Systems and methods for issuing a hard landing warning and providing maintenance advisories for hard landing incidents
AssigneeHoneywell International Inc.
InventorsNagarajan Chandran, Girish M. Lad
Life of this patent
Estimating the term…
Abstract
An aircraft is provided. The aircraft may include, but is not limited to, an accelerometer configured to measure a deceleration experienced by the aircraft and a processor coupled to the accelerometer. The processor may be configured to determine if the aircraft experienced a hard landing if the deceleration experienced by the aircraft was greater than a predetermined threshold, and generate a maintenance advisory if the aircraft experienced a hard landing.
Claims20
An aircraft, comprising:
- an accelerometer configured to measure a deceleration experienced by the aircraft;
- and
- a processor coupled to the accelerometer, the processor configured to:
- determine if the aircraft experienced a hard landing if the deceleration experienced by the aircraft was greater than a predetermined threshold;
- and
- generate a maintenance advisory if the aircraft experienced a hard landing.
A hard landing warning system for an aircraft, comprising:
- at least one flight instrument collecting flight instrument data;
- a hard landing indicator;
- and
- a processor coupled to the at least one flight instrument and the hard landing indicator, the processor configured to:
- determine if the aircraft is in the landing phase based upon the flight instrument data;
- determine, when the aircraft is in a landing phase, a descent condition of the aircraft based upon the flight instrument data;
- and
- issue a hard landing warning via the hard landing indicator if the descent condition indicates a potential hard landing before the aircraft has landed.
A method executed by a processor, the method comprising:
- determining if an aircraft is in a landing phase;
- determining, when the aircraft is in the landing phase, a descent condition for the aircraft;
- and
- issuing a hard landing warning when the descent condition indicates a possibility of a hard landing before the aircraft has landed.
Dependencies are inferred from the claim text.