Aviation Safety Technologies, LLC

États‑Unis d’Amérique

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Classe IPC
B64C 25/42 - Aménagement ou adaptation des freins 16
B60T 8/17 - Utilisation de moyens de régulation électriques ou électroniques pour la commande du freinage 4
B60T 8/171 - Détection des paramètres utilisés pour la régulationMesure des valeurs utilisées pour la régulation 4
B64C 19/00 - Dispositifs de commande des aéronefs non prévus ailleurs 2
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs 2
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1.

Method and device for communicating true runway braking performance using data from the flight data management systems of landed aircraft

      
Numéro d'application 14121622
Numéro de brevet 09260183
Statut Délivré - en vigueur
Date de dépôt 2014-09-26
Date de la première publication 2015-02-05
Date d'octroi 2016-02-16
Propriétaire AVIATION SAFETY TECHNOLOGIES, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

A computer network for calculating a value for the true braking coefficient of friction for an aircraft runway or taxiway using data from one or more aircraft's flight data recorders or flight data management systems, and reporting the calculated value information to individuals and agencies including air traffic control, airport operations and maintenance, and aircraft pilots and ground crews is described and claimed herein. The data may be obtained in real-time by either an onboard or an off-aircraft high-power computing system, calculating the aircraft's true braking coefficient of friction, and reporting the calculated information to the individuals and agencies.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins
  • B60T 8/171 - Détection des paramètres utilisés pour la régulationMesure des valeurs utilisées pour la régulation
  • B60T 8/17 - Utilisation de moyens de régulation électriques ou électroniques pour la commande du freinage
  • B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs

2.

Computer network for calculating aircraft cornering friction based on data received from an aircraft's on board flight data management system

      
Numéro d'application 14121183
Numéro de brevet 09073633
Statut Délivré - en vigueur
Date de dépôt 2014-08-08
Date de la première publication 2014-12-04
Date d'octroi 2015-07-07
Propriétaire AVIATION SAFETY TECHNOLOGIES, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

This invention relates to a computer network for calculating the true aircraft cornering friction coefficient of an aircraft runway or taxiway using the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR). The invention may optionally distribute to personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, the most accurate and most recent information concerning the true aircraft cornering friction coefficient to aid in making better and more accurate safety and economical decisions.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins
  • B60T 8/17 - Utilisation de moyens de régulation électriques ou électroniques pour la commande du freinage
  • B64C 19/00 - Dispositifs de commande des aéronefs non prévus ailleurs
  • G06F 19/00 - Équipement ou méthodes de traitement de données ou de calcul numérique, spécialement adaptés à des applications spécifiques (spécialement adaptés à des fonctions spécifiques G06F 17/00;systèmes ou méthodes de traitement de données spécialement adaptés à des fins administratives, commerciales, financières, de gestion, de surveillance ou de prévision G06Q;informatique médicale G16H)
  • B64D 45/04 - Aides à l'atterrissageDispositifs de sécurité pour éviter la prise de sol brutale
  • B60T 8/171 - Détection des paramètres utilisés pour la régulationMesure des valeurs utilisées pour la régulation

3.

Computer network for calculating and distributing the true aircraft braking friction coefficient for an aircraft runway or taxiway using data received from an aircraft's on board flight data management system

      
Numéro d'application 13999758
Numéro de brevet 08954254
Statut Délivré - en vigueur
Date de dépôt 2014-03-19
Date de la première publication 2014-07-24
Date d'octroi 2015-02-10
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

This invention relates to a computer network for calculating and distributing the true braking coefficient of aircraft on runways and taxiways using a computer which obtains data from an aircraft, including in some preferable embodiments dynamic aircraft properties recorded on the aircraft's flight data management system. Environmental and aircraft parameters may also be used to calculate the braking friction coefficient. A computer and network are used to obtain data and to calculate the friction coefficient, and may be used to distribute the result. The network may utilize, at least in part, wireless local area networks to facilitate data transfer and distribution of the result. The computer for calculating the braking coefficient may be located on the aircraft.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins
  • B60T 8/17 - Utilisation de moyens de régulation électriques ou électroniques pour la commande du freinage
  • B64C 19/00 - Dispositifs de commande des aéronefs non prévus ailleurs
  • G06F 19/00 - Équipement ou méthodes de traitement de données ou de calcul numérique, spécialement adaptés à des applications spécifiques (spécialement adaptés à des fonctions spécifiques G06F 17/00;systèmes ou méthodes de traitement de données spécialement adaptés à des fins administratives, commerciales, financières, de gestion, de surveillance ou de prévision G06Q;informatique médicale G16H)
  • B64D 45/04 - Aides à l'atterrissageDispositifs de sécurité pour éviter la prise de sol brutale
  • B60T 8/171 - Détection des paramètres utilisés pour la régulationMesure des valeurs utilisées pour la régulation

4.

