator for aircraft controls

Country Status (2)

Country Link
CA (1) CA1139130A (en)
IT (1) IT1207151B (en)

Also Published As

Publication number Publication date
IT8050109A0 (en) 1980-11-07
CA1139130A (en) 1983-01-11

Similar Documents

Publication Publication Date Title
IT8548377A0 (en) ROTARY ACTUATOR DRIVEN BY MULTI-STAGE GEARS, PARTICULARLY FOR AIRCRAFT
ES457666A1 (en) Adjustable motor car mirror with compact electrically driven adjusting means
EP0080805A3 (en) Motion transmitting system
US4796477A (en) Rotary reversible indexing mechanism
EP0360199A3 (en) Vibration wave driven actuator
ES472387A1 (en) Transmission input decelerating and reversing mechanism
ATE31206T1 (en) MECHANICAL REDUCTION GEAR.
IT1207151B (en) Eccentric actuator for aircraft controls
GB2075629A (en) Eccentric actuator
ES8304281A1 (en) Power transmission unit with infinite speeds.
CA2136430A1 (en) Rotary engine
JPS536750A (en) Pressure oil motor revolution controller for wave force power generation
GB1557951A (en) Underspeed actuator for a hydrostatic transmission having a shut valve
US4059024A (en) Gear train with integral stop
ATE123118T1 (en) DYNAMIC COUPLING DEVICE FOR TRANSMITTING A ROTARY MOTION BETWEEN TWO SHAFTS.
SU787753A1 (en) Roller-type linear drive
EP0135777A3 (en) Robot joint
JPS5316145A (en) Hydraulic motor
JPS5684581A (en) Wheel line structure of clock
JPS63214544A (en) Speed change mechanism
SU591594A1 (en) Gear-type hydraulic motor
RU2194893C2 (en) Reduction gear for antenna system control
SU565136A1 (en) Reduction engine
SU1636206A1 (en) Manipulator arm
SU929916A1 (en) Wave transmission