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AGARD Advisory Group. Fault tolerant hardware/ software architecture for flight critical function. / AGARD Lecture Series (1985)
Titre de série : AGARD Advisory Group Titre : Fault tolerant hardware/ software architecture for flight critical function. Type de document : texte imprimé Auteurs : AGARD Lecture Series, Auteur Editeur : NATO - OTAN Année de publication : 1985 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-LS-143 Importance : 150 p. Format : 21 x 30 cm. Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Computer systems programs, Computer systems hardware Flight control Errors Tolerances Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This lecture series is intended to provide basic concepts and therories in the design of fault-tolerant architectures for flight critical systems. It is intended to cover exêroence with flight tested fly_by_wire systems as well as issues in reduncary management of synchronous and asynchnonous approaches. It will specifically address the individual aspects of software fault tolerance, actuation fault tolerance, reliable data communication, and multi-computer operation using the ADA language. AGARD Advisory Group. Fault tolerant hardware/ software architecture for flight critical function. [texte imprimé] / AGARD Lecture Series, Auteur . - [S.l.] : NATO - OTAN, 1985 . - 150 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-LS-143) .
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Computer systems programs, Computer systems hardware Flight control Errors Tolerances Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This lecture series is intended to provide basic concepts and therories in the design of fault-tolerant architectures for flight critical systems. It is intended to cover exêroence with flight tested fly_by_wire systems as well as issues in reduncary management of synchronous and asynchnonous approaches. It will specifically address the individual aspects of software fault tolerance, actuation fault tolerance, reliable data communication, and multi-computer operation using the ADA language. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3199 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtAGARD Advisory Report. Aluminium Alloy Forgings / AGARD Advisory Group (1998) / 978-92-8361-074-8
Titre de série : AGARD Advisory Report Titre : Aluminium Alloy Forgings Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1998 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-353 Importance : 64 p. Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8361-074-8 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Airframes Airworthiness Aluminium alloys Components Loads Forgings Durability Damage Tolerances Aviation safety Crackings Service life Metal plates Properties Performance evaluation Fatigue Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : Historically, many aluminium aircraft components have been made from forgings. However, to reduce airframe manufacting cost aircraft manufacters are converting to parts machined from thick plate. The result of recent research indicates that forgings often offer significant adventages over components machined from plate. The purpose of this report is to present this information. AGARD Advisory Report. Aluminium Alloy Forgings [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1998 . - 64 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-353) .
ISBN : 978-92-8361-074-8
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Airframes Airworthiness Aluminium alloys Components Loads Forgings Durability Damage Tolerances Aviation safety Crackings Service life Metal plates Properties Performance evaluation Fatigue Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : Historically, many aluminium aircraft components have been made from forgings. However, to reduce airframe manufacting cost aircraft manufacters are converting to parts machined from thick plate. The result of recent research indicates that forgings often offer significant adventages over components machined from plate. The purpose of this report is to present this information. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 2898 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtAGARD Advisory Report. Echocardiography in NATO Aircrew - A Multy-national Study / AGARD Advisory Group (1997)
Titre de série : AGARD Advisory Report Titre : Echocardiography in NATO Aircrew - A Multy-national Study Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1997 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-351 Importance : 104 p. Format : 21 x 30 cm. Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Cardiography NATO forces Flight crews Pilots Acceleration stresses Tolerances Fighter aircraft Aerospace medicine Occupational diseases cardiovascular system surveys Quality control Acceleration tolerances Gravity Ultrasonic test Protocols Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report addresses the results of an AGARD epidemiological study of NATO aircrew, utilizing Echocardiography studies. This Echocardiography project was performed by AGARD Working Group 18, based upon an extensive protocol written by Woking group 13. The goal of the study was to determine whether repeatd high sustained +Gz acceleration produced permanent structural or functional changes in the heart, when compared to a control group of non-high performance pilots. The results conclusively confirm the absence of any abnormal Echocardiography parameters in the high sustained G pilots. AGARD Advisory Report. Echocardiography in NATO Aircrew - A Multy-national Study [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1997 . - 104 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-351) .
