18519459. MOVABLE FLOW BODY HAVING A HYBRID LOAD INTRODUCTION RIB simplified abstract (Airbus Operations GmbH)
Contents
- 1 MOVABLE FLOW BODY HAVING A HYBRID LOAD INTRODUCTION RIB
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 MOVABLE FLOW BODY HAVING A HYBRID LOAD INTRODUCTION RIB - 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
MOVABLE FLOW BODY HAVING A HYBRID LOAD INTRODUCTION RIB
Organization Name
Inventor(s)
Stefan Bensmann of HAMBURG (DE)
Alexander Burchard of HAMBURG (DE)
MOVABLE FLOW BODY HAVING A HYBRID LOAD INTRODUCTION RIB - A simplified explanation of the abstract
This abstract first appeared for US patent application 18519459 titled 'MOVABLE FLOW BODY HAVING A HYBRID LOAD INTRODUCTION RIB
Simplified Explanation
The patent application describes a movable flow body for an aircraft with a front skin that has an outer surface for contact with an ambient flow and an inner surface. The body includes load introduction ribs with coupling elements on the drive side for connection to a drive mechanism, and interface elements attached to the front skin interface side, bonded to the inner surface of the front skin.
- The movable flow body for an aircraft includes:
- Front skin with outer and inner surfaces
- Load introduction ribs with coupling elements
- Interface elements bonded to the inner surface of the front skin
Potential Applications
The technology could be applied in the aerospace industry for aircraft design and development, specifically in improving aerodynamic performance and control systems.
Problems Solved
1. Enhanced aerodynamic performance 2. Improved control mechanisms for aircraft
Benefits
1. Increased efficiency in airflow management 2. Enhanced maneuverability and control of the aircraft
Potential Commercial Applications
Optimizing aircraft design for better performance and control systems in commercial aviation.
Possible Prior Art
There may be prior art related to movable flow bodies for aircraft, but specific examples are not provided in the abstract.
Unanswered Questions
How does this technology compare to existing movable flow body designs in terms of efficiency and performance?
The article does not provide a direct comparison with existing designs to evaluate the advantages of this technology.
What are the specific materials and manufacturing processes used in creating the interface elements for bonding to the inner surface of the front skin?
The details of the materials and manufacturing processes for the interface elements are not mentioned in the abstract.
Original Abstract Submitted
A movable flow body for an aircraft including a front skin having an outer surface configured to be contacted by an ambient flow, and an inner surface opposite the outer surface, at least one load introduction rib having a skin interface side and a drive side, at least one coupling element arranged on the drive side for coupling with a drive mechanism, and at least one interface element removably attached to the front skin interface side. The at least one interface element includes a bonding surface having a shape corresponding to the shape of the inner surface of the front skin. The at least one interface element is materially bonded to the inner surface of the front skin.
