Pressure sensing Flashcards

1
Q

what instruments rely only on sensing pressure?

A

Altimeter
VSI
ASI
machmeter

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2
Q

Pressure sensing threats?

A

blockages

leaks

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3
Q

Units of pressure

A

1 Pa= 1 N/m2
1 mb= 1hPa
ISA pressure= 1013.25 hPa, 29.92inHg, 14.7psi

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4
Q

When is psi usually used?

A

for oil pressure, hydraulic pressure and differential cabin pressure

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5
Q

Gauge pressure

A

Dif between pressure to be measured and atmospheric

zero- referenced against ambient air pressure

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6
Q

absolute pressure

A

Dif between pressure to be measured and a vacuum

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7
Q

differential pressure

A

Dif between two sampled pressures

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8
Q

Aneroid capsule

A

single or multilayered
sealed partially evacuated
leaf spring(to stop capsule collapsing)

aneroid means no flow
thin sheets of brass(naturally springy)

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9
Q

other measuring devices

A

pressure capsules- not sealed, lets pressure in and out
diaphragms- flexible membrane move back and forth
burden tube- partially flatten tube wound into a curve, relatively stiff so measures high pressures

MEM tube- convert pressures to electrical signals

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10
Q

Static pressure

A

result of weight of air above object
fluid so acts in all directions
reduces as alt increases

only static instruments= VSI & altimeter

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11
Q

Pitot pressure

A

Also known as stagnation or total pressure

dynamic + static = pitot pressure

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12
Q

dynamic pressure

A

known as impact pressure
can’t directly measure
pressure relative to motion
dynamic= pitot - static

increases as airspeed increases

= 1/2pV2

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13
Q

pitot tube

A

parallel to longitudinal axis
needs heat element
drain from bottom

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14
Q

Static port

A

pairs at right angles to airflow
manoeuvre errors reduced by pairs
alternate static on light aircraft usually read low due to suction

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15
Q

combined probe

A

both pitot and static

common on light but not on large transport

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16
Q

What are the 3 main sources of errors?

A

IMP
instrument: manufacturer imperfections, play in linkages, friction
manoeuvre: temp changes in RAF, can’t really stop
position; modifications to airflow caused by aircraft, pitot and static port location