AM Book Ch 2 Aircraft Construction & Materials Flashcards
(109 cards)
What does the airframe of a fixed-wing aircraft consist of?
5 principal units: fuselage, wings, stabilizers, flight control surfaces, and landing gear
What does the airframe of a rotary-wing aircraft consist of?
Fuselage, landing gear, main rotor assembly, and tail rotor.
How many principal structural units are there on a fixed-wing (conventional) aircraft?
9: fuselage, engine mounts, nacelle(s), wings, stabilizer(s), flight control surfaces, and landing gear, arresting gear, and catapult equipment.
What is the main structure or body of the aircraft to which all the units attach?
Fuselage
What provides space for crew, passengers, cargo, most of the accessories, and other equipment?
Fuselage
The monocoque design can be divided into how many classes?
-monocoque design relies largely on strength of of skin or shell to carry various loads.
3: monocoque, semi-monocoque, reinforced shell
How is monocoque reinforced?
Has its only reinforcement vertical rings, station webs, and bulkheads
How is semimoncoque reinforced?
With same monocoque features and with addition with skin is reinforced by longitudinal members, that are stringers and longerons, but no diagonal web members.
How is reinforced shell reinforced?
By a complete framework of structural members.
Cross sectional shape= bulkheads, station webs, and rings,
Longitudinal contour with longerons, formers, and stingers. The skin is fastened to all these members, primarily Carrie’s the shear load and together with longitudinal members Carrie’s loads of tension and bending stresses.
How is the longitudinal contour developed?
Longerons, formers, and stringers
What materials is a semimonocoque fuselage co trusted primarily by?
Aluminum alloy, newer A/C use graphite epoxy composite. Steel and titanium are found in areas subject to high temperatures.
What absorbs primary bending loads?
Longerons
What structure carry concentrated loads where fittings attach other units like what?
Vertical members referred to bulkheads, frames, and formers.
Units that attach to it are wings, engines, and stabilizer.
How many sections are in fuselage in small aircraft compared to larger aircraft?
Small aircraft= 2 or more sections
Larger= 6 sections.
Station markings?
Various points in fuselage located by station number. A station on aircraft may be a rib or frame number
Fuselage Stations (FS)are neasured in?
Station 0 is @ or near nose of aircraft. Other stations are distances measured in inches aft of station 0.
Vibrations originating in the engine are transmitted to aircraft structure through the ___?
Engine mounts
Nacelles are similar in shape and design for the same size aircraft. Larger aircraft require less fairing therefore _____ nacelles.
Smaller
I’m certain cases the ____ is designed to transmit engine loads and stress to the ____ through the engine mounts.
Nacelle,
Wings
Internal structure of wings running spanwise?
Spars and stringers
Spars are main structural members of wing, often referred to as “beams”.
Internal structure is wings running chordwise (leading edge to trailing edge)?
Ribs and formers
What’s a box beam construction?
The stringers and sparlike sections are joined together in a box shaped beam. Remainder of wing is constructed around the box.
How many variations are there for wing construction?
3, monospar, multispar, and box beam
*1. How many principal structural units are there in a fixed wing aircraft?
5,
Fuselage, wings, stabilizers, flight control surfaces, and landing gear