問題一覧
1
He invented the “Turbo Jet”, it was first used in 1941
2
True
3
False
4
Turbo shaft
5
False
6
True
7
False
8
Springs
9
False
10
Exhaust gas temperature, outside air temperature
11
Engines can be broken down into separate sections, each section with its own log book and serial number. Each section can be replaced by a new assembly
12
The Brayton cycle
13
False
14
True
15
Hi-bypass
16
Hot section, cold section
17
250mph
18
?
19
Bernoulli
20
Turbo prop
21
Equivalent shaft horsepower. One pound of thrust = one thrust horsepower when flying at 375mph
22
Engine pressure ratio, true
23
True
24
375mph
25
36,000 ft
26
Convergent
27
True
28
Convergent
29
Pressure Increasing, velocity decreasing
30
Divergent
31
True
32
Variable guide vane adjusts its angle to match airflow. Delivers air to the inlet of the engines compressor
33
1. Simple to manufacture 2. Low weight and cost 3. Accelerates air rapidly 4.Efficient energy transfer
34
The diffuser station
35
Airframe
36
Bring in more air into engine under low speeds and high thrust demands from the plane
37
True
38
High temp bleed air from the compressor to the air inlet
39
They reduce FOD entering the engines
40
An inlet with movable ducts that move in order to provide the best effiency for the engine at different performance levels. SR71, Concorde
41
Positive
42
Free turbine
43
True
44
False
45
False
Composites test 2
Composites test 2
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11問 • 2年前問題一覧
1
He invented the “Turbo Jet”, it was first used in 1941
2
True
3
False
4
Turbo shaft
5
False
6
True
7
False
8
Springs
9
False
10
Exhaust gas temperature, outside air temperature
11
Engines can be broken down into separate sections, each section with its own log book and serial number. Each section can be replaced by a new assembly
12
The Brayton cycle
13
False
14
True
15
Hi-bypass
16
Hot section, cold section
17
250mph
18
?
19
Bernoulli
20
Turbo prop
21
Equivalent shaft horsepower. One pound of thrust = one thrust horsepower when flying at 375mph
22
Engine pressure ratio, true
23
True
24
375mph
25
36,000 ft
26
Convergent
27
True
28
Convergent
29
Pressure Increasing, velocity decreasing
30
Divergent
31
True
32
Variable guide vane adjusts its angle to match airflow. Delivers air to the inlet of the engines compressor
33
1. Simple to manufacture 2. Low weight and cost 3. Accelerates air rapidly 4.Efficient energy transfer
34
The diffuser station
35
Airframe
36
Bring in more air into engine under low speeds and high thrust demands from the plane
37
True
38
High temp bleed air from the compressor to the air inlet
39
They reduce FOD entering the engines
40
An inlet with movable ducts that move in order to provide the best effiency for the engine at different performance levels. SR71, Concorde
41
Positive
42
Free turbine
43
True
44
False
45
False