Dies ist unsere neueste Auswahl an weltweiten Veröffentlichungen und Patenten in englischer Sprache zum Thema Luftfahrt, die in zahlreichen wissenschaftlichen Online-Zeitschriften zu den Themen Luftfahrt, Aerodynamik, Avionik, Schub, Winglet, Leitwerk, Rumpf, Flugumschlag und Machzahl veröffentlicht wurden.
Powerline unmanned surfer
Patent published on the 2026-10-15 in WO under Ref WO2026217081 by THE BOARD OF REGENTS OF OKLAHOMA AGRICULTURAL AND MECH COLLEGES [US] (Faruque Imraan A [us], Patel Ujjval [us])
Abstract: A system and method for achieving powerline energy harvesting power are disclosed herein. The method comprises sensing a position and trajectory of a plurality of points of a powerline relative to a position and a trajectory of a UAV having an aerodynamic surface; estimating a local spatial wavelength (alternatively or additionally, spatial frequency) of the powerline having a catenary curve using a point cloud indicative of the plurality of points of the powerline; and modulating at least one a[...]
Our summary: The system enables powerline energy harvesting using an unmanned aerial vehicle (UAV). It senses the powerline s position and trajectory to estimate local spatial wavelengths. The UAV s aerodynamic surface is modulated to maintain parallel flight with the powerline.
Powerline energy harvesting, UAV trajectory estimation, aerodynamic surface modulation, catenary curve analysis
Patent
Watercraft having a retractable lift-propulsion system
Patent published on the 2026-10-15 in US under Ref US20260316904 by BOMBARDIER RECREATIONAL PRODUCTS INC [CA] (Godbout Hugo [ca], Gendron Jean-philippe [ca])
Abstract: A watercraft, a propulsion control system of the watercraft, and a method of controlling a propulsion unit of the watercraft. The watercraft includes a buoyant body and a retractable lift-propulsion system. The retractable lift-propulsion system includes a mast, moveable between a retracted and a deployed position, and a lift-propulsion assembly attached to the mast. The lift propulsion assembly includes a hydrofoil and a propulsion unit for providing thrust to the watercraft. The watercraft inc[...]
Our summary: The watercraft features a retractable lift-propulsion system with a mast and hydrofoil. A control unit manages the propulsion unit based on mast position signals from a sensor assembly. This system enhances the watercraft s buoyancy and thrust capabilities.
retractable lift-propulsion, watercraft, hydrofoil, propulsion control system
Patent
Flight device
Patent published on the 2026-10-15 in WO under Ref WO2026216466 by ISHIKAWA ENERGY RES CO LTD [JP] (Ishikawa Mitsuru [jp], Sekita Takahito [jp])
Abstract: Provided is a flight device capable of absorbing a difference in load between a main rotor and a sub rotor. An airframe 11 of a flight device 10 is configured to accommodate an engine 12 and a generator 13. The engine 12 generates power for rotationally driving a main rotor 15 and a sub rotor 16, the generator 13 is driven by the engine 12 to generate power for rotationally driving a motor 14, the motor 14 is rotationally driven by the power supplied from the generator 13, the main rotor 15 is[...]
Our summary: The flight device absorbs load differences between the main rotor and sub rotor. It includes an engine for driving the main rotor and a generator powering a motor for the sub rotor. A power conversion unit adjusts generator output or main rotor thrust.
flight device, main rotor, sub rotor, power conversion
Patent
Method for controlling coaxial multi-rotor aircraft, apparatus, and related device
Patent published on the 2026-10-15 in WO under Ref WO2026214215 by MEITUAN TECH CO LTD [CN] (Li Tuo [cn], Hu Lingyun [cn], Long Jinwei [cn], Liu Baoxu [cn], Mao Yinian [cn], Huang Guoquan [cn])
Abstract: The present disclosure provides a method for controlling a coaxial multi-rotor aircraft, an apparatus, and a related device. The method comprises: constructing a first objective function on the basis of single-axis thrust corresponding to each axis of a coaxial multi-rotor aircraft, and the roll moment, pitch moment and lift of the body of the coaxial multi-rotor aircraft; constructing a second objective function on the basis of single-axis torque corresponding to each axis and a yaw moment of t[...]
