Apparatus for detecting turbulence

Patent metadata

Field	Value
Publication number	US-12592155-B2
Application number	US-202318310026-A
Country	US
Kind code	B2
Filing date	May 1, 2023
Priority date	May 2, 2022
Publication date	Mar 31, 2026
Grant date	Mar 31, 2026

Abstract

An apparatus for detecting and evaluating turbulence for an aircraft. The apparatus contains a measuring device for acquiring a value, which indicates a movement of the aircraft relative to the earth, and a second measuring device for acquiring a second value, which indicates a movement of the aircraft relative to the air. The apparatus contains a computing system which receives the two values and determines a difference between the first value and the second value and, on the basis of the difference, a turbulence intensity. The computing system compares the second value with a predefined value range and classifies turbulence as classified turbulence if the second value departs from the predefined value range. The computing system determines the frequency of occurrence of such classified turbulences and detects a turbulent flight state on the basis of the determined turbulence intensity and the frequency of occurrence of the classified turbulences.

First claim

The invention claimed is:

1 . An unmanned aircraft, comprising an apparatus for detecting turbulence, the apparatus comprising:
a first sensor configured for acquiring and outputting a first measured value, which is indicative of a movement of the aircraft relative to the earth; a second sensor configured for acquiring and outputting a second measured value, which is indicative of a movement of the aircraft relative to the air; a computing system which is in communicative connection with the first sensor and with the second sensor and which is configured to receive the first measured value and the second measured value; wherein the computing system is further configured to:
determine a difference between the first measured value and the second measured value;
determine a wind strength based on the difference between the movement of the aircraft relative to the earth and the movement of the aircraft relative to the air;
determine a turbulence intensity based on the difference between the first measured value and the second measured value and additionally based on a variation of the wind strength over time in terms of amplitude and direction;
compare the second measured value with a predefined value range for the second measured value;
detect an angle of incidence defining an angle between the direction of an oncoming fluid and an aerofoil of the aircraft, and detect an angle of yaw defining a drift angle between a longitudinal axis of the aircraft and the direction of the oncoming flow, and determine a variation of the oncoming flow at the aerofoil of the aircraft based on the angle of yaw and the angle of incidence; and
classify instances of turbulence when the second measured value lies outside the predefined value range and additionally based on the variation of the oncoming flow at the aerofoil of the aircraft and to determine a frequency of occurrence of such classified turbulences; and
detect a turbulent flight state on a basis of the determined turbulence intensity and the frequency of occurrence of the classified turbulences and to transmit information indicative of the turbulent flight state to a remote operator terminal for controlling operation of the aircraft;
wherein the apparatus is coupled with a drive unit of the aircraft; wherein the computing system is configured to generate and output a control command for the drive unit when a turbulent flight state has been detected, and to change a speed of the aircraft by means of the control command to thereby adapt an angle of incidence of the aircraft.

2 . The unmanned aircraft as claimed in claim 1 , wherein the computing system is further configured to determine a change over time of the difference between the first measured value and the second measured value so as to determine the turbulence intensity on the basis of the change over time.

3 . The unmanned aircraft as claimed in claim 1 , wherein the computing system is further configured to determine the frequency of occurrence of the classified turbulences for different units of time.

4 . The unmanned aircraft as claimed in claim 1 , wherein the computing system is configured to detect of a turbulent flight state throughout an entire operating time of the aircraft.

5 . The unmanned aircraft as claimed in claim 1 , wherein the computing system has a plurality of computers, and
wherein each computer is configured to perform one or more functions of the computing system.

6 . The unmanned aircraft as claimed in claim 5 , wherein at least two computers from the plurality of computers are spatially and structurally separate from one another.

7 . The unmanned aircraft as claimed in claim 6 , wherein a first computer is connected to the first sensor and is configured to determine the turbulence intensity, and
wherein a second computer is connected to the second sensor and is configured to determine the frequency of occurrence of the classified turbulences.

8 . The unmanned aircraft as claimed in claim 1 , wherein the aircraft is configured to be connected by way of a wireless data transmission channel to an operating station so as to be remotely piloted by an operator.

Assignees

• Airbus Defence & Space Gmbh

Inventors

• Hanel Martin
• Rath Tobias

Classifications

• G08G5/76

  for monitoring atmospheric conditions · CPC title

• G08G5/57

  for unmanned aircraft · CPC title

• G05D1/0022

  characterised by the communication link (data switching networks in general H04L12/00) · CPC title

• B64U2201/20

  Remote controls · CPC title

• B64D2045/009

  Fire detection or protection; Erosion protection, e.g. from airborne particles · CPC title