DEVICES AND METHODS FOR CANTILEVERED-SUPPORT OF AIRCRAFT CARGO PAYLOADS IN FORWARD AND AFT ENDS OF A CARGO BAY

A fixture for supporting a payload including first and second carriages, first and second cantilevered supports, and a support beam is disclosed. The first and second carriages each have a longitudinal axis that is parallel with the other. Each cantilevered support is coupled to a respective carriag...

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Bibliographische Detailangaben
1. Verfasser:	KARNI, Etan D
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS,e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES,DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS CONVEYING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING THIN OR FILAMENTARY MATERIAL HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PACKAGES PACKAGING ELEMENTS PACKING PARACHUTES PERFORMING OPERATIONS PRODUCING MECHANICAL POWER STORING TRANSPORTING VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TOCARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS VEHICLES IN GENERAL WEAPONS WIND MOTORS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Beschreibung
Zusammenfassung:	A fixture for supporting a payload including first and second carriages, first and second cantilevered supports, and a support beam is disclosed. The first and second carriages each have a longitudinal axis that is parallel with the other. Each cantilevered support is coupled to a respective carriage and extends at an oblique angle with respect to the longitudinal axis of the carriage. The first and second cantilevered supports extend substantially parallel to each other. The support beam extends between the cantilevered supports such that a first end of the support beam is coupled to the first support structure and a second end of the support beam is coupled to the second support structure. The cantilevered supports enable the payload to extend into otherwise unusable cargo bay storage space within the nose or tailcones of an aircraft.