Tesla TI4100 GPU-24 Скачать руководство пользователя страница 21 | Manualshive

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Tesla TI4100 GPU-24 Скачать руководство пользователя страница 21

4-8 28.5 VDC GROUND POWER (WITH 208/240 VAC POWER) SYSTEM LOW POWER

DEMAND (100 amps or less).

1. TRANSPORT UNIT - The Turbo Start 4100 is easily transported us-

ing the wheels that are incorporated into the unit. The unit is en-

gineered to be pushed rather than pulled.

2. CONNECT AC POWER CORD TO UNIT - Make sure that the On/Off switch

is in the Off position. Ensure 208-240 Single Phase VAC 30AMP power

cord is properly connected to an approved AC power supply. Unit shall

be in Horizontal position to ensure unit’s vent ports are free from

blockage. After approximately 5-8 seconds, unit’s LED status indica-

tor will illuminate indicating power cells state of charge. Cooling

fan will operate. Ensure LED status indicator and cooling fan are

operational prior to continuing to step 3.

NOTE

THE ON/OFF SWITCH CONTROLS THE AC POWER INPUT. IT DOES NOT CONTROL

THE DC POWER OUTPUT. IF YOU PLUG THE UNIT INTO AN AIRCRAFT WITH THE

AC ON/OFF SWITCH IN THE OFF POSITION, THE UNIT WILL STILL PROVIDE

24VDC POWER TO THE AIRCRAFT.

3. CONNECT DC POWER CABLE TO UNIT - Ensure power cable connector is

fully seated into unit’s receptacle.

4. CONNECT DC POWER CABLE TO AIRCRAFT - Connect to aircraft ground

power receptacle. DC bus power should come on and aircraft volt

meter should indicate 27.5 VDC to 23.5 VDC (23 VDC minimum).

5. MOVE THE ON/OFF SWITCH TO THE ON POSITION - After approximately

2-3 seconds, the unit’s LED bar status indicator will illuminate,

indicating the power cells state of charge. The cooling fans will

operate. Ensure the LED status indicator and cooling fans are opera-

tional. At this time the unit can provide 100 amps at 28.5 VDC. If

the current demand is above 100 amps, the output voltage will de-

crease and two or more LED status indicator bars will illuminate.

7. REMOVING DC POWER SUPPLY FROM AIRCRAFT

a. Switch the ON/OFF switch to the OFF position

b. Remove DC power cable GPU connector from aircraft.

c. Remove DC power cable connector from Turbo Start (if neces-

sary).

4-9 POWER CELL RECHARGE

1. CONNECT AC POWER CORD TO UNIT -

Unit shall be in horizontal po-

sition to ensure unit’s vent ports are free from blockage. - Ensure

208-240 VAC power cord is properly connected to an approved AC power

supply. After approximately 5-8 seconds, ensure unit’s LED status

indicator illuminates indicating power cell state of charge and cool-

ing fan is operating.

4-5

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Содержание TI4100 GPU-24

Страница 1: ...012 3 45 6 7 8 9 3 02 1 1 A BCD201 4E5 1 A BCD20 F G www TESLAind com TI4100 GPU 24...

Страница 2: ...NT BLVD CENTERPOINT INDUSTRIAL PARK NEW CASTLE DELAWARE 19720 PH 302 324 8910 FAX 302 324 8912 WARNING SHOCK HAZARD POTENTIAL ATTEMPTS TO OPEN OR ENTER THE INSIDE OF THIS UNIT BY USING ANY TOOL OR DEV...

Страница 3: ...s 4 2 Section III Functional Check Procedures 4 5 CHAPTER 5 PERFORMANCE DATA 5 1 Section I Introduction 5 1 Section II Data Criteria 5 2 CHAPTER 6 CARE AND MAINTENANCE 6 1 Section I Unit Care 6 1 Sect...

Страница 4: ...ipment NOTE An operating procedure condition etc which is essential to highlight 1 3 DESCRIPTION This manual contains the complete operating instructions and proce dures for the TI4100GPU 24 Turbo Sta...

Страница 5: ...are used in this manual LIST OF ABBREVIATIONS AND SYMBOLS Abbreviation Definition amp Ampere AC Alternating Current C Celsius cont Continuous DC Direct Current F Fahrenheit Ft Feet FWD Forward GPU Gr...

Страница 6: ...technical manual the word shall is used to indicate a mandatory requirement for proper operation and warranty purposes The word should is used to indicate a non mandatory but preferred method of accom...

Страница 7: ...mp output of the 208 240 VAC to 28 5 VDC converter or a combination of converter and power cell output to provide 24 VDC output The following are the unit s four 4 main operational support capabilitie...

Страница 8: ...4100GPU 24 208 240 Single Phase VAC 50 60 Hz 30 0 amps max OUTPUT POWER DC CONVERTER 28 5 VDC TO 100 AMPS 24 VDC 121 AMPS AND ABOVE POWER CELLS 24 VDC PEAK OUTPUT 1500 AMPS POWER CELL DRY HIGH RATE DI...

Страница 9: ...2 3 UNIT DISCRIPTION AND DEMENTIONS...

Страница 10: ...ty from the Turbo Start 4100 ground power unit SECTION II OPERATIONAL RESTRICTIONS AND SAFETY LIMITS 3 3 POWER CELL RECHARGE LIMITS Any time the unit s power cells are discharged the unit shall be rec...

Страница 11: ...he power cells are fully charged the unit s intelligent charger will go to a standby mode monitor the power cells state of charge and only charge the power cells to ensure they stay at maximum capacit...