Our summary: The method controls a coaxial multi-rotor aircraft using two objective functions. It minimizes thrust and torque for each axis to determine rotor speeds. The aircraft is then controlled based on these calculated rotor speeds.
coaxial multi-rotor, control method, objective function, thrust and torque
Patent
An aeronautical energy network system
Patent published on the 2026-10-15 in US under Ref US20260321751 by AIRBUS OPERATIONS S L U [ES] (De Brouwer Gabrielle Josephine Christiane [es], HernÁndez Hidalgo Carlos [es])
Abstract: [0000] An aeronautical energy network system (100, 101) with an energy network having a defined nominal voltage operating range (Vr) to which electrical loads (11,12) and a battery are connected. Cells of the battery are arranged in cell groups being the cells forming a group connected in series in a fixed manner. The battery having an electrical connection circuit with controllable switch configured to at least selectively connect cell groups to each other in series or in parallel producing, in[...]
Our summary: The system includes an energy network with a defined nominal voltage range. It connects electrical loads and a battery with cell groups arranged in series. A controller manages the connection state of the battery to maintain the output voltage within the network s operating range.
Aeronautical, Energy Network, Battery Management, Voltage Control
Patent
Aerodynamic component with film cooling passage for a gas turbine
Patent published on the 2026-10-14 in EP under Ref EP4822140 by ROLLS ROYCE PLC [GB] (Heyen Sabina [de], Murphy Adrian [de], King Tom [de], Sikorski Igor [de])
Abstract: An aerodynamic component for a gas turbine. The aerodynamic component has a wall-shaped body with a first surface on a first side of the wall-shaped body, and a second surface on a second side of the wall-shaped body. The second side is opposite of the first side. The wall-shaped body has at least one channel extending from an inlet at the first surface to an outlet at the second surface. A bead extends at least partially around a circumference of the outlet. The bead protrudes away from the sec[...]
Our summary: The aerodynamic component features a wall-shaped body with distinct first and second surfaces. It includes a channel that connects an inlet on the first surface to an outlet on the second surface. A protruding bead surrounds the outlet, enhancing cooling efficiency.
aerodynamic component, gas turbine, film cooling, wall-shaped body
Patent
Prompt-guided diffusion approach for deep generative vehicle designs under user-defined specifications
Published on 2026-06-24 by @OXFORD
Abstract: AbstractEngineering vehicle design presents significant challenges due to its resource-intensive nature and the need to satisfy diverse design requirements. While recent data-driven generative models have shown promise, key limitations remain: (1) the difficulty of simultaneously addressing multiple design factors, such as user intent and engineering validity, and (2) the lack of accessibility and user-friendliness for intuitive design exploration. To overcome these challenges, this study introd[...]
Our summary: This study presents a prompt-guided diffusion framework for generating high-fidelity vehicle designs. It addresses challenges in engineering design by integrating user-defined specifications with generative models. Evaluations show significant improvements in design quality and generalization under data-scarce conditions.
diffusion framework, generative design, vehicle engineering, user-defined specifications
Publication
CFD-based analysis of chimney performance optimization for the Manzanares pilot plant
Published on 2026-03-19 by @OXFORD
Abstract: AbstractThis research conducts an extensive computational fluid dynamics (CFD) analysis aimed at optimizing the geometric configuration of solar chimney power plants (SCPPs), with particular emphasis on the Manzanares pilot plant. The research analyses the effects of chimney diameter and divergent chimney design on system performance under steady-state conditions at 1000 W/m2 solar irradiance and 300 K ambient temperature. A validated three-dimensional CFD model with a 90° symmetry sector is [...]
Our summary: This research utilizes CFD to optimize chimney design for the Manzanares pilot plant. The study finds that increasing chimney diameter significantly boosts power output, while a divergent configuration further enhances performance. Optimal design parameters lead to substantial improvements in airflow and energy generation, providing a cost-effective solution for future installations.
CFD, chimney optimization, solar chimney power plants, aerodynamic design
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