Force Gradient Switch With Non-Contact Proximity Sensing
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Solution Overview
Problem
Traditional force gradient mechanisms in aircraft control systems require frequent adjustments and are prone to mechanical wear, leading to reliability issues and inconvenience in maintaining proper operating conditions.
Innovation Solution
A force gradient design incorporating a non-contact proximity sensor, which eliminates mechanical contact and adjustments by using a spring and a proximity sensor to signal the Automatic Flight Control System (AFCS) state changes, reducing the need for manual alignment and maintenance.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a mechanical actuator mechanism is used in the force gradient switch, then the AFCS operation can be controlled, but frequent adjustments and maintenance are required due to mechanical wear
Solution Approach 1:
The patent replaces the mechanical actuator mechanism with a non-contact proximity sensor that detects the position of a target member on the shaft. This eliminates mechanical contact and wear, thereby improving reliability and reducing maintenance requirements while maintaining the ability to control AFCS operation based on cyclic stick position
2Ease of operation
If a mechanical actuator mechanism is used in the force gradient switch, then the switch can control AFCS operation, but the mechanism requires frequent adjustment to maintain proper operating conditions
Solution Approach 1:
The proximity sensor provides contactless detection of shaft position, eliminating the need for mechanical alignment and adjustment. The sensor automatically detects the target member's position without requiring manual intervention, thereby maintaining ease of operation while eliminating time-consuming adjustments
Solution Approach 2:
The proximity sensor system is self-aligning and requires no manual adjustment to maintain proper operating conditions. The sensor automatically adapts to the shaft position through its non-contact detection mechanism, making the system self-servicing and eliminating maintenance downtime
3Ease of repair
If a mechanical actuator mechanism is used in the force gradient switch, then the switch can signal AFCS state changes, but disassembly is required to service inner parts
Solution Approach 1:
By replacing the complex mechanical actuator mechanism with a proximity sensor and target member arrangement, the patent simplifies the overall structure. The sensor can be mounted externally on the force gradient housing and detect the target member on the shaft without requiring internal mechanical linkages, making components more accessible and reducing assembly complexity
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
The solution provides a more reliable and convenient control system with reduced mechanical wear, improved pilot feedback, and accurate filtering of intended and unintended inputs, enhancing the overall operational reliability and ease of maintenance.
Implementation Method 1
a non-contact proximity sensor mounted on the second end. The spring has a first position and is compressed to a second position so that the non-contact proximity sensor signals an AFCS to change state
Data Source
AI summary
An improved design for a force gradient using a proximity sensor is disclosed. A force gradient comprises a shaft having a first end and a second end. The switch includes a spring contained between the first end and the second end and a non-contact proximity sensor mounted on the second end. The spring has a first position and is compressed to a second position so that the non-contact proximity sensor signals an AFCS to change state.