Device for calculating and communicating the true aircraft braking coefficient of a runway or taxiway using data from the flight data management systems of landed aircraft

      
Numéro d'application 13998833
Numéro de brevet 08855886
Statut Délivré - en vigueur
Date de dépôt 2013-12-12
Date de la première publication 2014-04-17
Date d'octroi 2014-10-07
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

A computer network for calculating a value for the true braking coefficient of friction for an aircraft runway or taxiway using data from one or more aircraft's flight data recorders or flight data management systems, and reporting the calculated value information to individuals and agencies including air traffic control, airport operations and maintenance, and aircraft pilots and ground crews is described and claimed herein. The data may be obtained in real-time by either an onboard or an off-aircraft high-power computing system, calculating the aircraft's true braking coefficient of friction, and reporting the calculated information to the individuals and agencies.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins
  • B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
  • B60T 8/171 - Détection des paramètres utilisés pour la régulationMesure des valeurs utilisées pour la régulation
  • B60T 8/17 - Utilisation de moyens de régulation électriques ou électroniques pour la commande du freinage

5.

Computer network for calculating aircraft cornering friction based on data received from an aircraft's on board flight data management system

      
Numéro d'application 13987734
Numéro de brevet 08838358
Statut Délivré - en vigueur
Date de dépôt 2013-08-26
Date de la première publication 2013-12-26
Date d'octroi 2014-09-16
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

This invention relates to a computer network for calculating the true aircraft cornering friction coefficient of an aircraft runway or taxiway using the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR). The invention may optionally distribute to personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, the most accurate and most recent information concerning the true aircraft cornering friction coefficient to aid in making better and more accurate safety and economical decisions.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

6.

Computer network for calculating and distributing the true aircraft braking friction coefficient for an aircraft runway or taxiway using data received from an aircraft's on board flight data management system

      
Numéro d'application 13815370
Numéro de brevet 08682561
Statut Délivré - en vigueur
Date de dépôt 2013-02-25
Date de la première publication 2013-08-29
Date d'octroi 2014-03-25
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

This invention relates to a computer network for calculating and distributing the true braking coefficient of aircraft on runways and taxiways using, in part, the aircraft itself, by utilizing dynamic aircraft properties recorded on and obtained from the aircraft's flight data management system. Environmental and aircraft parameters may also be used to calculate the braking friction coefficient. A computer and network are used to obtain data and to calculate the friction coefficient, and may be used to distribute the result. The network may utilize, at least in part, wireless local area networks to facilitate data transfer and distribution of the result. The computer for calculating the braking coefficient may be located on the aircraft.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

7.

Method and device for communicating true runway braking performance using data from the flight data management systems of landed aircraft

      
Numéro d'application 13694746
Numéro de brevet 08630782
Statut Délivré - en vigueur
Date de dépôt 2012-12-28
Date de la première publication 2013-07-25
Date d'octroi 2014-01-14
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

A method and apparatus for calculating a standardized value for the actual runway braking coefficient of friction of one or more arriving aircraft using data from each aircraft's flight data recorder or flight data management system, standardizing the calculated information to provide redundancy and to make it usable by subsequently arriving aircraft, and reporting the calculated standardized value information to individuals and agencies including air traffic control, airport operations and maintenance, and aircraft pilots and ground crews; and A method and apparatus for calculating the actual runway braking coefficient of friction of an aircraft using data from the aircraft's flight data recorder or flight data management system, transmitting the data in real-time to an off-aircraft high-power computing system, calculating off-aircraft the landing aircraft's actual runway braking coefficient of friction, and reporting the calculated information to individuals and agencies including air traffic control, airport operations and maintenance, and aircraft pilots and ground crews.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

8.

