Apparatus and method for measuring static deflection of runway surface under aircraft loading
AssigneeThe Boeing Company
InventorsRoger F. Johnson, Allen M. Mitzel
Life of this patent
Estimating the term…
Abstract
A target comprising a displacement sensitive photodiode perpendicularly disposed with respect to the measuring axis perpendicular to the runway surface is provided above a runway surface under aircraft load. A laser beam is directed towards the diode and signal processing circuits coupled between the photodiode and display means during aircraft loading, and subsequent to aircraft load removal provide signals to the display means representative of displacement of runway surface.
Claims4
In an aircraft runway surface deflection measuring system including a reference potential, a detector circuit and a display device, said detector circuit coupled to said display device, said detector circuit comprising:
- photodiode target means responsive to a reference beam of light for providing first and second output currents;
- sum and difference amplifier circuits responsive to said first and second output currents for providing sum and difference signals;
- analog divider circuit means responsive to said sum and difference signals for providing an output voltage;
- circuit means for calibrating said display device;
- said circuit means coupled between said analog divider circuit means and said display device;
- and,
- measuring speed control circuit means for providing fast or slow measuring speeds, said measuring speed control circuit means connected between said circuit means and said display device, and said reference potential.
Method of measuring runway surface deflection comprising the steps of:
- maneuvering an aircraft over a point P on a runway surface;
- positioning a receiver adjacent a point P representative of said runway surface point deflected by the load of said aircraft;
- directing a laser beam towards said receiver;
- adjusting said receiver output to provide a null reading;
- maneuvering said aircraft away from said point P on said runway surface;
- then,
- obtaining a readout of said receiver representative of the actual displacement of said point P caused by aircraft loading.
Dependencies are inferred from the claim text.