ZHAW Aviatik AC-SYS Manfriani HS15
Theoriefragen der Vorlesungen
Theoriefragen der Vorlesungen
Kartei Details
Karten | 10 |
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Lernende | 52 |
Sprache | English |
Kategorie | Technik |
Stufe | Universität |
Erstellt / Aktualisiert | 02.11.2015 / 23.01.2021 |
Lizenzierung | Keine Angabe |
Weblink |
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Aircraft: Core functions, essential functions and auxiliary functions
Core functions: flight: takeoff, land, climb, cruise, descend, maneuver; Payload transport:load, unload, storage.
essential functions: Propulsion, power generation, information, control, CNS, NAV, Crew and passenger safety.
auxiliary functions: Crew and passenger coonfort, Flight planning and management, Bad weather avoidance, ice protection.
Aircraft: Subsystems:
Structure (airframe): Fuselage, Wings, Flaps, Empennage, Control surfaces.
Vehicle systems: Landing gear, Flight controls, propulsion, fuel system, hydraulics, electrics, environmental control system.
Avionic systems: Navigation, controls, displays, flight management, CNS.
Mission systems: Sensors, mission computers, weapons, passive defence.
which of the aircrafts subsystems are physical inegrated? which are informationally integrated?
The structure (airframe) and the vehicle systems have a strog physical inegration.
Avionics and mission system have an information based integration.
All systems interact.
Practical safety objectives: Definitions of words:
System: A combination of parts, components, facilities, procedures, personell, skills, ..., that are connected in an organized way to perform one or more functions.
Functions: The lowest level of a specific action of a system, equipment and flight crew performance on the airplane.
Failure: the inability of a system, subsystem or component to perform a function as intended.
Failure condition: a condition with an effect on the ACFT and its occupants caused by one or more failures considering the relevant operational and environmental conditions.
Types of failures:
-function not provided when required.
-function provided incorrectly.
-function provided when not required.
design-concepts:
Safe-Life: system or components will survive a specific design-life w/ no failures.
Fail-Safe: a failure will cause no or minimum harm to other parts and systems or danger to personnel.
Fault-Tolerant: the system can continue operating in the event of the failure of one or more of it components.
what is a stringer? where is it used?
To make the fuselage stiffer.
Fuselage.
Reference systems:
zones and coordinates.