HYDROSTATIC AUTOMATIC FLIGHT SERVO SYSTEMS

摘要

A hydrostatic automatic flight servo system is provided. The automatic flight servo system includes a manifold that defines a first fluid chamber, and a hydraulic fluid is received in the first fluid chamber. The first fluid chamber includes a first bellows and a second bellows. The automatic flight servo system includes a stick received at least partially within the manifold and pivotally coupled to the manifold. The stick includes a control arm fixedly coupled to the first bellows, and the stick is to receive an input. The automatic flight servo system includes a flight output system pivotally coupled to the manifold. The flight output system includes a second control arm received at least partially within the manifold and coupled to the second bellows such that the pivotal movement of the stick pivots the flight output system relative to the manifold.

主权项

1. A hydrostatic automatic flight servo system comprising:
a manifold that defines a first fluid chamber, with a hydraulic fluid received in the first fluid chamber, the first fluid chamber including a first bellows and a second bellows; a stick received at least partially within the manifold and pivotally coupled to the manifold, the stick including a control arm fixedly coupled to the first bellows, the stick adapted to receive an input; and a flight output system pivotally coupled to the manifold, the flight output system including a second control arm received at least partially within the manifold and coupled to the second bellows such that the pivotal movement of the stick pivots the flight output system relative to the manifold.