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Latest Publications & Patents on Aeronautics

. Latest Publications & Patents on Aeronautics. Aerodynamics

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This is our latest selection of worldwide publications and patents in english on Aeronautics, between many scientific online journals, classified and focused on aeronautic, aerodynamic, avionic, thrust, winglet, empennage, fuselage, flight envelope and Mach number.

Fuel cell cooling system as vehicle control mechanism

Patent published on the 2026-07-01 in EP under Ref EP4768393 by HONEYWELL INT S R O [CZ] (Trnka Pavel [us], Kotaba Ondrej [us])

Abstract: A fuel cell cooling system is provided. The fuel cell cooling system is a vehicle system that may be a yaw control mechanism for a vehicle. Additionally or alternatively, the fuel cell cooling system may be a pitch control mechanism. A vehicle may include a fuel cell system and a fuel cell cooling system. The fuel cell cooling system may include one or more heat exchangers connected to the fuel cell system to cool a first cooling medium; one or more air motive flow sources configured to receive [...]


Our summary: A fuel cell cooling system acts as a yaw and pitch control mechanism for vehicles. It includes heat exchangers to cool a medium and air motive flow sources to generate airflow. Directional thrusters direct the cooled air as thrust for vehicle control.

fuel cell, cooling system, vehicle control, heat exchangers

Patent

Method of estimating the pitch angle of a rotor blade for an aircraft, and rotor for an aircraft

Patent published on the 2026-07-01 in EP under Ref EP4768387 by LEONARDO SPA [IT] (Novembrini Giovanni [it], Brunetti Massimo [it], Manenti Giuseppe [it], Zaccaria Alessio [it], Nesci Andrea [it], Delli Paoli Michele [it])

Abstract: A method is described for estimating the pitch angle (γ) of the blades of a rotor (10, 10 ) of an aircraft capable of hovering comprising a motor member with a stator and an output shaft rotatable about the stator; a hub rotatable about the axis (B) and operatively connected with the output shaft so as to be rotatable with an angular velocity (ω) about the axis (B); at least two blades rotatable about the axis (B) and about corresponding second axes (D) of extension of the blades, so as to adj[...]


Our summary: The method estimates the pitch angle of rotor blades in an aircraft. It involves computing various torque and thrust coefficient values. The final pitch angle is derived from comparisons with threshold values.

pitch angle, rotor blade, torque computation, thrust coefficient

Patent

Flow accelerator device for enhancing ventilation and smoke extraction and uses thereof

Patent published on the 2026-07-01 in EP under Ref EP4768719 by ASSOCIACAO BLC3 CAMPUS DE TECNOLOGIA E INOVACAO [PT] (Dos Santos Almeida Nunes JoÃo Miguel [pt], Nunes Pereira Cid Teles JoÃo Manuel [pt], Francisco De Figueiredo Filipa Daniela [pt])

Abstract: [0001] The present disclosure provides a flow accelerator device comprising an inverted aerofoil-shaped cross-section formed by one or more panels, defining a leading edge, trailing edge, upper surface, and lower surface, where the lower surface extends further than the upper surface. Mechanically connected to a base fixed upstream of a duct, the device generates low pressure within the duct to enhance air extraction. By leveraging aerodynamic principles, the device increases airflow efficiency [...]


Our summary: The flow accelerator device enhances ventilation and smoke extraction using an inverted aerofoil-shaped design. It generates low pressure in ducts to improve airflow efficiency in various structures. The device operates passively, promoting sustainable indoor air quality management.

flow accelerator, ventilation, smoke extraction, aerodynamic principles

Patent

Planetary gear arrangement for a distribution gearing

Patent published on the 2026-07-01 in EP under Ref EP4768294 by ZAHNRADFABRIK FRIEDRICHSHAFEN [DE] (Fan Zhenhua [cn], Li Tingting [cn], Sun Jiabin [cn], Fei Ningzhong [cn])

Abstract: [0001] The present disclosure relates to a planetary gear arrangement for a distribution gearing, comprising a first structure, a planet gear rotatable about an axis of rotation relative to the first structure and a first thrust bearing. The first thrust bearing has a first bearing element and a second bearing element rotatable relative to the first bearing element. The first thrust bearing is arranged between the planet gear and the first structure in the direction of the axis of rotation. A to[...]


Our summary: The document describes a planetary gear arrangement for distribution gearing. It includes a planet gear, thrust bearing elements, and a mechanism for torque transfer. Additionally, it relates to vehicles utilizing this gear arrangement and distribution gearing.

planetary gear, thrust bearing, torque transfer, distribution gearing

Patent

A load dampuing apparatus

Patent published on the 2026-07-01 in EP under Ref EP4768385 by TUSAS TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI [TR] (Eryilmaz Emre Onur [tr])

Abstract: [0001] This invention relates to a body in an aircraft, a cockpit in the form of a cabin on the body, in which the pilot is located, a panel located in the cockpit, on which the avionic devices are positioned and which is accessible to the pilot, a plurality of beams forming the side walls of the cockpit, arranged longitudinally opposite each other so that the cockpit is located between them, at least one damper located in the cockpit, damping the loads on the panel in the cockpit.[...]


Our summary: This invention describes a load damping apparatus for an aircraft cockpit. It includes a panel for avionic devices accessible to the pilot. The design features beams forming side walls to support the cockpit and dampen loads effectively.

load damping, aircraft cockpit, avionic devices, structural beams

Patent

Thrust addition

Patent published on the 2026-06-24 in EP under Ref EP4764194 by KELLY PHILIP [CA] (Kelly Philip [ca], Venturino Gemma [ca])

Abstract: A thrust-addition system is provided and configured to be mounted to a vehicle and is also configured to propel the vehicle forward. In accordance with example embodiments, a fan is arranged in a duct within a vehicle, such as an air vehicle, with blow-in intake doors, serving as a primary purpose of exhaust as a thrust addition system, while also providing temperature, humidity, velocity, and/or deflection at the outlet for a secondary purpose to reduce heat signature, contrails, radar cross se[...]


Our summary: A thrust-addition system is designed to enhance vehicle propulsion. It includes a fan in a duct with blow-in intake doors for exhaust. The system also mitigates heat signature and other detection factors.

Thrust addition, propulsion system, fan duct, heat signature

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

Topics covered: aeronautics, aerodynamic, avionic, thrust, winglet, empennage, fuselage, flight envelope, Mach number, azimuth sensing, True North, two-phase flow, hybrid electric aircraft, aerodynamic design, vertical tail, numerical simulation, dynamic stability, and URANS..

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(if date is unknown or not relevant, e.g. "fluid mechanics", a rounded estimation of its notable emergence is provided)

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