Usage of vortex circles for pressurization of fuel tanks of launch vehicles powerplant engines
DOI:
https://doi.org/10.15587/1729-4061.2012.4154Keywords:
pressurization, limiting action, vortex circles, range, high elongation tanks.Abstract
One of the ways of improving the efficiency of pressurization systems of fuel tanks of launch vehicles powerplant engines is raising the temperature increase of working body while entering the tank. At the moment 1100 K temperature is reached, but even with usage of this temperature the problem of overheating of aluminum top floor occurred. Attempts to stretch a cloud of overheated gas gave no result due to limiting action of its design using tradition jet input of hot gas into tanks. The extension movement of hot gas injected as vortex circles considering carrier conditions (a range of pressures, tank geometry, time of pressurization work and other) was experimentally investigated. Inject speed ranged 4-10 m/s. Ratios of tank diameter to ring diameter in which limiting action of tank starts showing were found. Frequencies for injection of vortex circles into tank when channeling mode begins are determined. Also main factors that influence on vortex circles range in tank are identified. Main parameters of gas flow in tank after breaking of vortex circles are counted. The obtained results of vortex circles spreading in ranged conditions allow to see the prospects optimistically in using this method of injecting working body with high temperature in free space of powerplant engines fueled tanks. It is appropriate to continue exploring the determination of interaction mechanism of vortex circles and fuel surface, to continue exploring optimal design of vortex circles generator.References
- Митиков, Ю.А. Газобаллонные системы наддува и ракеты-носители нового поколения [Текст] / Ю.А. Митиков // Космическая техника. Ракетное вооружение. – 2012. – №1. – С. 179 – 185.
- Митиков, Ю.А. Пути повышения надежности и безопасности эксплуатации ракетных комплексов [Текст] / Ю.А. Митиков, В.А. Антонов, М.Л. Волошин, А.И. Логвиненко // Авиационно-космическая техника и технология. – 2012. – № 3 (90). – C. 30 – 36.
- Мітіков, Ю.О. Рекомендації по проектуванню газовводів баків великого подовження [Текст] / Ю.А. Митиков, М.В. Поляков // Збірник наукових праць ХУПС. – 2012. – Вип. №2 (31). – С. 118 – 121.
- Козлов А.А., Новиков В.Н., Соловьев Е.В. Системы питания и управления жидкостных ракетных двигательных установок. – М.: Машиностроение, 1988. – 352 с.
- Митиков, Ю.А. Определение коэффициентов стеснения неизотермических турбулентных струй [Текст] / Ю.А. Митиков, С.А. Куда // Проектирование сложных технических систем. Сб. тр. ИТМ АН УССР. – 1989. – С.153 – 155.
- Митиков, Ю.А. Оптимизация скорости ввода горячего гелия в бак с кислородом [Текст] / Ю.А. Митиков, С.А.Куда // Вісник НТУ «ХПІ». [Текст] 2012. – №34. – С. 9–16.
- Тарасов, В.Ф. Экспериментальные исследования переноса примеси турбулентным вихревым кольцом [Текст] / В.Ф. Тарасов, В.И. Якушев // ПМТФ. – 1974. – №1. – С. 130–136.
- Будник, В.С. Обощенный энергетический подход к организации темпломассообменных процессов в свободном газовом объеме топливных баков жидкостных ракет [Текст] / В.С. Будник, Ю.Ф. Даниев, Н.Ф. Свириденко // Техническая механика. – 1998. – №7. – С. 98 – 106.
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2014 Юрий Алексеевич Митиков
This work is licensed under a Creative Commons Attribution 4.0 International License.
The consolidation and conditions for the transfer of copyright (identification of authorship) is carried out in the License Agreement. In particular, the authors reserve the right to the authorship of their manuscript and transfer the first publication of this work to the journal under the terms of the Creative Commons CC BY license. At the same time, they have the right to conclude on their own additional agreements concerning the non-exclusive distribution of the work in the form in which it was published by this journal, but provided that the link to the first publication of the article in this journal is preserved.
A license agreement is a document in which the author warrants that he/she owns all copyright for the work (manuscript, article, etc.).
The authors, signing the License Agreement with TECHNOLOGY CENTER PC, have all rights to the further use of their work, provided that they link to our edition in which the work was published.
According to the terms of the License Agreement, the Publisher TECHNOLOGY CENTER PC does not take away your copyrights and receives permission from the authors to use and dissemination of the publication through the world's scientific resources (own electronic resources, scientometric databases, repositories, libraries, etc.).
In the absence of a signed License Agreement or in the absence of this agreement of identifiers allowing to identify the identity of the author, the editors have no right to work with the manuscript.
It is important to remember that there is another type of agreement between authors and publishers – when copyright is transferred from the authors to the publisher. In this case, the authors lose ownership of their work and may not use it in any way.