Method and a device for determining the wind speed to be taken into account in order to optimize the takeoff weight of an aircraft

Patent metadata

Field	Value
Publication number	US-9728092-B2
Application number	US-201614995285-A
Country	US
Kind code	B2
Filing date	Jan 14, 2016
Priority date	Jan 15, 2015
Publication date	Aug 8, 2017
Grant date	Aug 8, 2017

Abstract

A method of determining the speed of the wind to be taken into account for determining a maximum authorized takeoff weight of an aircraft. A measured speed TAS mes of the local wind is calculated from at least one current speed TAS inst of the local wind and an observed speed TAS obs of the local wind on the basis of weather observations and on the basis of a heading value. The measured speed TAS mes is compared with the observed speed TAS obs in order to determine a calculated speed TAS perfo of the local wind while also making use of at least one instability criterion of the local wind as supplied by the weather observations and weather forecasts. The calculated speed TAS perfo is then for taking into account in order to optimize the maximize authorized takeoff weight of the aircraft.

First claim

What is claimed is:

1. A method of determining the speed of the wind that is to be taken into account when determining the maximum authorized takeoff weight of an aircraft, the aircraft waiting to take off, and including at least:
anemometer means;
receiver means for receiving observation information and weather forecast information;
consolidation means; and
display means;
the method comprising the following steps:
determining a heading value in a terrestrial reference frame;
measuring at least one current speed value TAS inst of the local wind in a predefined direction, the predefined direction being a direction corresponding to the heading value;
receiving weather observation information and weather forecast information for the area in which the aircraft is situated or for a nearby area;
calculating a measured speed TAS mes of the local wind in the predefined direction from at least one current speed value TAS inst of the speed of the local wind;
calculating an observed speed TAS obs of the local wind in the predefined direction from the weather observation information and the heading value;
comparing the measured value TAS mes and the observed speed TAS obs of the local wind;
determining a calculated speed TAS perfo of the local wind for taking into account when determining the authorized maximum takeoff weight of the aircraft in the predefined direction; and
displaying the calculated speed TAS perfo of the local wind on display means.

2. A method according to claim 1 , wherein the measured speed TAS mes of the local wind is equal to the current speed value TAS inst .

3. A method according to claim 1 , wherein at least two current speed values TAS inst are measured over a predetermined duration, and a mean measured speed TAS moy of the local wind in the predefined direction is measured from the current speed values TAS inst measured over the predetermined duration, the mean measured speed TAS moy being equal to the mean of the current speed values TAS inst , the measured speed TAS mes of the local wind being equal to the mean measured speed TAS moy .

4. A method according to claim 3 , wherein the predetermined duration is equal to 2 min.

5. A method according to claim 1 , wherein the heading value is determined by a pilot of the aircraft, the instantaneous heading of the aircraft also being determined when the heading value is different from the instantaneous heading of the aircraft in order to calculate a bearing of the predefined direction relative to a longitudinally extending direction of the aircraft extending between the front and the rear of the aircraft.

6. A method according to claim 1 , wherein the aircraft has means for determining the heading of the aircraft, the heading value is equal to the instantaneous heading of the aircraft as determined by the means for determining the heading of the aircraft, the predefined direction then being a longitudinally extending direction of the aircraft extending from the front to the rear of the aircraft.

7. A method according to claim 1 , wherein the weather observation information is decoded and a mean observed speed of the local wind and an observed direction of the local wind together with a first instability criterion for the local wind are extracted from the observation information, and then the observed speed TAS obs of the local wind in the predefined direction is calculated from the mean observed speed, from the mean observed direction of the local wind, and from the heading value.

8. A method according to claim 7 , wherein the weather forecast information is decoded and a second criterion for instability of the local wind is extracted from the forecast information.

9. A method according to claim 8 , wherein when the measured speed TAS mes and the observed speed TAS obs are positive, a speed of the local wind in the predefined direction is considered to be positive when the local wind constitutes at least in part a head wind relative to the aircraft; and
if the first instability criterion and/or the second instability criterion for the local wind indicate(s) instability of the local wind, the calculated speed TAS perfo of the local wind is equal to the observed speed divided by two, TAS obs /2;
if the measured speed TAS mes is greater than or equal to the observed speed TAS obs and if the first instability criterion and the second instability criterion for the local wind do not indicate any instability of the local wind, the calculated speed TAS perfo is equal to the observed speed TAS obs ;
if the measured speed TAS mes lies strictly between the observed speed TAS obs and the observed speed divided by two, TAS obs /2, and if the first instability criterion and the second instability criterion for the local wind do not indicate any instability of the local wind, the calculated speed TAS perfo is equal to the measured speed TAS mes ;
if the measured speed TAS mes is less than or equal to the observed speed divided by two, TAS obs /2, and if the first instability criterion and the second instability criterion for the local wind do not indicate any instability of the local wind, the calculated speed TAS perfo is equal to the observed speed divided by two, TAS obs /2;
if no measured speed TAS mes is provided and if the first instability criterion and the second instability criterion for the local wind do not indicate any instability of the local wind, the calculated speed TAS perfo is equal to the observed speed divided by two, TAS obs /2; and
if no observed speed TAS obs is available and if the first instability criterion and the second instability criterion for the local wind do not indicate any instability of the local wind, the calculated speed TAS perfo is equal to the measured speed TAS mes divided by two.

10. A method according to claim 1 , wherein when the measured speed TAS mes and/or the observed speed TAS obs are negative, a speed of the local wind in the predefined direction being considered as being negative when the local wind constitutes at least in part a tail wind relative to the aircraft, the calculated speed TAS perfo is equal to the minimum value from among the measured speed TAS mes and the observed speed TAS obs .

11. A method according to claim 1 , wherein the aircraft includes locating means, and location information and time information supplied by the locating means is used to determine the observation information and the forecast information that is to be used.

12. A method according to claim 1 , wherein a pilot of the aircraft supplies location information for the aircraft and time information in order to determine the observation information and the forecast information for use.

13. A method according to claim 1 , wherein the observation information and the forecast information come from reports containing digital data corresponding to the position of the aircraft and to the current time.

14. A method according to claim 1 , wherein the observation information comes from a METAR report and the forecast information comes from a TAF report.

15. A method according to claim 1 , wherein the aircraft is a rotary wing aircraft having at least a main rotor and possibly a tail rotor, and each current speed value TAS inst is corrected in order to take account of the disturbances caused by the main rotor and/or by the tail rotor on each current speed value TAS inst .

16. A method according to claim 1 , wherein each current speed value TAS inst is measured in the immediate surroundings of the aircraft.

17. A method according to claim 1 , wherein each current

Assignees

• Airbus Helicopters

Inventors

• Poudrai Etienne
• Certain Nicolas
• Spinosi Bernard

Classifications

• G08G5/0065 Primary

  Physics · mapped topic

• G01P21/025

  for measuring speed of fluids; for measuring speed of bodies relative to fluids (for measuring volume flow G01F25/10) · CPC title

• G01P5/26 Primary

  by measuring the direct influence of the streaming fluid on the properties of a detecting optical wave · CPC title

• G08G5/0091

  Physics · mapped topic

• B64C27/04

  Helicopters · CPC title