Other

Richard T Russ

Thomas C Williams

An apparatus for rigidly interlocking a control stick and the rudder pedals of an aircraft is provided for protecting the control surfaces of the aircraft operated by the control stick and the rudder pedals against wind loads. The apparatus comprises a control stick clamp assembly rigidly connected to one end of a first lever arm and a rudder pedal retaining assembly rigidly connected to another end of the first lever arm. A second lever arm has one end connected to the rudder pedal retaining assembly. The second lever arm is moveable between a collapsed position and an extended position wherein the distal end of the second lever arm is engageable with a support surface such that the second lever arm is able to support the rudder pedal retaining assembly in engagement with each of the rudder pedals and thereby cause, upon the control stick clamp assembly being secured to the control stick, the first lever arm to support the control stick in a selected position.

Apparatus for locking control surfaces of stick controlled aircraft

A locking apparatus in combination with a locking pin and method for rigidly interlocking a control wheel and the rudder pedals of an aircraft is provided for securing the control surfaces of the aircraft operated by the control wheel and the rudder pedals in a stable position. The locking pin is adapted to be disposed through aligned locking pin receiving holes of the control column and the control panel collar and has a recess formed therein for lockingly receiving a portion of the control column. The locking apparatus includes a pair of control wheel retaining members rigidly connected to one end of a rod member for retainingly engaging the control wheel and a rudder pedal engaging bar rigidly connected to one end of another rod member. The rudder pedal engaging bar is positionable in a V-shaped notch of each of the rudder pedals so as to engage each of the rudder pedals and so as to secure the rudder pedal engaging bar on the rudder pedals. The rod members are disposed in a telescoping relationship with respect to one another and are adjustably securable whereby the control wheel retaining members are rigidly locked in a selected position relative to the rudder pedal retaining bar wherein the control wheel retaining members cooperate with the rudder pedal retaining bar to support the control column in a pin locking position wherein the control column is lockingly disposed in the recess of the locking pin.

Apparatus for locking aircraft controls

An apparatus and method for rigidly interlocking a control wheel and the rudder pedals of an aircraft is provided for securing the control surfaces of the aircraft operated by the control wheel and the rudder pedals in a stable position. The apparatus comprises a pair of control wheel retaining members rigidly connected to one end of a rod member in a spaced apart, parallel relationship with one another for retainingly engaging opposing radially extending portions of the control wheel and a pair of rudder pedal retaining members rigidly connected to one end of another rod member in a spaced apart, parallel relationship with one another for retainingly engaging a lever of each of the rudder pedals. The rod members are disposed in a telescoping relationship with respect to one another and are adjustably securable whereby the control wheel retaining members are rigidly locked in a selected position relative to the rudder pedal retaining members wherein the control wheel retaining members cooperate with the rudder pedal retaining members to secure the control wheel in a level position, the control column in an inward position, and the rudder pedals in a neutral or centered position.

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Oklahoma City, OK, United States of America

Richard T Russ