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...

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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:	T Technology (General) TA Engineering (General). Civil engineering (General)
Online Access:	http://irep.iium.edu.my/58551/ http://irep.iium.edu.my/58551/ 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

id	iium-58551
recordtype	eprints
spelling	iium-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 PeerReviewed 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
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
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/ http://irep.iium.edu.my/58551/ 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
first_indexed	2023-09-18T21:22:48Z
last_indexed	2023-09-18T21:22:48Z
_version_	1777411994560757760

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

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