Quiz
Tema 1
Crie uma conta grátis para terminar este quiz
Salve seu progresso e veja sua nota final.
Já tem uma conta? Inicie sessão
Perguntas do quiz (28)
1Q1. It is not a function of the airframe
- AA. Transmit the loads
- BB. Allow the taxiing of the aircraft in the airport
- CC. Provide the aerodynamic configuration in every flight condition
- DD. Protect the payload from the environmental conditions
2Q2. The use of biplanes at the beginning of the aviation was due to
- AA. Structural considerations
- BB. Aerodynamic considerations
- CC. A and B are true
- DD. A and B are false
3Q3. The failure of the Langley flight in 1903 was a consequence of
- AA. A defect of velocity to generate enough lift force
- BB. A lack of wing stiffness
- CC. A wrong aerodynamic wing design
- DD. The interference between the front and rear wings
4Q4. The buckling is a phenomenon that appear in (i) structures subjected to (ii) loads
- AA. (i) wide (ii) tension
- BB. (i) wide (ii) compression
- CC. (i) thin (ii) tension
- DD. (i) thin (ii) compression
5Q1. What does the AXIAL STRESS consist on?
- Aa)It occurs when the aircraft is pressurised and the pressure hull lengthens.
- Bb)Stress raised in a container when it is filled, where the contents act to expand thecontainer.
- Cc)It occurs when an structure is subject to several different loads.
- Dd)It produces Stress Cracks due to tension and compression.
6Q2. The factor that doesn’t affect creep (elongation) is:
- Aa)Material type
- Bb)Temperature applied
- Cc)Duration of the load
- Dd)Type of object that produces it
7Q3. Which of the following events does not produce SHOCK LOADS?
- Aa)Bird strike directly on to the compressor blades of a jet engine
- Bb)Heavy landing
- Cc)Old rubber band stretches and then fails before the normal load is applied
- Dd)High intensity wind gust
8Q4. What is DESIGN LIMIT LOAD OR DLL
- Aa) This is the maximum load that the aircraft designer or component manufacturer expects the airframe or component to be subject to in operation.
- Bb) After the aircraft has been subject to this load, there may be permanent deformation of the aircraft’s structure, but it must not collapse.
- Cc) Is equal to the safety factor multiplied by 2
- Dd) Load which produces a catastrophic failure
9Q5. The Safe life is based on:
- Aa) Landings
- Bb) Pressurisation cycles
- Cc) Calendar time
- Dd) All the above
10Q6. About FAIL-SAFE STRUCTURE:
- Aa) Structure safe because one strong takes the entire load.
- Bb) Allows the structure to continue operating normally up to the static ultimate permanently.
- Cc) Damage would be found by luck because the structure does not show any problem.
- Dd) Extra structural items have a weight penalty, and this has led to a change toward designing damage-tolerant structures.
11Q7. DUL = Design Ultimate Load magnitude order in airplanes is:
- Aa) X4
- Bb) X5.5
- Cc) X10
- Dd) None of above
12Q.8 FRAME CONSTRUCTION in airplanes involves the use of mainly:
- Aa) SEMI-MONOCOQUE STRUCTURES
- Bb) MONOCOQUE STRUCTURES
- Cc) BICOQUE STRUCTURES
- Dd) BULB SHAPE STRUCTURES
13Q.9 In regard to the pressurization of the plane:
- Aa) It has a Front Pressure Bulkhead
- Bb) It has a TOP Pressure Bulkhead
- Cc) The plane is completely pressurized to avoid internal forces
- Dd) The Pressure is different depending of the seat that you occupy
14Q.10.PASSENGER CABIN WINDOWS
- Aa) Are essential for temperature regulation
- Bb) The higher pressure of the outside can make them break in mid air
- Cc) Are non-FAIL-SAFE STRUCTURE
- Dd) Are points where the structure weakens
15Q.11 ALUMINUM ALLOYS used in aviation:
- Aa) 2024
- Bb) 4070
- Cc) 7075
- Dd) A and c are correct.
16Q.12 Which of the COMPONENTS OF WING STRUCTURE has holes to let fuel go throw?
- Aa) Spars
- Bb) Ribs
- Cc) Stringers
- Dd) Skin
17Q.13 Which of these resins are used in aviation?
- Aa) BLU- TACK
- Bb) PTFE
- Cc) A and B are true
- Dd) A and B are false
18Q.14 Which of the following materials has been introduced in contemporany times into the structure of new airplanes?
- Aa) Aluminium
- Bb) Steel Phosphate
- Cc) Composites
- Dd) Zinc plus Gold
19Q.15 According to the shape of fuselages, in which type of fuselage is common to find the area rule?
- Aa) Subsonic
- Bb) Supersonic
- Cc) Both of them
- Dd) None is correct
20Q.16 Which are the three spars normally used in a large aircraft?
- Aa) Front spar, forward spar and main spar
- Bb) Front spar, rear spar and auxiliary spar
- Cc) Forward spar, main spar and auxiliary spar
- Dd) Front spar, forward spar and rear spar
21Q.17 The torsion box:
- Aa) Increases the rigidity of the wing and resists the twisting and bending motion
- Bb) Increases the mass of material used during the construction and due to this the weight is increased
- Cc) Is formed between the spars and the stringers
- Dd) Is the best structure to resist the compression forces
22Q.18 From JAR 23s. Aircraft are categorised into 3 groups:
- Aa) Normal, fixed wing aircraft and rotatory wing aircraft
- Bb) Normal, utility and aerobatic
- Cc) Normal, aerobatic and fixed wing aircraft
- Dd) Normal, utility and rotatory wing aircraft
23Q. 19 In combat aircraft the nose and forward fuselage is used to:
- Aa) place the main intake ducts for engines
- Bb) Minimize the length
- Cc) Place secondary fuel tanks
- Dd) Radar and laser-ranging installations
24Q.20 According to monocoque structures, choose the right answer:
- Aa) Are tubes with horizontal armours
- Bb) The skin only supports ground loads
- Cc) Are used in missiles
- Dd) Are easy to design
25Q.21 Which one is the main structural element that gives longitudinal strength?
- Aa) Stringers
- Bb) Formers
- Cc) Longerons
- Dd) Frames
26Q.22 What elements support the pressure loads?
- Aa) Bulkhead and skin
- Bb) Stringers
- Cc) Longerons
- Dd) Longerons and frames
27Q.23 The main objective of winglets is:
- Aa) Delay the critical Mach
- Bb) Increase the stall speed
- Cc) Aesthetic reasons
- Dd) Reduce wing tip vortices
28Q. 24 According to wing mounted engines:
- Aa) Engines are joined to the wing structure by a pylon
- Bb) The pylon is attached to the front and mains spars
- Cc) In flight, the weight of the engine balances the aerodynamic loads (lift)
- Dd) All of them are right
Informações
- Descrição
- Quiz sobre Tema 1, criado por David Nunez em 27-03-2018.
- Autor
- David Nunez
- Idioma
- Español
- Visualizações
- 3
- Etiquetas
- Avaliação
- Ainda sem avaliações Avalie este quiz