这是我们最新精选的关于航空学的全球出版物和专利(英文),涉及许多科学在线期刊,分类并侧重于航空学、空气动力学、航空电子学、推力、小翼、机翼、机身、飞行包络和马赫数。
Multi-directional input device
Patent published on the 2026-05-21 in WO under Ref WO2026105176 by NINTENDO CO LTD [JP] (Inoue Masanori [jp], Okamura Takanori [jp], Jinguji Gagaku [jp], Takei Masaya [jp], Minagawa Shinta [jp])
Abstract: A multi-directional input device according to the present embodiment comprises: a housing; an operation member that protrudes from the housing and can be tilted; a first interlocking member that holds the operation member so as to be able to rotate in a second direction (X), and is held by the housing so as to be able to rotate in a first direction (Y) that is orthogonal to the second direction in response to a tilting operation of the operation member; a second interlocking member that is held [...]
Our summary: The device features a housing with a tiltable operation member. It includes interlocking members that allow rotation in two orthogonal directions. Detection units and a biasing mechanism ensure accurate operation and return to a neutral position.
multi-directional input device, rotation detection, interlocking mechanism, biasing member
Patent
Turbofan engine including a fan actuation system
Patent published on the 2026-05-21 in US under Ref US20260139602 by GEN ELECTRIC [US] (Vondrell Randy M [us], Miedema Keith A [us], Sibbach Arthur W [us], Kray Nicholas J [us])
Abstract: A turbofan engine for an aircraft includes a fan and a fan actuation system. The fan has a plurality of fan blades coupled to a fan shaft having one or more fan bearings. The fan blades are rotatable about a pitch axis. The fan actuation system is disposed within a fan hub and includes one or more actuators for rotating the fan blades about the pitch axis and one or more radial thrust bearings. The fan actuation system is characterized by a fan actuation system length envelope in a range from 8.[...]
Our summary: The turbofan engine includes a fan with rotatable blades and a fan actuation system. The actuation system features actuators for adjusting blade pitch and radial thrust bearings. Its length envelope is defined by specific parameters related to the fan blades and bearings.
Turbofan engine, fan actuation system, fan blades, thrust bearings
Patent
A ship with a ship hull thruster
Patent published on the 2026-05-20 in EP under Ref EP4745020 by ECO LINE THRUSTER TECH B V [NL] (Van Der Laan Markus [nl])
Abstract: A ship hull thruster that offers excellent manoeuvrability without increasing sailing resistance. The ship hull thruster comprises a water duct comprising a water inlet at a first end of said water duct and a water outlet at a second end of said water duct; at least one water pump enclosed in the first end of said water duct for pumping water towards the second end of the water duct, wherein said nozzle is rotatable by an angle up to 360 degrees around an axis parallel to a yaw axis of the ship,[...]
Our summary: The ship hull thruster enhances manoeuvrability while minimizing sailing resistance. It features a water duct with an inlet and outlet, along with a pump to move water. The nozzle can rotate up to 360 degrees, aligning with the ship hull when not in use.
ship hull thruster, manoeuvrability, water duct, nozzle rotation
Patent
System for propelling watercraft, watercraft, and method of propelling watercraft
Patent published on the 2026-05-20 in EP under Ref EP4745023 by YAMAHA MOTOR CO LTD [JP] (Ikegaya Yuji [jp])
Abstract: The present watercraft propulsion system includes a principal propulsion device, an auxiliary propulsion device, a steering actuator, a steering motor, and a main controller. The principal propulsion device is attached to a hull of a watercraft. The auxiliary propulsion device is attached to the hull and has a smaller rated output than the principal propulsion device. The steering actuator changes a rudder angle of the principal propulsion device. The steering motor changes a rudder angle of the[...]
Our summary: The system includes a principal and auxiliary propulsion device for watercraft. The steering actuator and motor adjust rudder angles for effective maneuvering. The main controller ensures coordinated operation between the propulsion devices during steering.
propulsion system, watercraft, steering actuator, main controller
Patent
Wind turbine
Patent published on the 2026-05-20 in UA under Ref UA163085U by NATIONAL UNIV OF WATER AND ENVIRONMENTAL ENGINEERING [UA] (Serilko Leonid Stepanovych [ua], Serilko Dmytro Leonidovych [ua], Hlinchuk Nazarii Valeriiovych [ua])
Abstract: Wind turbine consists of a rotor containing parallel cross-members, in the trunnions of which blades of aerodynamic shape are fixed. The rotor is placed horizontally. The blades are attached to the cross-members in such a way that the plane of the blade passes through the axis of the cross-member, ensuring the optimal angle of attack for a given blade profile.[...]
Our summary: Wind turbines feature a horizontally placed rotor with parallel cross-members. Aerodynamic blades are fixed to these cross-members. The design ensures optimal angle of attack for efficiency.
wind turbine, rotor, aerodynamic blades, angle of attack
Patent
Vertical axis wind turbine power with aerodynamic brake
Patent published on the 2026-05-20 in EP under Ref EP4745397 by JEZEWSKI ANDRZEJ [PL] (Jezewska Elzbieta [pl], Jezewski Andrzej [pl], Jezewski Wojciech [pl])
Abstract: [0001] A vertical axis wind turbine (VAWT) power featuring an aerodynamic brake, comprising a rotor permanently coupled to a rotating shaft which is further linked to an electric generator. The turbine is characterized in that it includes at least a lower module (B) rotor and at least an upper rotor (A), wherein these rotors are permanently mounted on a common rotating axis at different axial heights, and the rotor of the lower module (B) is a Savonius-type drag rotor equipped with external flow[...]
Our summary: The content describes a vertical axis wind turbine (VAWT) with an aerodynamic brake. It features a Savonius-type drag rotor in a lower module and a lift-driven rotor in an upper module. The design allows for enhanced efficiency by utilizing different rotor types at varying axial heights.
Vertical axis wind turbine, aerodynamic brake, Savonius rotor, electric generator
Patent
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
Publication
Prediction and Suppression of Liquid Propellant Sloshing-Induced Oscillation in RLV Terminal Flight
Published on 2026-02-03 by Yuzhou Liao, Shuguang Zhang, Zhiyue Xiong, Pengxin Han @MDPI
Abstract: During the reentry terminal flight of lifting-body Reusable Launch Vehicles (RLVs) propelled by liquid fuel, the sloshing of liquid propellent presents new features that, if neglected, could lead to adverse flight oscillations or even worse. This paper focuses on liquid sloshing coupled flight dynamics, sloshing effect prediction, and the suppression of adverse flight oscillations. First, a transfer function model for unsteady aerodynamics is improved and applied to describe the sloshing force e[...]
Our summary: This paper addresses the impact of liquid propellant sloshing on the flight dynamics of Reusable Launch Vehicles (RLVs). It presents an improved transfer function model to predict sloshing-induced oscillations and evaluates suppression control measures. Simulations confirm that the proposed compensation control effectively mitigates adverse oscillations caused by sloshing.
Liquid Propellant, Sloshing Dynamics, Flight Oscillations, Control Measures
Publication