TY - GEN
T1 - Design of a customized fuselage full airworthiness flexible fuel tank
AU - Ribinik, Eugene
AU - Trangle, Etan
AU - Goldin, Nir
AU - Alian, Hasib
AU - Manor, Shirry
AU - Strauss, Itai
AU - Rabaev, Moshe
AU - Wolfson, Leon
AU - Haris, Eliau
AU - Ankori, Tzahi
AU - Konforty, Shlomi
AU - Khapun, Shimon
AU - Atir, Micha
PY - 2012/10/8
Y1 - 2012/10/8
N2 - 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.
AB - 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.
UR - https://www.scopus.com/pages/publications/84867010032
M3 - Conference contribution
AN - SCOPUS:84867010032
SN - 9781618399144
T3 - 52nd Israel Annual Conference on Aerospace Sciences 2012
SP - 420
EP - 442
BT - 52nd Israel Annual Conference on Aerospace Sciences 2012
T2 - 52nd Israel Annual Conference on Aerospace Sciences 2012
Y2 - 29 February 2012 through 1 March 2012
ER -