Results 11 to 20 of about 1,707 (248)

Analysis of unstable mode of a free gas turbine of turbo-compressors engines [PDF]

open access: yesMATEC Web of Conferences, 2021
This paper analyses unstable mode of a free gas turbine of turboshaft helicopter engine TV3-117. The analysis is focused on the conditions of this phenomenon and the possibilities of its solution in a turboshaft helicopter engine and an industrial ...
Hocko Marián, Al-Rabeei Samer
doaj   +1 more source

Preliminary investigation on the self-propulsion performance of wedge-shaped functional surfaces [PDF]

open access: yesJournal of Intelligent Manufacturing and Special Equipment, 2022
Purpose – The purpose of this paper is to artificially construct a functional surface with self-propulsion flow characteristics for the directional transportation of propellant in surface tension tanks.
Qianqian Li   +5 more
doaj   +1 more source

Influence of Engine Dynamic Characteristics on Helicopter Handling Quality in Hover and Low-Speed Forward Flight

open access: yesAerospace, 2023
This study assesses the influence of engine dynamic characteristics on helicopter handling quality during hover and low-speed forward flight. First, we construct the helicopter–engine coupling model (HECM) based on the power-matching relationship between
Yuan Wei   +3 more
doaj   +1 more source

Forming of turboshaft engine mathematical model

open access: yesАвіаційно-космічна техніка та технологія, 2023
The subject of the study is the process of forming a mathematical model (MM) of a turboshaft gas turbine engine and a twin-engine helicopter power plant, which provides the determination of parameters of the working process in steady and transient ...
Sergiy Yepifanov, Oleksii Bondarenko
doaj   +1 more source

STUDY ON SAFETY TECHNOLOGY SCHEME OF THE UNMANNED HELICOPTER [PDF]

open access: yesThe International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, 2013
Nowadays the unmanned helicopter is widely used for its' unique strongpoint, however, the high failure rate of unmanned helicopter seriously limits its further application and development.
Z. Lin   +4 more
doaj   +1 more source

Study on the Engagement Characteristics and Control Strategy of High Speed Difference Dry Friction Clutch

open access: yesMachines, 2023
In the short/vertical take-off and landing aircraft propulsion system, the vertical take-off/landing and rapid flight are switched through the engagement and disconnection of the dry friction clutch. The smooth and rapid connection of the friction clutch
Chu Zhu   +3 more
doaj   +1 more source

Energy and Exergy Analysis on a Waste Heat Recovery Module for Helicopters

open access: yesIEEE Access, 2021
The exhaust of turboshaft engines contains a big amount of waste heat but does not provide propulsion power to the helicopter. Reusing the heat can increase fuel efficiency and reduce carbon emissions of the engine.
Yuxue Ge, Yuhao Wei, Qian Zhao, Yang Pei
doaj   +1 more source

An Advanced Helicopter Engine Control System [PDF]

open access: yesAircraft Engineering and Aerospace Technology, 1982
The Amalgamation of Functions The requirements of the first engine controllers were primarily to satisfy the needs of the engine and, almost as an afterthought, to consider interface with the aircraft and the pilot. The latter resulted in the overwhelming plethora of “essential” ground test‐sets and cockpit instruments that we see today.
openaire   +1 more source

Comparative Study of Helicopter Engine Particle Separators [PDF]

open access: yesJournal of Aircraft, 2014
Particle separators are fitted to helicopter engine intakes to remove potentially harmful dust from the influent air. Their use is necessary in desert environments to eliminate the risk of rapid engine wear and subsequent power deterioration. However, their employment is concomitant with an inherent loss in inlet pressure and, in some cases, auxiliary ...
Filippone, Antonino, Bojdo, Nicholas
openaire   +1 more source

Impact of dust erosion on the reduction of axial compressor efficiency of a turboshaft engine and on the stability of its operation [PDF]

open access: yesMATEC Web of Conferences, 2022
This paper aimed to solve the impact of operational abrasive wear on the rotor blades of the axial compressor of the turboshaft engine on the decrease in its total compression efficiency ηCt and its transition into unstable work mode (surge).
Hocko Marián, Al-Rabeei Samer
doaj   +1 more source

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