A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft

Concept of aerostatic lift from the long ignored buoyant aerial vehicles has now a day been applied for partial fulfilment of the lift requirement for hybrid buoyant aircraft. This diffused lift technology seems to have eradicated the separate requirement of the heating mechanism for the lifting gas...

Full description

Saved in:
Bibliographic Details
Main Authors: Haque, Anwar Ul, Asrar, Waqar, Sulaeman, Erwin, Mohamed Ali, Jaffar Syed, Omar, Ashraf Ali
Format: Conference or Workshop Item
Language:English
English
Published: IEOM Society 2016
Subjects:
Online Access:http://irep.iium.edu.my/58551/1/58551_A%20Prospective%20Solution_complete.pdf
http://irep.iium.edu.my/58551/2/58551_A%20Prospective%20Solution_scopus.pdf
http://irep.iium.edu.my/58551/
http://ieomsociety.org/ieom_2016/pdfs/561.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Universiti Islam Antarabangsa Malaysia
Language: English
English
id my.iium.irep.58551
record_format dspace
spelling my.iium.irep.585512017-09-27T05:41:56Z http://irep.iium.edu.my/58551/ A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft Haque, Anwar Ul Asrar, Waqar Sulaeman, Erwin Mohamed Ali, Jaffar Syed Omar, Ashraf Ali T Technology (General) TA Engineering (General). Civil engineering (General) Concept of aerostatic lift from the long ignored buoyant aerial vehicles has now a day been applied for partial fulfilment of the lift requirement for hybrid buoyant aircraft. This diffused lift technology seems to have eradicated the separate requirement of the heating mechanism for the lifting gas. In comparison with conventional aircraft, such aircraft have big surface area available on the voluminous fuselage which is made up of thin shells and transverse frames. Depending on the power requirement and the power available through the irradiance modeling, partial surface area of fuselage can be utilized to provide power to the miniaturized avionics, specially the electrically driven heating elements; a prospective solution to provide heat to the lifting gas on as and when required basis. Potential issues related to the heat generated by the solar cells, bulky batteries and fuel powered plasmatrons are also discussed. A methodology for system design for the said issue is proposed. Based on the irradiance model of Malaysia, solar energy available throughout the day has been calculated. A detailed analysis is required for accurate estimation of energy and power budget along with a fine balance between the heat available and the one required. © IEOM Society International. IEOM Society 2016-03 Conference or Workshop Item REM application/pdf en http://irep.iium.edu.my/58551/1/58551_A%20Prospective%20Solution_complete.pdf application/pdf en http://irep.iium.edu.my/58551/2/58551_A%20Prospective%20Solution_scopus.pdf Haque, Anwar Ul and Asrar, Waqar and Sulaeman, Erwin and Mohamed Ali, Jaffar Syed and Omar, Ashraf Ali (2016) A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft. In: 6th International Conference on Industrial Engineering and Operations Management in Kuala Lumpur, IEOM 2016, 8 -10 March 2016, JW Marriott Hotel K LKuala Lumpur. http://ieomsociety.org/ieom_2016/pdfs/561.pdf
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic T Technology (General)
TA Engineering (General). Civil engineering (General)
spellingShingle T Technology (General)
TA Engineering (General). Civil engineering (General)
Haque, Anwar Ul
Asrar, Waqar
Sulaeman, Erwin
Mohamed Ali, Jaffar Syed
Omar, Ashraf Ali
A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft
description Concept of aerostatic lift from the long ignored buoyant aerial vehicles has now a day been applied for partial fulfilment of the lift requirement for hybrid buoyant aircraft. This diffused lift technology seems to have eradicated the separate requirement of the heating mechanism for the lifting gas. In comparison with conventional aircraft, such aircraft have big surface area available on the voluminous fuselage which is made up of thin shells and transverse frames. Depending on the power requirement and the power available through the irradiance modeling, partial surface area of fuselage can be utilized to provide power to the miniaturized avionics, specially the electrically driven heating elements; a prospective solution to provide heat to the lifting gas on as and when required basis. Potential issues related to the heat generated by the solar cells, bulky batteries and fuel powered plasmatrons are also discussed. A methodology for system design for the said issue is proposed. Based on the irradiance model of Malaysia, solar energy available throughout the day has been calculated. A detailed analysis is required for accurate estimation of energy and power budget along with a fine balance between the heat available and the one required. © IEOM Society International.
format Conference or Workshop Item
author Haque, Anwar Ul
Asrar, Waqar
Sulaeman, Erwin
Mohamed Ali, Jaffar Syed
Omar, Ashraf Ali
author_facet Haque, Anwar Ul
Asrar, Waqar
Sulaeman, Erwin
Mohamed Ali, Jaffar Syed
Omar, Ashraf Ali
author_sort Haque, Anwar Ul
title A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft
title_short A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft
title_full A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft
title_fullStr A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft
title_full_unstemmed A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft
title_sort prospective solution for consistent aerostatic lift for a hybrid buoyant aircraft
publisher IEOM Society
publishDate 2016
url http://irep.iium.edu.my/58551/1/58551_A%20Prospective%20Solution_complete.pdf
http://irep.iium.edu.my/58551/2/58551_A%20Prospective%20Solution_scopus.pdf
http://irep.iium.edu.my/58551/
http://ieomsociety.org/ieom_2016/pdfs/561.pdf
_version_ 1643615381671116800