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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.

Aerodynamic movable tonneau cover

Patent published on the 2026-06-11 in US under Ref US20260158884 by FCA US LLC [US] (Partin Andrew L [us], Vincent Anthony L [us], Lewis Kivin Roberto-lee [us], Adam Aslam [us])

Abstract: A tonneau system for a vehicle including a cargo bed includes a cover coupled to a frame being movable between a deployed position and a retracted position. The frame is movable between a horizontal position and an aerodynamic position. A leading edge of the frame is positioned at a higher elevation than a trailing edge of the frame when the frame is at the aerodynamic position. A first side panel includes a first portion pivotally coupled to the frame and a second portion pivotally coupled to t[...]


Our summary: The system features a movable tonneau cover that transitions between horizontal and aerodynamic positions. The frame s leading edge is elevated in the aerodynamic position. A pivotally coupled side panel adjusts to close openings when in the aerodynamic position.

aerodynamic, tonneau cover, movable frame, vehicle cargo

Patent

Data security management

Patent published on the 2026-06-11 in US under Ref US20260161778 by HONEYWELL INT INC [US] (Govindillam Sreenivasan [in], Kosuri Sri Harsha [in], Selvarajan Ravikumar [in])

Abstract: Techniques for managing security of input data to be used with avionics are described. In one example implementation, the present subject matter facilitates in processing of the input data at different flight plan applications and determining a confidence level of the output data at different flight plan applications depending on a degree of agreement between the output data. Further, using the output data for calculating flight modification parameters if the output data is not corrupted.[...]


Our summary: The content discusses techniques for managing the security of input data in avionics. It describes processing input data for flight plan applications and determining the confidence level of output data. Additionally, it addresses calculating flight modification parameters based on the integrity of the output data.

data security, avionics, input data management, confidence level

Patent

Electromagnetically controlled flapping wing aerial device

Patent published on the 2026-06-11 in WO under Ref WO2026122076 by KATO KIYENGO JEFFREY [UG] (Kato Kiyengo Jeffrey [ug])

Abstract: The present invention relates to a flapping-wing aerial body capable of controlled flight using electromagnetically driven wing motion. The invention mimics the flight dynamics of insects, such as wasps and bees, by creating lift and thrust through the up-and-down movement of its wings. Electromagnets are employed to attract and release metallic plates connected to the wings, causing them to flap. This motion allows the aerial body to move in multiple directions, including forward, backward, lef[...]


Our summary: The invention is an electromagnetically controlled flapping wing aerial device that mimics insect flight dynamics. It uses electromagnets to drive wing motion for multi-directional movement and precise control. This design offers a compact and energy-efficient alternative to conventional drone technologies.

flapping wing, electromagnet, microcontroller, UAV

Patent

A door release mechanism

Patent published on the 2026-06-11 in WO under Ref WO2026122054 by TUSAS TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI [TR] (Ozturk Ersin [tr], Sanli Tahir Volkan [tr], Doda Pinar [tr])

Abstract: The present invention relates to a fuselage (G) which is an aircraft, at least one door located on the fuselage (G) for providing a passenger with access into or out of the fuselage (G); at least one hinge located on the fuselage (G) providing for the pivoting of the door such that it can move on the fuselage (G); at least one fastener providing for the securing of the door to the fuselage (G) by means of the hinge; a handle located within the fuselage (G) so as to be accessible to a user; a fir[...]


Our summary: The invention describes a door release mechanism for an aircraft fuselage. It includes a hinge for pivoting the door and a handle accessible to the user. The mechanism allows the door to transition between fixed and separated positions via a rod that transmits motion from the handle to the fastener.

door release mechanism, aircraft fuselage, pivoting hinge, user handle

Patent

Coupled aerodynamic and optical sizing of airborne particles

Patent published on the 2026-06-11 in US under Ref US20260160664 by AEROSOL DYNAMICS INC [US] (Hering Susanne Vera [us], Amanatidis Stavros [us])

Abstract: [0000] A method and apparatus for aerodynamic sizing of particles are disclosed. An airflow containing particles is introduced into an inlet at or near atmospheric pressure and passed through a focusing acceleration nozzle. The nozzle rapidly accelerates the flow at an exit into a measurement chamber. A light beam is focused near the nozzle exit, and a detector measures light scattered by particles passing through the beam. A signal measurement device determines the transit time of individual pa[...]


Our summary: A method for sizing airborne particles combines aerodynamic and optical techniques. Particles are accelerated through a nozzle and measured via scattered light. The system outputs a size distribution based on transit times and calibration standards.

aerodynamic sizing, optical sizing, particle measurement, light scattering

Patent

Generating attribute labels for aviation notices

Patent published on the 2026-06-11 in US under Ref US20260162540 by HONEYWELL INT INC [US] (Shamasundar Raghu [in], Dani Minal [in], Desarkar Munendra [in], Kamath Mythili [in], Mallavarapu Sreedhara [in])

Abstract: [0000] Approaches for generating attribute labels for aviation notices are described. According to one example, a system employs a machine learning pipeline to analyse and label aviation notices with pre-defined formats. The process involves tokenizing the aviation notices, generating vector embeddings, and using models such as Bidirectional Long Short-Term Memory (BiLSTM) and Conditional Random Field (CRF) to identify attributes and assign labels. The system incorporates pre-defined rules, real[...]


Our summary: A system uses a machine learning pipeline to analyze and label aviation notices. It employs tokenization, vector embeddings, and models like BiLSTM and CRF to identify attributes. The labeled notices are sent to various devices for real-time updates and anomaly detection.

machine learning, attribute labeling, aviation notices, anomaly detection

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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