Commercial aircraft on-board inerting system

Fluent material handling – with receiver or receiver coacting mea – Diverse fluid containing pressure filling systems involving... – Gas treatment

Reexamination Certificate

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C141S066000, C141S094000, C141S082000, C244S13500B

Reexamination Certificate

active

07152635

ABSTRACT:
An inerting system (10) for an aircraft (12) includes one or more fuel tank circuits (15) associated with fuel tanks (16). An air source (17) supplies pressurized air. A heat exchanger (56) cools the pressurized air. An air separation module (46) is in fluid communication with the heat exchanger (56) and separates inerting gas from the pressurized air. A controller (40) controls flow of the inerting gas from the air separation module (46) to the fuel tanks (16).

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Author Unknown, “Fluid Thinking for Aerospace —Environmental Control Systems”, printed from Internet website: http://www.flowmaster.com/apps/aero—ecs.html, Mar. 10, 2003.
Author Unknown, “Cabin Cooling and Antifog Systems”, printed from Internet website: http://www.tpup.com/ase2/62.htm, Mar. 10, 2003.
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Aviation Rulemaking Advisory Committee, “Fuel Tank Inerting Harmonization Working Group —Final Report”, Jun. 2001, Submitted joint by: AEA, AECMA, AtA, ALPA, API, ATA, FAA, JAA, and NADA/F.
Aviation Rulemaking Advisory Commitee, “Fuel Tank Inerting Harmonization Working Group —Team Reports”, Jun. 2001, Appendixes A —D.

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