91.Semana de Caro

Question

Q1. The maximum speed at which a plane can use its breaks is mostly related to:

Answer 1

A. The drag of the wheels due to the wind

Answer 2

B. The capability of the break system to dissipate energy

Answer 3

C. The viscosity of the hydraulic system

Answer 4

D. The inerce created by a fast deceleration

Answer 5

A. Compression

Answer 6

B. Expansion

Answer 7

C. Compression and it needs to disipate the energy generated

Answer 8

D. Expansion but it’s a system which doesn’t need to disipate any energy

Answer 9

A. It will be able to stop 0.5 the time it would need without brakes

Answer 10

B. It will be able to stop in 500m

Answer 11

C. It will be able to resist a energy dissipation of a breaking distance of 1500m

Answer 12

D. It will continue being useful after a breaking of 500m

Answer 13

A. Consists of an anti-locked breaking system

Answer 14

B. Is typical in aeronautics

Answer 15

C. Is located in the aileron of the F1 cars

Answer 16

D. Recovers energy from the braking

Answer 17

A. By using a thermal fuse

Answer 18

B. By using chemical substances

Answer 19

C. By using protections in the contact zone between the brake and the wheel

Answer 20

D. By strengthening the discs of the braking system

Answer 21

A. External diameter and section

Answer 22

B. Section and maximum tyre pressure

Answer 23

C. External diameter, section and maximum groundspeed

Answer 24

D. External diameter, section and hub diameter

Answer 25

A. There is a viscous liquid in the taxiway while taxiing

Answer 26

B. A wedge of water builds up in front of your tires and lifts them off the runway

Answer 27

C. Tires lock up, the rubber begins to melt, and trapped water under the tire turns into steam

Answer 28

D. All previous answers are correct

Answer 29

A. The aircraft mass but it doesn’t depend on the heat sink specific heat

Answer 30

B. Temperature increment during braking

Answer 31

C. A and B are correct

Answer 32

D. A and B are false

Answer 33

A. Elevator

Answer 34

D. A,B and C more basic maneuvers.

Answer 35

D. All are correct

Answer 36

D. All are correct

Answer 37

A. 1500 psi

Answer 38

B. 2000 psi

Answer 39

C. 2500 psi

Answer 40

D. 3000 psi

Answer 41

A. Unstable and very maneuverable

Answer 42

B. Stable and very maneuverable

Answer 43

C. Unstable and not maneuverable

Answer 44

D. Stable and not maneuverable

Answer 45

B. Reliability

Answer 46

C. Minimum weight and cost

Answer 47

D. A,B and C are correct

Answer 48

A. 1 failure per 10^3 million hours

Answer 49

B. 10 failure per 1 million hours

Answer 50

C. 1 failure per 10^3 billion hours

Answer 51

D. All are false

Answer 52

A. Fly by wire

Answer 53

B. Power by wire

Answer 54

C. Mechanical by wire

Answer 55

D. Electrical by wire

Answer 56

A. Elevator, flaps, lateral

Answer 57

B. Pitching, rolling, yawing

Answer 58

C. Spoilers, direction, rudder

Answer 59

D. Yaw, pitch, rudder

Answer 60

A. Aerodynamic forces tend put the control surface in an equilibrium position

Answer 61

B. Aerodynamic forces tend put the control surface in an non-controlable position

Answer 62

C. It is imposible to know.

Answer 63

D. None of the above

Answer 64

A. Quick response

Answer 65

B. Slow response

Answer 66

C. Low aerodynamic loads

Answer 67

D. A and C are correct

Answer 68

A. Great cost

Answer 69

B. No high pressure fluid needed

Answer 70

C. Great Maintenance

Answer 71

D. High power ( in relation weight/power)

Answer 72

A) Both are correct

Answer 73

B) 5.2 is correct

Answer 74

C) 5.1 is correct

Answer 75

D) Both incorrect

Answer 76

A. two, electrical

Answer 77

B. three, electrical

Answer 78

C. three, combustion

Answer 79

D. four, electrical

Answer 80

B. Hinge axis displacement

Answer 81

C. Anti-tab

Answer 82

D. Non of the above

Answer 83

A. Split flap

Answer 84

B. Flower flap

Answer 85

C. Plain flap

Answer 86

D. Kruger flap

Answer 87

B. Landing gear

Answer 88

D. A and C are both correct

Answer 89

A. An element which allows a movement being the flexible part the electric engine rotor.

Answer 90

B. The backlash

Answer 91

C. The jamming

Answer 92

D. None of the above

Answer 93

A. It has no electromagnetic effect

Answer 94

B. It is lighter than wive

Answer 95

C. It is cheaper than wive

Answer 96

D. It doesn’t have any advantage

Answer 97

A. Are lighter

Answer 98

B. Are easier to maintain

Answer 99

C. Are safer

Answer 100

D. None of the above

Answer 101

A. Full FBN mode

Answer 102

B. Direct Electrical Link Mode

Answer 103

C. Mechanical Reversion Mode

Answer 104

D. Crew Mode

Answer 105

A. Fly-by-wire

Answer 106

B. Hidraulic transmission

Answer 107

C. Cable and pulley transmission

Answer 108

D. None of the above

Answer 109

A. Transform a position of the hammer into an electrical signal

Answer 110

B. Calculate the movement of the hammer in a hydraulic way

Answer 111

C. Transmit the orders of the flight controls in an electric way

Answer 112

D. Transform an electrical signal into a movement of the pile driver

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91.Semana de Caro

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Question 27

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Question 29

Question 30

Question 31

Question 32

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	Created by Ismael Vázquez about 6 years ago