Method and device for compensation of mechanical stresses in an aircraft structure
First Claim
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1. A method for compensation of mechanical stresses in an aircraft structure, comprising the steps of:
- producing signals that represent mechanical stresses occurring in the aircraft structure, andoperating actuators, which absorb at least some of the mechanical stresses and are arranged in the aircraft structure, such that the mechanical stresses are compensated,wherein the signals that represent the mechanical stresses are derived from at least one of central processor, input-output memory, sensors, flight state data, maneuver data, and by means of an electronic computation device from the flight state data and maneuver data and from data that represents load states which occur in the aircraft structure as a function of at least one of the flight stat and maneuvers, andwherein said flight state data and maneuver data are derived from a primary flight computer.
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Abstract
A method and a device are described for compensation of mechanical stresses in an aircraft structure. The method comprises the steps of producing signals that represent mechanical stresses occurring in the aircraft structure, and operating actuators, which absorb at least some of the mechanical stresses and are arranged in the aircraft structure, such that the mechanical stresses are compensated.
18 Citations
11 Claims
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1. A method for compensation of mechanical stresses in an aircraft structure, comprising the steps of:
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producing signals that represent mechanical stresses occurring in the aircraft structure, and operating actuators, which absorb at least some of the mechanical stresses and are arranged in the aircraft structure, such that the mechanical stresses are compensated, wherein the signals that represent the mechanical stresses are derived from at least one of central processor, input-output memory, sensors, flight state data, maneuver data, and by means of an electronic computation device from the flight state data and maneuver data and from data that represents load states which occur in the aircraft structure as a function of at least one of the flight stat and maneuvers, and wherein said flight state data and maneuver data are derived from a primary flight computer. - View Dependent Claims (2, 3, 4, 5)
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6. A device for compensating of mechanical stresses in on the aircraft structure, comprising:
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actuators, which are arranged in the aircraft structure and absorb at least some of the mechanical stresses, in order to compensate the mechanical stresses, wherein the device is adapted to produce signals representing mechanical stresses which occur in the aircraft structure producing signals that represent mechanical stresses occurring in the aircraft structure, and wherein the signals that represent the mechanical stresses are derived from at least one of central processor, input-output memory, sensors, flight state data, maneuver data, and by means of an electronic computation device for derivation of the signals which represent the mechanical stresses from the flight state data and maneuver data, and from data which respresents load states which occur in the aircraft structure as a function of at least one of the flight state and maneuvers, and wherein the flight state data and maneuver data are derived from a primary flight computer. - View Dependent Claims (7, 8, 9, 10, 11)
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Specification