18172569. Linear Actuator Driven Flap Mechanism simplified abstract (The Boeing Company)
Contents
- 1 Linear Actuator Driven Flap Mechanism
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 Linear Actuator Driven Flap Mechanism - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Key Features and Innovation
- 1.6 Potential Applications
- 1.7 Problems Solved
- 1.8 Benefits
- 1.9 Commercial Applications
- 1.10 Prior Art
- 1.11 Frequently Updated Research
- 1.12 Questions about Aircraft Wing Flap Mechanisms
- 1.13 Original Abstract Submitted
Linear Actuator Driven Flap Mechanism
Organization Name
Inventor(s)
Samuel L. Block of Bothell WA (US)
Kevin R. Tsai of Redmond WA (US)
Linear Actuator Driven Flap Mechanism - A simplified explanation of the abstract
This abstract first appeared for US patent application 18172569 titled 'Linear Actuator Driven Flap Mechanism
Simplified Explanation
A linear actuator driven flap mechanism for an aircraft wing is designed to be compact and fit within thinner, smaller aircraft wings. The mechanism is attached to the wingbox structure and utilizes a linear actuator and motion linkage for operation.
- The flap mechanism is contained within a wing support and fairing of the aircraft wing.
- The rib frame of the flap mechanism is attached to the wingbox structure at two points.
- A linear actuator and motion linkage are positioned within the rib frame.
- The linear actuator is not mechanically driven rotary or linear actuation.
- This design allows for the flap mechanism to be used in thinner, smaller aircraft wings.
Key Features and Innovation
- Compact design to fit within thinner aircraft wings.
- Utilizes a linear actuator and motion linkage for operation.
- Attached to the wingbox structure at two points.
- Rib frame design for structural support.
Potential Applications
The technology can be applied in the aerospace industry for various aircraft models that require efficient and compact flap mechanisms.
Problems Solved
This technology addresses the need for flap mechanisms that can fit within thinner and smaller aircraft wings without compromising functionality.
Benefits
- Allows for the use of thinner and smaller aircraft wings.
- Provides efficient operation with a linear actuator.
- Enhances the overall performance of the aircraft.
Commercial Applications
Commercial aircraft manufacturers can benefit from this technology by incorporating it into their designs to improve aerodynamic efficiency and performance.
Prior Art
Readers can explore prior patents related to aircraft wing flap mechanisms to understand the evolution of this technology.
Frequently Updated Research
Stay updated on advancements in aircraft wing technology and innovations in flap mechanisms to enhance your understanding of the field.
Questions about Aircraft Wing Flap Mechanisms
How does the linear actuator driven flap mechanism improve aircraft performance?
The linear actuator driven flap mechanism enhances aircraft performance by providing efficient operation and allowing for the use of thinner wings, which can improve aerodynamic efficiency.
What are the key components of the rib frame design in the flap mechanism?
The rib frame design of the flap mechanism includes two webs that define the width of the mechanism, providing structural support for the linear actuator and motion linkage.
Original Abstract Submitted
A linear actuator driven flap mechanism for an aircraft wing is contained within a wing support and fairing of the aircraft wing. The rib frame of the flap mechanism is attached to the wingbox structure of the aircraft wing at a first and second point. The rib frame of the flap mechanism defines a width with a first and second web. A linear actuator and a motion linkage are positioned with the width between the first and second webs of the rib frame. The linear actuator is not mechanically driven rotary actuation or mechanically driven linear actuation. As a result of the compact construction, the flap mechanism can be employed in thinner, smaller aircraft wings being designed today.
