Aircraft weight and center of gravity cockpit readout system

• US 4,463,428 A
• Filed: 10/26/1981
• Issued: 07/31/1984
• Est. Priority Date: 10/26/1981
• Status: Expired due to Fees

• Current Assignee: The United States of America As Represented By The Secretary of Agriculture
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Gilliam, Raymond J.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US06/314,616
• Time in Patent Office: 1,009 Days
• Field of Search: 364/463, 364/466, 364/567, 340/27 R, 340/666, 235/61 T, 73/65, 177/25
• US Class Current: 701/124
• CPC Class Codes: G01G 19/07 for weighing aircraft
• CPC Class Codes: G01M 1/127 during the flight

Abstract

An aircraft system which provides the pilot with a continuous cockpit reat of the weight and center of gravity of an aircraft carrying an externally lifted load together with the impact on aircraft controllability of load shifts and fuel burnoff, by transmitting input signals from load cells installed in the lifting hook system, input signals from a fuel totalizer, and input data from a system keyboard to a system computer.

Claims

1. An in-flight aircraft weight and center of gravity cockpit readout device comprising:

a plurality of lifting hooks for attaching to and lifting a load external to said aircraft;

a plurality of load measuring means, adapted to sense the weight of said external load suspended from said lifting hooks, for continuously producing a first electrical signal proportional to said weight during the in-flight time of said aircraft;

fuel measuring means for continuously producing a second electrical signal proportional to the amount of fuel remaining in said aircraft'"'"'s fuel tanks during the in-flight time of said aircraft;

keyboard input means for providing a third electrical signal proportional to said aircraft'"'"'s weight and center of gravity prior to the takeoff of said aircraft lifting of said external load;

means for receiving and processing said first, second and third electrical signals from said plurality of load measuring means, said fuel measuring means and said keyboard input means respectively to produce a combined weight and center of gravity output signal;

indicator means for receiving and displaying said combined weight and center of gravity output signal from said microprocessor means and weight on wheels interlock switch, connected between said microprocessor means and a weight on wheels interlock switch, connected between said microprocessor means and said keyboard input means, for disabling said keyboard input means while said aircraft is in flight thus preventing data alterations from being entered therefrom.

2. An aircraft weight and center of gravity cockpit readout device according to claim 1 wherein said plurality of load measuring means are load cells.

3. An aircraft weight and center of gravity cockpit readout device according to claim 2 wherein said fuel measuring means is a fuel totalizer.

4. An aircraft weight and center of gravity cockpit readout device according to claim 3 wherein said indicator means further comprises:

a center of gravity location display for showing the combined center of gravity of said aircraft and said external load;

a hook load display; and

selecting means for selecting the hook load to be displayed.