US Patent : https://lnkd.in/dqmiyb7b / https://lnkd.in/eRPM_K-Z
RES-Morphing Wing, please see independent claims 20-25 for Fig. 24.
The invention is an asymmetric wing profile with an adjustment device. The profile has a thickness and a chord extending between the wing's leading and trailing edges. The profile has a three-part, variable wing in at least one longitudinal section. The front and rear wing segments are connected to the middle wing segment via two hinges with axes of rotation. These segments are designed to enable rotational movement about an associated axis in relation to the middle wing segment. The middle wing segment forms a rigid housing that accommodates the adjustment device. The longitudinal element of the asymmetric blade profile is a hollow profile that forms an abutment for the adjustment device in at least one longitudinal section. The adjustment device contains at least one electric motor in the middle blade segment. With the help of an electric motor, the front and rear wing segments can be swung in opposite directions. This creates a variable suction side of the asymmetric wing profile. This adjusts the angle of attack of the profile line as the wing segments are swung in or out. In a preferred embodiment, the adjustment device is equipped with a step gear. At least one longitudinal section of the asymmetric wing profile is connected to the retaining element of the adjustment device, as are the middle wing segment with at least one electric motor and the front and rear wing segments of the three-part wing profile. This connection enables the lift generated by the suction side of the variable wing profile to adapt to the aircraft's flight situation through actuation of the adjustment device.
#resmw1 #resewing #resmorphingwing #drones #airplains #cars #racing #composites #sustainabledevelopment #aviation #thefutureiselecric #engineering #engineeredmind #aerodynamics #aam #uam #evtol #electricaircraft #mechanical #engineering res-institute.com
res-institute.com

US Patent : https://lnkd.in/dqmiyb7b / https://youtu.be/BA1f6diP4fY
RES-Morphing Wing, please see independent claims 20-25 for Fig. 24.
This invention is an electrically actuated, variable, asymmetrical wing profile that can be used as an adaptive wing on an aircraft. Using AI control, a lidar system scans the air mass in front of the aircraft so that the wing can react instantly to changes in air density and airflow. The schematic cross-section of the wing illustrates the variable wing profile, excluding the electric actuators which are the subject of European and American patent applications.
#resmw2 #resewing #resmorphingwing #drones #airplains #lift #lidar #sensor #composites #aviation #thefutureiselecric #engineering #aerodynamics #aam #uam #evtol #electricaircraft #mechanical #engineering
res-institute.com

US Patent : https://lnkd.in/dqmiyb7b / https://youtu.be/iWuc4beP0Ug
RES-Morphing Wing, please see independent claims 20-25 for Fig. 24.
The middle wing segment of the variable, three-part, asymmetrical wing profile is designed to support an airfoil. The nose and trailing edge segments are hinged to the middle wing segment via redundant electric actuators.
#resmw3 #resewing #resmorphingwing #drones #airplains #lift #lidar #sensor #composites #aviation #thefutureiselecric #engineering #aerodynamics #aam #uam #evtol #electricaircraft #mechanical #engineering
res-institute.com

US Patent : https://lnkd.in/dqmiyb7b / https://youtu.be/OpXS06qyJz0
RES-Morphing Wing, please see independent claims 20-25 for Fig. 24.
This invention is an electrically actuated, variable, asymmetrical wing profile that can be used as an adaptive wing on an aircraft. Using AI control, a lidar system scans the air mass in front of the aircraft so that the wing can react instantly to changes in air density and airflow. The schematic cross-section of the wing illustrates the variable wing profile, excluding the electric actuators which are the subject of European and American patent applications.
#resmw4 #resewing #resmorphingwing #drones #airplains #lift #lidar #sensor #composites #aviation #thefutureiselecric #engineering #aerodynamics #aam #uam #evtol #electricaircraft #mechanical #engineering
res-institute.com

