AM Book Ch 2 Aircraft Construction & Materials Flashcards
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
*2. On a semi monocoque fuselage, what component absorbs the primary bending loads?
Longerons
The text also mentions that longerons are supplemented by other longitudinal members called “stringers,” but the longerons are the main components handling those primary bending loads!
2-1: The shimmy damper on a nose landing gear assembly prevents the nosewheel from shimmying during takeoff and landing by what means?
- By actuating a low-rate gear train
- By forcing a rotary bar to move against a
friction plate - By accentuating sudden torque loads ap-
plied to the nose wheel - By metering hydraulic fluid through a
small orifice between two cylinders or
chambers
2-3: When comparing catapult hookup methods on a carrier, the nose gear launch method is superior to the holdback pendant method for all EXCEPT which of the following?
- It saves time
- It cost less to operate
- It requires fewer personnel
- It is the safest method
2-4: Which of the following helicopter components provide(s) lift?
The rotor blades
2-6: The tail landing gear of a helicopter is capable of swiveling how many degrees?
- 45°
- 90°
- 180°
- 360°
2-7: What type of spar is used in the construction of a rotor blade?
Titanium spar
2-8: How many rotor blades are attached to the main rotor head of an H-60 helicopter?
Four
2-9: Which of the following components is NOT a part of the tail pylon of a helicopter?
- The intermediate gearbox
- The tail gearbox
- The horizontal stabilator
- The swash plate
2-14: What high tensile metal is used to manufacture tubes, rods, and wires?
- Aluminum
- Titanium
- Magnesium
- Alloy steel
2-20: What metal property allows a metal to carry heat or electricity?
Conductivity
2-21: When all other metal properties are equal, what method of joining metals structurally has the greatest advantage?
Welding
2-22: The intermediate shape of steel that has width greater than twice the thickness and from which sheets are rolled is known by what name?
Slab
2-25: While holding a piece of metal against a
revolving stone, you see red sparks leave the
stone and turn to straw color. This is what type
of metal?
Cast iron
2-27: An aluminum alloy containing manganese as the major alloying element is identified by what number?
3003
2-38: In various aircraft structural components, what materials are replacing and supplementing
metallic materials?
Composite
*3. What multiengine aircraft structure is designed to transmit engine loads, stresses, and vibrations to the aircraft structure?
A. Fuselage
B. Landing gear
C. Nacelle
D. Tires
Nacelle
*4. A rudder is designed to move an aircraft about (movement around) what axis?
A. Lateral
B. Longitudinal
C. Horizontal
D. Vertical
Vertical
*5. What secondary flight controls are small airfoils recessed in the trailing edge of a primary control surface?
A. Slats
B. Spoilers
C. Trim tabs
D. Wing flaps
Trim tabs
“Trim tabs are small airfoils recessed in the trailing edge of a primary control surface. Their purpose is to enable the pilot to neutralize any unbalanced condition that might exist during flight, without exerting any pressure on the control stick or rudder pedals.”
These clever little devices help reduce pilot fatigue by eliminating the need for constant pressure on the controls
*6. What secondary flight control on some aircraft are long, narrow surfaces hinged at their leading edge to the upper wing skin?
A. Slats
B. Spoilers
C. Trim tabs
D. Wing flaps
Spoilers
“The spoilers on some aircraft are long, narrow surfaces hinged at their leading edge to the upper wing skin. In the retracted position, the spoiler is flush with the wing skin. In the extended position, the spoiler is pivoted up and forward.”
The text also mentions that spoilers work by disturbing the smooth airflow over the wing to reduce lift and add drag!