Flight Simulator Seat Positioning Mechanism
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Solution Overview
Problem
Current flight simulators are costly and inefficient due to the need for multiple configurations to accommodate different types of helicopters, with limited range of motion and unstable support for pilot seats, which hinders effective training across various aircraft types.
Innovation Solution
A flight simulation apparatus featuring a base plate with parallel rails and sliders, auxiliary rails, and block units that allow for adjustable and stable positioning of pilot seats in both left-right and front-rear directions, utilizing permanent magnets for alignment and support, enabling flexible and secure seating arrangements.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If multiple simulators are manufactured for different helicopter types, then training capability for various aircraft is improved, but manufacturing cost and equipment complexity increase
Solution Approach 1:
The patent implements a universal simulator platform that can accommodate multiple helicopter types through interchangeable seat assemblies. The base structure, control systems, and simulation environment remain constant while only the seat configurations need to be changed to train for different aircraft types (UH-1H, UH-60, Bo-105, CH-47, etc.), eliminating the need for multiple dedicated simulators.
Solution Approach 2:
The simulator is divided into modular components: a fixed base structure and interchangeable seat assemblies. Each seat assembly can be independently configured and replaced based on the training requirements for specific helicopter types, allowing rapid reconfiguration without affecting the overall system.
2Adaptability or versatility
If pilot seats are made adjustable for different arrangements, then versatility for various helicopter types is improved, but stability and support of seats deteriorate
Solution Approach 1:
The seat assemblies are designed with movable and adjustable components that allow dynamic reconfiguration between different helicopter cockpit layouts. The seats can be positioned in various arrangements (side-by-side, tandem, etc.) while maintaining structural integrity through guided motion paths and controlled adjustment mechanisms.
Solution Approach 2:
The seat assembly includes pre-designed support structures and mounting mechanisms that ensure stable support is maintained during and after reconfiguration. The structural framework is designed in advance to accommodate various seat positions while providing consistent support and safety for pilots during simulation training.
3Adaptability or versatility
If seat arrangement is changed frequently for different training, then adaptability to various aircraft is improved, but training interruption and operational reliability worsen
Solution Approach 1:
Multiple seat assemblies for different helicopter types are pre-configured and ready for installation. When reconfiguration is needed, the appropriate pre-prepared seat assembly can be quickly installed without requiring on-site modification or complex setup procedures, minimizing training interruptions.
Data Source
AI summary
Disclosed is a flight simulation apparatus. According to the flight simulation apparatus of the present disclosure, first left and right rails and second left and right rails slide along a pair of first front and rear rails and a pair of second front and rear rails so that first and second seats can freely move forward and rearward, first and second auxiliary rails are formed to position the first and second seats at various locations in the front-rear direction, and the first and second seats can be stably supported by first and second sliders.