Страница 12: ...tion Use only adapters with proper ground ing mechanism 3 6 ONE 1 HOUR RATE 24 VDC CONSTANT OUTPUT 23 amp hour without AC power connected power cell output see Figure 5 2 123 amp hours with AC power c...

Страница 13: ...icient engine start under specific current load demands ENGINE START CURRENT LOAD DEMAND MINIMUM CHARGE Under 650 peak starting amps 40 charged 650 850 peak starting amps 50 charged 850 1000 peak star...

Страница 14: ...ffort has been made within the scope of existing technology to prevent foreseeable safety hazards and make the Turbo Start 4100 moisture resistant to prevent damage or failure If the Turbo Start 4100...

Страница 15: ...ithout 208 240 power cord DO NOT CONNECT 208 240 VAC power cord until unit has been dried for a MINIMUM of one 1 hour prior to use Blowing sand or dust Minimize exposure to sand and dust when 208 240...

Страница 16: ...ower cell output only DO NOT CONNECT 208 240 VAC POWER SUPPLY 208 240 VAC power charger or AC DC converter functions of unit shall not be operated during any aircraft fuel handling operation WARNING F...

Страница 17: ...he unit 4 2 OPERATING LIMITS AND RESTRICTIONS The minimum maximum and normal operating ranges result from careful engineering and evaluation of test data These limitations must be adhered to during al...

Страница 18: ...is plugged in the unit must be placed in the horizontal position to allow the cooling fan to operate properly 4 5 BEFORE OPERATION CHECK 1 CHECK UNIT FOR STATE OF CHARGE Ensure power unit is connected...

Страница 19: ...unit is engi neered to be pushed rather than pulled 2 CONNECT DC POWER CABLE TO UNIT Ensure power cable connector is fully seated into unit s connector Set the unit down horizontally ensuring vent po...

Страница 20: ...ctor is fully seated into unit s receptacle 4 CONNECT DC POWER CABLE TO AIRCRAFT Connect to aircraft ground power receptacle DC bus power should come on and aircraft volt meter should indicate 27 5 VD...

Страница 21: ...is fully seated into unit s receptacle 4 CONNECT DC POWER CABLE TO AIRCRAFT Connect to aircraft ground power receptacle DC bus power should come on and aircraft volt meter should indicate 27 5 VDC to...

Страница 22: ...y charged the last LED bar AC power may be left connected to unit when power cells are fully charged NOTE Under a full charge two things will be observable with the unit A non blinking lighted green b...

Страница 23: ...INTO 208 240 VDC Unplug AC power if plugged in 3 CHECK UNIT INTERNAL RESISTANCE TEST FOR SHORTS Better than 10 Megohms Ensure no short exists Negative DC receptacle terminal and unit case Positive DC...

Страница 24: ...blink ing green bar at the bottom of the LED column both indicate a full charge 7 CHECK DC VOLTAGE READING AT DC RECEPTACLE TERMINALS Ensure power cells are fully charged see step 6 28 5 0 57 VDC with...

Страница 25: ...ables for which data is not presented d To help the operator determine if an aircraft system malfunc tion exists by comparing actual performance with expected perfor mance NOTE The information provide...

Страница 26: ...a are not presented but which may affect that phase of performance are discussed in associated text Where data are available or reasonable estimates can be made the amount that each variable affects p...

Страница 27: ...5 3 FIGURE 5 1...

Страница 28: ...FIGURE 5 2 5 4 TI41000GPU 24 OUTPUT VOLTAGE OUTPUT VOLTAGE MINUTES 23 AMP CONSTANT CURRENT LOAD 24 20 16 12 8 4 0 0 10 20 30 40 50 60...

Страница 29: ...5 5 0 0 150 300 450 600 750 900 1050 1500 1350 1200 5 10 15 20 25 30 25 C Temp 29 C Temp Calculations based on actual test data at Pratt Whitney Canada on 30 March 1992 SECONDS AMPS MAXIMUM OUTPUT CU...

Страница 30: ...TER CASE CLEAN wipe with dry cloth 2 KEEP FOREIGN OBJECTS OUT OF UNIT Cover unit to prevent foreign objects water and dirt from entering vent ports and recep tacles 3 KEEP FROM PROLONGED EXPOSURE TO E...

Страница 31: ...4100 is a maintenance free unit no repairs are authorized Warranty will be void if unit is tampered with If unit fails to operate contact Manufactures War ranty Claim see unit warranty 6 2 Warranty V...

Страница 32: ...ACTED FROM THE UNIT BEFORE YOU DEPRESS THE PUSH TO TEST BUTTON THIS WILL ENSURE A CORRECT READING 2 WITHOUT AC POWER INPUT OR DC POWER OUTPUT SIMPLY DEPRESS THE PUSH TO TEST BUTTON ON THE FACE PLATE A...

Страница 33: ...ut power funtion 8 2 OPERATION 1 Place the On Off switch in the Off position 2 Plug the unit into 208 240 single phase 30 AMP AC power 3 Connect the DC cord to the Aircraft or vehicle At this time the...

Страница 34: ...Limits 3 5 After Use 6 2 Appendix A Line Cord Table Before Operation Check 4 5 Continuous Output Rate 28 5 VDC Constant Output 3 8 Data Basis 5 3 DC Functional Check 4 12 Definitions of Abbreviations...

Страница 35: ...s 4 4 Operating Position 3 12 Performance 4 3 Power Cell Recharge 4 9 Power Cell Recharge Limits 3 3 Purpose Chapter 3 3 1 Purpose Chapter 5 5 1 Rated Peak Output Engine Starting 3 7 Required Equipmen...

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