18519478. WING FOR AN AIRCRAFT simplified abstract (Airbus Operations GmbH)
Contents
- 1 WING FOR AN AIRCRAFT
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 WING FOR AN AIRCRAFT - 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
WING FOR AN AIRCRAFT
Organization Name
Inventor(s)
Bernhard Schlipf of HAMBURG (DE)
WING FOR AN AIRCRAFT - A simplified explanation of the abstract
This abstract first appeared for US patent application 18519478 titled 'WING FOR AN AIRCRAFT
Simplified Explanation
The patent application describes an aircraft wing with a trailing edge high lift assembly that includes a flap and a connection assembly. The flap can be moved between retracted and extended positions, with a gap present between the main wing lower rear panel and the flap leading-edge section in the extended position. A gap closing device is included to minimize the gap in both retracted positions and open it in the extended position.
- Aircraft wing with trailing edge high lift assembly
- Flap movable between retracted and extended positions
- Gap present in extended position, closed or minimized in retracted positions
- Gap closing device to adjust the gap as needed
Potential Applications
The technology could be applied in the design and construction of aircraft wings to improve aerodynamic performance and efficiency.
Problems Solved
1. Improved lift and control of aircraft during flight. 2. Enhanced maneuverability and stability of the aircraft.
Benefits
1. Increased efficiency and fuel savings. 2. Better overall performance and safety during flight operations.
Potential Commercial Applications
Optimizing aircraft wing design for commercial airlines to improve fuel efficiency and reduce operating costs.
Possible Prior Art
One possible prior art could be the use of similar flap systems in aircraft wings for aerodynamic purposes.
Unanswered Questions
How does the gap closing device work exactly?
The patent application mentions a gap closing device, but the specific mechanism or technology behind it is not detailed. Further information on how this device operates would be beneficial for a deeper understanding of the innovation.
What are the specific performance improvements achieved with this technology?
While the abstract mentions improved aerodynamic performance and efficiency, specific data or metrics on the actual performance improvements resulting from this technology are not provided. More information on the quantifiable benefits of this innovation would be valuable for potential users or investors.
Original Abstract Submitted
An aircraft wing, including a main wing and a trailing edge high lift assembly movably arranged at a main wing trailing edge. The trailing edge high lift assembly includes a flap and a connection assembly movably mounting the flap to the main wing, the flap being movable between retracted and extended positions. In the extended position, a gap is present between a main wing lower rear panel and a flap leading-edge section. In the retracted position, the gap is closed or minimized. The flap is movable between the extended position, a first retracted position, and a second retracted position where the flap is moved beyond the first retracted position in a forward direction, and the wing includes a gap closing device configured to close or minimize the gap in both the first and second retracted flap positions, and to open the gap in the extended flap position.