US Patent : https://lnkd.in/dqmiyb7b / https://youtu.be/Nizgd0f1a7g
RES-Morphing Wing, please see independent claims 20-25 for Fig. 24.
The invention is an asymmetrical wing profile with an adjustment device. The profile has a thickness and a chord that extends between the wing's leading and trailing edges. The profile consists of a three-part variable wing in at least one longitudinal section. The front and rear wing segments are hinged to the middle wing segment via two hinges with axes of rotation. These segments are designed to enable rotational movement about an associated axis relative to the middle wing segment. The middle wing segment forms a rigid housing that accommodates the adjustment device. The asymmetrical blade profile's longitudinal element is a hollow profile that forms a bearing for the adjustment device in at least one longitudinal section. The adjustment device contains at least one electric motor in the middle blade segment. With the aid of the motor(s), the front and rear wing segments can pivot in opposite directions, creating a variable suction side of the asymmetrical wing profile. Pivoting the front and rear wing segments in or out changes the angle of attack of the profile line. The US patent describes a wing profile in which the joints are offset from the chord line. This allows a super-lift position to be achieved during takeoff and landing through an air gap that opens between the wing segments. Once the aircraft reaches its operating altitude, electric actuators on the wing's suction side enable quick reactions to the air masses in front of the aircraft. The aircraft then glides through the air with minimal drag, sparing passengers and crew uncomfortable lateral acceleration during flight. This invention fulfills the concept of a variable wing and could be realized already in the near future.
#resmw5 #resewing #resmorphingwing #drones #airplains #lift #lidar #sensor #composites #aviation #thefutureiselecric #engineering #aerodynamics #aam #uam #evtol #electricaircraft #mechanical #engineering
res-institute.com

US Patent : https://lnkd.in/dqmiyb7b / https://youtu.be/Nizgd0f1a7g
RES-Morphing Wing, please see independent claims 20-25 for Fig. 24.
This is the only morphing wing that can be built right away. This innovative design integrates electric actuators into the wing for the nose-side slats and trailing-edge flaps. If you look closely, you will notice the absence of canoes, also known as flap jacks or track fairings, on the underside of the wing. As demonstrated in video #resmw5, these actuators enable the wing profile to transition to a laminar flow configuration in fractions of a second. This allows the aircraft to respond to changes in air mass during flight with both wings, ensuring that passengers enjoy the smoothest and most comfortable journey possible. This is made possible by a lidar system integrated into the wings. The fully electric slat and flap actuators do not interfere with the integration of the fuel tanks (shown in red) into the central wing spar, which is rigidly connected to the fuselage. The video also shows the high-lift configuration of the wings required for takeoff and landing. In the high-lift configuration, the wing surface area increases due to an eccentric arrangement of joints connected to the center spar. Additionally, the space between the center wing segment and the slats and flaps is ventilated.
#resmw6 #resewing #resmorphingwing #drones #airplains #cars #racing #composites #sustainabledevelopment #aviation #thefutureiselecric #engineering #engineeredmind #aerodynamics #aam #uam #evtol #electricaircraft #mechanical #engineering
res-institute.com

US Patent : https://lnkd.in/dqmiyb7b / https://youtu.be/Nizgd0f1a7g
RES-Morphing Wing, please see independent claims 20-25 for Fig. 24.
The invention relates to an asymmetrical wing profile with an adjustment device. The profile has a thickness and a chord that extends between the wing's leading and trailing edges. Designed in at least three parts, the profile has a central spar to which the front and rear wing segments are connected via two joints with axes of rotation. The hairline gaps between the three wing segments ensure laminar airflow around the profile in every wing position. The middle wing segment forms a rigid housing for the actuators. With the aid of electric motors, the front and rear wing segments can pivot in opposite directions, creating a variable suction side of the asymmetrical wing profile. This adjusts the profile chord's angle of attack when the front and rear wing segments are pivoted in or out. In a preferred embodiment, the adjustment device is equipped with a step-locking gear.
#resmw7 #resewing #resmorphingwing #cars #spoilers #racing #composites #thefutureiselecric #engineering #engineeringexcellence #aerodynamics #electricaircraft #mechanical
res-institute.com

US Patent : https://lnkd.in/dqmiyb7b / https://youtu.be/Nizgd0f1a7g
RES-Morphing Wing, please see independent claims 20-25 for Fig. 24.
The invention relates to a symmetrical wing profile consisting of at least three parts with an adjustment device. The profile has a thickness and a chord extending between the wing's leading and trailing edges. In this embodiment, the front and rear wing segments are designed with multiple parts and a central joint chain. These kinematic hinge chains have an abutment formed by the middle wing segment and can be controlled by pushrods, allowing the wing profile to move from a symmetrical basic position to a lift or downforce position. The central wing segment forms a rigid housing that accommodates the electrical actuators. The central wing segment of the symmetrical wing profile is a rigid, hollow profile that resists thrust, bending, and torsion. It serves as a rigid abutment for the nose and trailing edge segments, which are connected to the body of the sports car. The adjustment device contains at least one electric motor in the middle wing segment. With the help of the motor(s), the front and rear wing segments can pivot in opposite directions. In a preferred embodiment, the adjustment device is equipped with a step-locking gear. #resmw8 #resewing #resmorphingwing #cars #spoilers #racing #composites #thefutureiselecric #engineering #engineeringexcellence #aerodynamics #electricaircraft #mechanical
res-institute.com