Patent · US Active

System and method for determining a center of gravity of an aircraft

US7890249B2 · kind B2 · utility

3Cited by
5References
21Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 3, 2008
Grant dateFeb 15, 2011
Priority date
Expiry dateAug 3, 2029

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01M1/125
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

According to one embodiment of the disclosure, a method of determining a center of gravity of an aircraft includes receiving a strut length for each of the gears of an aircraft, determining an arm length for each of the gears, and determining a center of gravity of the aircraft based on a relationship between the center of gravity and respective arm lengths for each of the gears. The arm length of each of the gears is determined according to the strut length of a gear strut of a respective gear and a relationship between the strut length of the gear strut to another gear of another aircraft and the arm length of the respective gear.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.