18732897. ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR simplified abstract (GOODRICH CORPORATION)
ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR
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ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR - A simplified explanation of the abstract
This abstract first appeared for US patent application 18732897 titled 'ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR
Simplified Explanation:
The patent application describes a landing gear system for an aircraft that includes various components such as a truss frame, retraction actuator, truss links, and articulation actuator.
- The system features a truss frame that can rotate about an axis, pivotally connected to the aircraft frame.
- A retraction actuator is used to rotate the truss frame about the axis.
- Truss links and locking links are pivotally connected to the truss frame, allowing for movement and locking of the landing gear.
- An articulation actuator pivots the truss links with respect to the truss frame.
Key Features and Innovation:
- Truss frame pivotally connected to aircraft frame.
- Retraction actuator for rotating truss frame.
- Truss links for movement and articulation actuator for pivoting.
Potential Applications:
The landing gear system can be used in various types of aircraft to improve landing and take-off operations.
Problems Solved:
This technology addresses the need for a reliable and efficient landing gear system for aircraft.
Benefits:
- Improved landing and take-off operations.
- Enhanced safety and stability during flight.
Commercial Applications:
The landing gear system can be utilized in commercial airlines, military aircraft, and private jets to enhance overall performance and safety.
Prior Art:
Readers can start searching for prior art related to landing gear systems in the field of aviation engineering and aircraft design.
Frequently Updated Research:
Stay updated on advancements in landing gear technology and aircraft systems to ensure optimal performance and safety.
Questions about Landing Gear Systems: 1. What are the key components of a landing gear system? 2. How does the articulation actuator contribute to the functionality of the landing gear system?
Original Abstract Submitted
A landing gear system for an aircraft is disclosed. In various embodiments, the system includes a truss frame pivotally connected to a frame of the aircraft and configured to rotate about an axis; a retraction actuator configured to rotate the truss frame about the axis; a first truss link pivotally connected to the truss frame; a second truss link pivotally connected to the first truss link; a truss locking link pivotally connected to the truss frame and to the second truss link; and an articulation actuator configured to pivot the first truss link with respect to the truss frame.