Computer network for calculating aircraft cornering friction based on data received from an aircraft's on board flight data management system

      
Numéro d'application 13694866
Numéro de brevet 08538655
Statut Délivré - en vigueur
Date de dépôt 2013-01-11
Date de la première publication 2013-05-30
Date d'octroi 2013-09-17
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

This invention relates to a computer network for calculating the true aircraft cornering friction coefficient of an aircraft runway or taxiway using the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR). The invention may optionally distribute to personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, the most accurate and most recent information concerning the true aircraft cornering friction coefficient to aid in making better and more accurate safety and economical decisions.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

9.

Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system

      
Numéro d'application 13507470
Numéro de brevet 08412434
Statut Délivré - en vigueur
Date de dépôt 2012-06-28
Date de la première publication 2012-11-01
Date d'octroi 2013-04-02
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Radó, Zolán Iván

Abrégé

This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

10.

Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system

      
Numéro d'application 13374757
Numéro de brevet 08244444
Statut Délivré - en vigueur
Date de dépôt 2012-01-11
Date de la première publication 2012-05-17
Date d'octroi 2012-08-14
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Radó, Zoltán Iván

Abrégé

This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

11.

Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system

      
Numéro d'application 13134801
Numéro de brevet 08355850
Statut Délivré - en vigueur
Date de dépôt 2011-06-17
Date de la première publication 2011-10-20
Date d'octroi 2013-01-15
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Radó, Zoltán Iván

Abrégé

This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

12.

Method and device for communicating true runway braking performance using data from the flight data management systems of landed aircraft

      
Numéro d'application 12661657
Numéro de brevet 08346455
Statut Délivré - en vigueur
Date de dépôt 2010-03-20
Date de la première publication 2011-06-16
Date d'octroi 2013-01-01
Propriétaire AVIATION SAFETY TECHNOLOGIES, LLC (USA)
Inventeur(s) Rado, Zoltan Ivan

Abrégé

A method and apparatus for calculating a standardized value for the actual runway braking coefficient of friction of one or more arriving aircraft using data from each aircraft's flight data recorder or flight data management system, standardizing the calculated information to provide redundancy and to make it usable by subsequently arriving aircraft, and reporting the calculated standardized value information to individuals and agencies including air traffic control, airport operations and maintenance, and aircraft pilots and ground crews; and A method and apparatus for calculating the actual runway braking coefficient of friction of an aircraft using data from the aircraft's flight data recorder or flight data management system, transmitting the data in real-time to an off-aircraft high-power computing system, calculating off-aircraft the landing aircraft's actual runway braking coefficient of friction, and reporting the calculated information to individuals and agencies including air traffic control, airport operations and maintenance, and aircraft pilots and ground crews.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

13.

Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system

      
Numéro d'application 12927393
Numéro de brevet 07957878
Statut Délivré - en vigueur
Date de dépôt 2010-11-12
Date de la première publication 2011-03-31
Date d'octroi 2011-06-07
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Radó, Zoltán Iván

Abrégé

This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

14.

Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system

      
Numéro d'application 12802065
Numéro de brevet 08121771
Statut Délivré - en vigueur
Date de dépôt 2010-05-28
Date de la première publication 2010-11-25
Date d'octroi 2012-02-21
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Rado', Zolta'N Iva'N

Abrégé

This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

15.

Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system

      
Numéro d'application 12802101
Numéro de brevet 08050840
Statut Délivré - en vigueur
Date de dépôt 2010-05-28
Date de la première publication 2010-11-25
Date d'octroi 2011-11-01
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Radó, Zoltán Iván

Abrégé

This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins

16.

Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system

      
Numéro d'application 11352984
Numéro de brevet 07797095
Statut Délivré - en vigueur
Date de dépôt 2006-02-13
Date de la première publication 2006-11-02
Date d'octroi 2010-09-14
Propriétaire Aviation Safety Technologies, LLC (USA)
Inventeur(s) Radó, Zoltán Iván

Abrégé

This invention relates to method and apparatus of the calculation of aircraft braking friction and other relating landing parameters including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system for example the Quick Access Recorder (QAR) to provide every involved personnel in the ground operations of an airport and airline operations including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making.

Classes IPC  ?

  • B64C 25/42 - Aménagement ou adaptation des freins