Dual-axis loadmeter

Details Dual-axis loadmeter Dual-axis loadmeter

2006-05-30

2009-08-25

Pham, Toan N (Department: 2612)

Communications: electrical

Aircraft alarm or indicating systems

Flight alarm

C340S967000, C340S968000, C340S980000

Reexamination Certificate

active

07579966

ABSTRACT:
The present invention is directed to a computerized system that includes a graphical user interface (GUI) having a display and a data input device. The computerized system performs a method including the step of providing a plurality of aircraft parameters. At least one vertical g-force value is calculated in real time based on the plurality of aircraft parameters. A lateral g-force value is calculated in real time based on the plurality of aircraft parameters. The at least one vertical g-force value is displayed relative to at least one predetermined vertical reference value. The lateral g-force value is displayed relative to at least one predetermined lateral reference value.

REFERENCES:
patent: 5912627 (1999-06-01), Alexander
patent: 6989769 (2006-01-01), Gray
Travis Hunnings; Patent Cooperation Treaty PCT International Search Report for PCT/US07/69747; Form PCT/ISA/210; Aug. 29, 2008; ISA/US; 2 pages.
Travis Hunnings; Patent Cooperation Treaty PCT Written Opinion of the ISA for PCT/US07/69747; Form PCT/ISA/237; Aug. 29, 2008; ISA/US; 4 pages.

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