System and method for improved rotary-wing aircraft performance with interior/external loads
First Claim
1. A system to manage aircraft loads, comprising:
- a sensor system that receives weight information;
an aircraft load management system in communication with said sensor system;
a display in communication with said aircraft load management system, said display operable to display an aircraft C.G. in real time, said aircraft C.G. represented by an actual C.G. indicator ball symbology relative to a C.G. limit ring symbology;
said actual C.G. indicator ball symbology and said C.G. limit ring symbology overlaid on an aircraft plan view which comprises an aircraft internal cargo area schematic; and
a cargo symbol, said cargo symbol placed relative to said aircraft internal cargo area schematic by an input device in communication with said display, said aircraft load management system operable to adjust said aircraft C.G. in real time in response to a relative position of said cargo symbol and upon said aircraft internal cargo area schematic.
1 Assignment
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Accused Products
Abstract
An interactive aircraft load management system automates calculation and provides simulation capability to changes in an aircraft C.G. limit for display on a three-dimensional aircraft symbology. The aircraft load management system also communicates with a fly by wire (FBW) flight control system wherein the aircraft'"'"'s control system is programmed to automatically compensate for C.G. excursions and to alter control laws. The aircraft load management system also selectively reels-in and reels out sling lines as the aircraft pitches and rolls to maintain a load vector from a slung load along the aircraft centerline. Load vector travel is accomplished by coupling a winch control system into the flight control system.
77 Citations
22 Claims
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1. A system to manage aircraft loads, comprising:
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a sensor system that receives weight information; an aircraft load management system in communication with said sensor system; a display in communication with said aircraft load management system, said display operable to display an aircraft C.G. in real time, said aircraft C.G. represented by an actual C.G. indicator ball symbology relative to a C.G. limit ring symbology;
said actual C.G. indicator ball symbology and said C.G. limit ring symbology overlaid on an aircraft plan view which comprises an aircraft internal cargo area schematic; anda cargo symbol, said cargo symbol placed relative to said aircraft internal cargo area schematic by an input device in communication with said display, said aircraft load management system operable to adjust said aircraft C.G. in real time in response to a relative position of said cargo symbol and upon said aircraft internal cargo area schematic. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14)
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15. A system to manage aircraft loads, comprising:
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an aircraft load management system that determines aircraft C.G. data of an aircraft with an; a flight control system in communication with said aircraft load management system, said flight control system programmed to adjust an aircraft trim state in real time through alteration of at least one flight control law of said flight control system to automatically compensate for aircraft C.G. excursions in response to said aircraft C.G. data, said aircraft C.G. data includes one or both of an internal cargo load within an aircraft internal cargo area and an external cargo load; and a sling system in communication with said aircraft load management system, said aircraft load management system programmed to adjust a slung load in real time to maintain a load vector of the slung load generally along an aircraft centerline. - View Dependent Claims (16, 17, 18, 19)
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20. A system to manage aircraft loads, comprising:
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a sensor system that receives weight information; an aircraft load management system in communication with said sensor system; a display in communication with said aircraft load management system, said display operable to display an aircraft C.G. in real time, said aircraft C.G. represented by an actual C.G. indicator ball symbology relative to a C.G. limit ring symbology, said actual C.G. indicator ball symbology and said C.G. limit ring symbology overlaid on an aircraft plan view which comprises an aircraft internal cargo area schematic; and a multiple of PAX symbols which represent cabin seating within said aircraft internal cargo area schematic, said multiple of PAX symbols individually selectable to represent a predetermined passenger type, said aircraft load management system operable to adjust said aircraft C.G. in real time in response to said selection. - View Dependent Claims (21, 22)
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Specification