18514422. AIRCRAFT CONTROL SURFACE SYSTEM simplified abstract (AIRBUS OPERATIONS LIMITED)
Contents
- 1 AIRCRAFT CONTROL SURFACE SYSTEM
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 AIRCRAFT CONTROL SURFACE 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 Unanswered Questions
- 1.11 Original Abstract Submitted
AIRCRAFT CONTROL SURFACE SYSTEM
Organization Name
Inventor(s)
Denys Custance of Bristol (GB)
AIRCRAFT CONTROL SURFACE SYSTEM - A simplified explanation of the abstract
This abstract first appeared for US patent application 18514422 titled 'AIRCRAFT CONTROL SURFACE SYSTEM
Simplified Explanation
The aircraft control surface system described in the patent application is a mechanism for deploying a control surface member, such as a pop-up spoiler, on an aircraft wing. The system allows the control surface member to move between a retracted position, where it is curled for stowage within the aircraft structure, and a deployed position, where it extends from the surface of the aircraft structure. The deployment mechanism enables the control surface member to extend to have a straight portion with a length greater than the local depth of the aircraft structure.
- The system includes a deployable control surface member and a deployment mechanism.
- The deployment mechanism moves the control surface member between a retracted and deployed position.
- In the retracted position, the control surface member is curled for stowage within the aircraft structure.
- In the deployed position, the control surface member extends from the aircraft structure.
- The deployment mechanism allows the control surface member to extend with a length greater than the local depth of the aircraft structure.
Potential Applications
The technology could be applied in the aerospace industry for various aircraft models to improve aerodynamic performance and control.
Problems Solved
1. Improved aerodynamic performance. 2. Enhanced control over the aircraft.
Benefits
1. Increased efficiency in aircraft operation. 2. Enhanced safety and maneuverability. 3. Potential fuel savings.
Potential Commercial Applications
Optimizing aircraft performance and control systems in commercial aviation.
Possible Prior Art
There may be prior art related to aircraft control surface systems and mechanisms for deploying control surfaces on aircraft wings.
Unanswered Questions
How does the deployment mechanism ensure the control surface member extends smoothly and efficiently?
The patent application does not provide detailed information on the specific mechanisms or technologies used to ensure the smooth and efficient extension of the control surface member.
What materials are used in the construction of the deployable control surface member?
The patent application does not specify the materials used in the construction of the deployable control surface member.
Original Abstract Submitted
An aircraft control surface system for an aircraft structure, that can be a pop-up spoiler for an aircraft wing, includes a deployable control surface member and a deployment mechanism. The deployment mechanism moves the deployable control surface member between a retracted position and a deployed position. In the retracted position, the deployable control surface member is curled to facilitate stowage within the aircraft structure. In the deployed position, the deployable control surface member is uncurled and extends from a surface of the aircraft structure. The deployment mechanism enables the deployable control surface member to extend to have a straight portion with a length greater than the local depth of the aircraft structure.
