Design of a customized fuselage full airworthiness flexible fuel tank

  • Eugene Ribinik
  • , Etan Trangle
  • , Nir Goldin
  • , Hasib Alian
  • , Shirry Manor
  • , Itai Strauss
  • , Moshe Rabaev
  • , Leon Wolfson
  • , Eliau Haris
  • , Tzahi Ankori
  • , Shlomi Konforty
  • , Shimon Khapun
  • , Micha Atir

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Flexible fuel tanks as a means for allowing more consumable fuel are not a new concept in both the Israeli and foreign air forces: "Bladder" tanks have been in use for many years. Most flexible fuel tanks in existence are similar to one another, having the same advantages and disadvantages. A project completed by the Israeli Air Force involved the design and development of a customized flexible fuel tank. The tank is unique because it was designed in a shape specific to the end user's operational needs: The main requirements from the tank were that it be made collapsible, contain a maximum ratio of usable fuel weight to tank weight, allow for maximum usable in-flight storage volume and be airworthy for all air mobility aircraft types. The development of the tank involved selecting the appropriate materials and optimal shape and size, developing a support system to hold it, proving the tank in various extreme conditions and deciding on the tank's operation and maintenance procedures, all while satisfying the tank's operational requirements.

Original languageEnglish
Title of host publication52nd Israel Annual Conference on Aerospace Sciences 2012
Pages420-442
Number of pages23
StatePublished - 8 Oct 2012
Externally publishedYes
Event52nd Israel Annual Conference on Aerospace Sciences 2012 - Tel-Aviv and Haifa, Israel
Duration: 29 Feb 20121 Mar 2012

Publication series

Name52nd Israel Annual Conference on Aerospace Sciences 2012
Volume1

Conference

Conference52nd Israel Annual Conference on Aerospace Sciences 2012
Country/TerritoryIsrael
CityTel-Aviv and Haifa
Period29/02/121/03/12

ASJC Scopus subject areas

  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Design of a customized fuselage full airworthiness flexible fuel tank'. Together they form a unique fingerprint.

Cite this