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Cardiography NATO forces Flight crews Pilots Acceleration stresses Tolerances Fighter aircraft Aerospace medicine Occupational diseases cardiovascular system surveys Quality control Acceleration tolerances Gravity Ultrasonic test Protocols Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report addresses the results of an AGARD epidemiological study of NATO aircrew, utilizing Echocardiography studies. This Echocardiography project was performed by AGARD Working Group 18, based upon an extensive protocol written by Woking group 13. The goal of the study was to determine whether repeatd high sustained +Gz acceleration produced permanent structural or functional changes in the heart, when compared to a control group of non-high performance pilots. The results conclusively confirm the absence of any abnormal Echocardiography parameters in the high sustained G pilots. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 2896 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtRTO Meeting proceedings, 17. Qualification of life extension schemes for engine components / RTO Applied Vehicule Technology (AVT) (1999) / 978-92-8371-012-7
Titre de série : RTO Meeting proceedings, 17 Titre : Qualification of life extension schemes for engine components : Papers presented at the Work of the RTO Applied Vehicule Technology Panel (AVT) - organised by the former AGARD Structures and Materials Panel- held in Corfu, Greece, 5-6 october 1998 Titre original : Homologation des programmes de prolongation du cycle de vie des organes moteur Type de document : texte imprimé Auteurs : RTO Applied Vehicule Technology (AVT), Auteur Editeur : NATO - OTAN Année de publication : 1999 Collection : RTO Research and Technology Organisation num. RTO-MP-17 AC/323(AVT)TP/17 Importance : pagination multiple Présentation : ill. noir&blanc, schémas, photos Format : 29.5 x 21 cm ISBN/ISSN/EAN : 978-92-8371-012-7 Prix : Distribution of Unclassified RTO Publications Langues : Anglais (eng) Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:Mécanique et fonctionnement du vol aéronautiqueTags : aircraft engines service life life cycle costs defense economics damage control durability performance reliability materials replacement protective coatings reconditioning maintenance design safety engineering tolerances (mechanics) fatigue (materials) cost effectiveness benefit cost analysis turbine components Index. décimale : D.004 Partie constituante d'aéronef ou d'avion Résumé : The replacementcost of service-damaged components contributes significantly to the life cycle costs of an aero-engine. Damaged engine components also impact on the realibility and safety of aircraft. RTO Meeting proceedings, 17. Qualification of life extension schemes for engine components = Homologation des programmes de prolongation du cycle de vie des organes moteur : Papers presented at the Work of the RTO Applied Vehicule Technology Panel (AVT) - organised by the former AGARD Structures and Materials Panel- held in Corfu, Greece, 5-6 october 1998 [texte imprimé] / RTO Applied Vehicule Technology (AVT), Auteur . - [S.l.] : NATO - OTAN, 1999 . - pagination multiple : ill. noir&blanc, schémas, photos ; 29.5 x 21 cm. - (RTO Research and Technology Organisation; RTO-MP-17 AC/323(AVT)TP/17) .
ISBN : 978-92-8371-012-7 : Distribution of Unclassified RTO Publications
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:Mécanique et fonctionnement du vol aéronautiqueTags : aircraft engines service life life cycle costs defense economics damage control durability performance reliability materials replacement protective coatings reconditioning maintenance design safety engineering tolerances (mechanics) fatigue (materials) cost effectiveness benefit cost analysis turbine components Index. décimale : D.004 Partie constituante d'aéronef ou d'avion Résumé : The replacementcost of service-damaged components contributes significantly to the life cycle costs of an aero-engine. Damaged engine components also impact on the realibility and safety of aircraft. Réservation
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Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 231 D.004 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible RTO Meeting proceedings, 24. Application of damage tolerance principles for improved airworthiness of rotocraft / RTO Applied Vehicule Technology (AVT) (2000) / 978-92-8371-024-0
Titre de série : RTO Meeting proceedings, 24 Titre : Application of damage tolerance principles for improved airworthiness of rotocraft : Papers presented at the specialists Meeting of the RTO Applied Vehicle Technology Panel (AVT), held in Corfu, Greece, 21-22 april 1999 Titre original : L'application des principes de la tolérance à l'endommagement pour une meilleure aptitude au vol des aéronefs à voilure tournante Type de document : texte imprimé Auteurs : RTO Applied Vehicule Technology (AVT), Auteur Editeur : NATO - OTAN Année de publication : 2000 Collection : RTO Research and Technology Organisation num. RTO-MP-24 AC/323/(AVT)TP/12 Importance : pagination multiple Présentation : ill. noir&blanc, schémas, photos Format : 29.5 x 21 cm ISBN/ISSN/EAN : 978-92-8371-024-0 Prix : Distribution of Unclassified RTO Publications Langues : Anglais (eng) Tags : Rotary wing aircraft helicopters airworthiness damage tolerances (mechanics) service life safety fatigue (materials) design flight control systems engineering crack propagation loads(forces) delaminating equipement health monitoring structures metals composite structures composite materials Index. décimale : D.002 Aéronef Résumé : The specialists' meeting dealt with aging systems and more specifically application of damage tolerance principles of improved airworthiness of rotorcraft. RTO Meeting proceedings, 24. Application of damage tolerance principles for improved airworthiness of rotocraft = L'application des principes de la tolérance à l'endommagement pour une meilleure aptitude au vol des aéronefs à voilure tournante : Papers presented at the specialists Meeting of the RTO Applied Vehicle Technology Panel (AVT), held in Corfu, Greece, 21-22 april 1999 [texte imprimé] / RTO Applied Vehicule Technology (AVT), Auteur . - [S.l.] : NATO - OTAN, 2000 . - pagination multiple : ill. noir&blanc, schémas, photos ; 29.5 x 21 cm. - (RTO Research and Technology Organisation; RTO-MP-24 AC/323/(AVT)TP/12) .
ISBN : 978-92-8371-024-0 : Distribution of Unclassified RTO Publications
Langues : Anglais (eng)
Tags : Rotary wing aircraft helicopters airworthiness damage tolerances (mechanics) service life safety fatigue (materials) design flight control systems engineering crack propagation loads(forces) delaminating equipement health monitoring structures metals composite structures composite materials Index. décimale : D.002 Aéronef Résumé : The specialists' meeting dealt with aging systems and more specifically application of damage tolerance principles of improved airworthiness of rotorcraft. Réservation
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Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 235 D.002 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible
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