CHAPTER 5 Flashcards

(30 cards)

1
Q

The concentrator is designed to provide

A

supply of breathing oxygen for two aircrewmembers’ open loop breathing schedules up to 50,000 feet.

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2
Q

The GGU-12/A oxygen concentrator consists of

A

an air heater assembly, inlet filter assembly, pressure reducer assembly, rotary valve assembly, two molecu- lar sieve beds, a plenum assembly, a thermal resistor, a junction box assembly, a thermostatic switch, and a shroud.

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3
Q

The GGU-12/A oxygen concentrator uses

A

engine bleed air and electrical power from the aircraft and provides oxygen-enriched air for aircrewmember breathing.

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4
Q

The regeneration by desorption of nitrogen in the vented bed is enhanced by

A

a reverse flow of oxygen- enriched gas from the output or product end of the pressurized bed.

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5
Q

The amount of the reverse purge flow through the vented bed is controlled

A

by the purge orifice connecting the output ends of the two beds. The two beds are cycled alternately between pressurization or oxygen producing mode and the vented, regenerative mode by the motor driven rotary valve.

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6
Q

The output oxygen-enriched product gas from the pressurized bed flows into

A

the plenum assembly and through check valves at the outlet of each sieve bed preventing backflow.

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7
Q

The oxygen-enriched product gas from the con- centrator flows through

A

a filter and then to the aircrew breathing system.

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8
Q

Mounting

A

2 index pins,2 captive fasteners used for aircraft mounting

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9
Q

Voltage

A

115Vac,400Hz,6amps(max)

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10
Q

Heater

A

1 unit with air heater overtemperature indicator

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11
Q

Filter

A

0.6Micron

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12
Q

Inlet Pressure Range

A

8 to 250 psig, 50 psig preferred

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13
Q

Pressure Reducer

A

Cut in at 50 psig inlet pressure and increases to 85 5 psig at 250 psig inlet pressure

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14
Q

Relief Valve

A

125 psig outlet pressure

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15
Q

Rotary Valve

A

6.35RPM (continuousrotation)

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16
Q

Sieve Beds

A

Two unit, molecular type

17
Q

Plenum

A

Oxygen enriched air storage

18
Q

Junction Box

A

Power supply for heater and rotary valve

19
Q

Operating Altitude Range

A

Sea level to 50,000 feet

20
Q

Operating Temperature

21
Q

oxygen concentrator

Overall Dimensions:

A

Length: 13 3/4inches
Width: 8 2/3inches
Height: 10 1/3inches
Weight: 37.5lbs.

22
Q

GGU-12/A oxygen concentrators which do not pass inspection and cannot be adjusted in the aircraft shall be

A

removed and replaced with a Ready-For- Installation (RFI) GGU-12/A oxygen concentra- tor. The replaced oxygen concentrator shall be for- warded to AIMD/MALS for Bench Test and Repair.

23
Q

The Turnaround/Pre- flight/Postflight/Transfer Inspections are performed

A

in conjunction with the aircraft inspection requirements for the aircraft in which the GGU-12/A oxygen con- centrator is installed.

24
Q

The Acceptance/Special/Daily Inspections shall be performed

A

in conjunction with the aircraft inspection requirements for the aircraft in which the GGU-12/A oxygen concentrator is installed using ap- plicable aircraft technical publications and mainte- nance requirement cards.

25
The Calendar/Phased/SDLM Inspections require
removal of the GGU-12/A oxygen concentrator from the aircraft. In no case shall the interval exceed 400 flight hours.
26
When working with oxygen, make certain that
clothing, tubing, fittings, and equipment are free of oil, grease, fuel, hydraulic fluid, or any combustible liquid.
27
Bench Test shall be performed on the GGU-12/A oxygen concentrator prior
to being placed in service and every 400 flight hours.
28
Bench Test shall be performed using the Oxygen Concentrator Test Set
Model TTU-518A/E only or the Test Set utilizing that OBOGS adapter
29
The Test Set Monitor Test is performed only
if the concentrator fails the Oxygen Flow Test/Filter Drain Flow Test
30
Krytox 240 AC Lubricant
MIL-PRF-27617