18514075. AIRCRAFT CONTROL SURFACE DEPLOYMENT SYSTEM simplified abstract (AIRBUS OPERATIONS LIMITED)
Contents
- 1 AIRCRAFT CONTROL SURFACE DEPLOYMENT SYSTEM
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 AIRCRAFT CONTROL SURFACE DEPLOYMENT SYSTEM - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Potential Commercial Applications
- 1.9 Possible Prior Art
- 1.10 Original Abstract Submitted
AIRCRAFT CONTROL SURFACE DEPLOYMENT SYSTEM
Organization Name
Inventor(s)
Denys Custance of Bristol (GB)
Marc Lopezboix of Bristol (GB)
AIRCRAFT CONTROL SURFACE DEPLOYMENT SYSTEM - A simplified explanation of the abstract
This abstract first appeared for US patent application 18514075 titled 'AIRCRAFT CONTROL SURFACE DEPLOYMENT SYSTEM
Simplified Explanation
The aircraft control surface deployment system described in the patent application is a mechanism that allows for the raising and lowering of an aircraft control surface, such as a spoiler on an aircraft wing. The system includes a cam body, an actuator, and a coupling mechanism that connects the actuator to the cam body. The coupling mechanism is designed to allow for free relative movement and rotation of its parts, preventing loads transverse to the actuator's movement axis from being transferred to the actuator.
- Cam body, actuator, and coupling mechanism work together to control the movement of the aircraft control surface.
- Actuator moves the cam body to raise and lower the control surface.
- Coupling mechanism allows for free movement and rotation of its parts to prevent transferring loads to the actuator.
Potential Applications
The technology can be applied in various aircraft systems where precise control of control surfaces is required, such as in spoiler deployment systems for aircraft wings.
Problems Solved
The system prevents loads transverse to the actuator's movement axis from being transferred to the actuator, ensuring smooth and efficient operation of the aircraft control surface.
Benefits
- Improved control and maneuverability of the aircraft. - Prevents damage to the actuator from transverse loads. - Enhanced safety and reliability of the aircraft system.
Potential Commercial Applications
The technology can be utilized in commercial aircraft manufacturing and maintenance to enhance the performance and safety of aircraft control systems.
Possible Prior Art
One possible prior art could be similar aircraft control surface deployment systems used in the aerospace industry, but without the specific design features of the coupling mechanism described in this patent application.
Unanswered Questions
How does the system handle extreme weather conditions or high-speed flight situations?
The patent application does not provide details on how the system performs in extreme weather conditions or high-speed flight situations. Further testing and analysis would be needed to determine the system's effectiveness in such scenarios.
What materials are used in the construction of the cam body, actuator, and coupling mechanism?
The patent application does not specify the materials used in the construction of the components. Understanding the materials used is crucial for assessing the system's durability and performance in real-world applications.
Original Abstract Submitted
An aircraft control surface deployment system for an aircraft structure, that can be a spoiler deployment system for an aircraft wing, includes a cam body, an actuator, and a coupling mechanism. The actuator moves the cam body such that it raises and lowers the aircraft control surface. The actuator is connected to the cam body via the coupling mechanism. The coupling mechanism has a first portion connected to the cam body and a second portion connected to the actuator, configured such that the coupling mechanism allows some free relative movement and rotation of the first and second portions. Loads transverse to the axis of movement of the actuator, resulting from relative movement of the cam body, are not transferred to the actuator.
