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3 Manual Number 9018047 • Revision L, January 6, 2022

REVISION HISTORY

Rev

Date

Detail

Approved

10/17/2013

Initial release.

BAW

12/10/2013

Miscellaneous revisions to grammar and content.

BAW

10/23/2015

Updates for MOD 1 monitoring signal definitions and other
miscellaneous revisions.

BAW

03/21/2016

Updates for MOD 2 battery operational characteristics;
added QTR 1727 and DO-160 Sections 10, 12 to Appendix
1 EQF.

BAW

04/22/2016

Added Modifications section (2.6).

WVC

06/23/2017

Added 6430017-2 and associated references; revised
weight to 16.0 lbs.; clarified battery storage charge interval.

WVC

11/01/2017

Removed technical content not required for Installation and
Operating Instructions.

WVC

05/04/2020

Updated style and brand to meet Marketing and
Engineering guidelines. Section 1.5.1, updates to title and
symbols. Inserted Section 5.7, Environmental Qualification
Statement.

DLR

09/21/2020

Added 6430017-3 and -4 and associated references.

VAA

07/23/2021

Updated dimensions to single place precision.

MEK

01/06/2022

Added recommended chargers; updated Section 4.2,
added Section 5.2.2

WVC

Содержание TB17 Series

Страница 1: ...Revision L January 6 2022 ...

Страница 2: ... truebluepowerusa com www mcico com We welcome your comments concerning this manual Although every effort has been made to keep it free of errors some may occur When reporting a specific problem please describe it briefly and include the manual part number the paragraph figure table number and the page number Send your comments to True Blue Power c o Mid Continent Instrument Co Inc Attn Technical ...

Страница 3: ...TION 9 2 3 ROUTING OF CABLES 9 2 4 LIMITATIONS 10 2 5 MODIFICATION 10 SECTION 3 INSTALLATION 11 3 1 GENERAL 11 3 2 PRE INSTALLATION INSPECTION 11 3 3 PARTS 11 3 4 INSTALLATION 12 SECTION 4 OPERATION 16 4 1 DESCRIPTION 16 4 2 OPERATIONAL MODES 16 4 3 ACTIVE MONITORING 18 SECTION 5 CONFORMANCE 19 5 1 DISPATCH VERIFICATION AND IN FLIGHT MONITORING 19 5 2 ROUTINE MAINTENANCE 19 5 3 COMPONENT MAINTENAN...

Страница 4: ...ions section 2 6 WVC F 06 23 2017 Added 6430017 2 and associated references revised weight to 16 0 lbs clarified battery storage charge interval WVC G 11 01 2017 Removed technical content not required for Installation and Operating Instructions WVC H 05 04 2020 Updated style and brand to meet Marketing and Engineering guidelines Section 1 5 1 updates to title and symbols Inserted Section 5 7 Envir...

Страница 5: ...s associated with the proper care and use of this product 1 2 PHYSICAL ATTRIBUTES The TB17 is a single integrated component contained in a metal enclosure with positive and negative power terminals and a 7 pin circular communication connector The top of the enclosure supports the use of a hold down bar for typical aircraft mounting There is a 1 inch diameter vent port on top of the unit for an exh...

Страница 6: ... 26 4 volts DC Nominal Continuous Current 500A Power Peak Current IPP 840A Power Rated Current IPR 600A Battery Capacity 17 amp hours Ah 23 C Table 1 1 Physical Attributes Weight 16 0 pounds 7 2 kg 1 and 2 configurations 17 1 pounds 7 5 kg 3 and 4 configurations Dimensions see Figure 1 1 not including vent or connectors 7 3 x 7 4 x 6 1 inches 1 and 2 configurations 185 x 188 x 155 mm 7 3 x 9 4 x 6...

Страница 7: ...6 Manual Number 9018047 Revision L January 6 2022 Figure 1 1 1 and 2 Unit Outline Drawing Figure 1 2 3 and 4 Unit Outline Drawing ...

Страница 8: ...ery Remove metal items such as rings bracelets and watches when working with battery packs A battery could produce a short circuit current high enough to weld jewelry to metal and cause a severe burn Always use appropriate Electrostatic Discharge ESD protection while working with the battery pack All connections for battery pack testing must include appropriate short circuit protection The battery...

Страница 9: ...ations as prescribed by industry and regulatory standards This includes compliance with the UN recommendations on the Transport of Dangerous Goods IATA Dangerous Goods Regulations and applicable U S DOT regulations for the safe transport of lithium ion batteries and the International Maritime Dangerous Goods Code In accordance with IATA and per UN 3480 PI 965 Section 1A and 1B the TB17 series Adva...

Страница 10: ...vent of such an occurrence Details for vent installation are provided in Section 3 The unit should not be installed in compartments where lines tanks or equipment containing fuel oil or other flammable fluids are present Installation near potential sources of ignition should be avoided Consideration should be given to how the status and reporting functions of the battery will be displayed within t...

Страница 11: ...r part number description certification s and technical specifications of the unit It also includes the MOD or modification number representing notable changes in the hardware design of the unit Modification MOD 0 is the initial release of the product and is identified on the nameplate by the lack of marking on the MOD numbers 1 through 9 i e 1 9 are visible All subsequent modifications are identi...

Страница 12: ...nsit If necessary return the unit to the factory using the original shipping container and packing materials File any claim for damages with the carrier 3 3 PARTS Included Parts A TB17 Advanced Lithium ion Battery MCIA P N 6430017 B Hold down bar assembly MCIA P N 9018087 C Installation and operation manual MCIA P N 9018047 Available Parts A Connector Kit MCIA P N 9018048 i Power terminal lugs ii ...

Страница 13: ...owing steps Harness Preparation Prepare aircraft wiring with mating connectors in accordance with the proper Wire Size and Type Table 3 1 Connector Locations and Pin Identification Diagrams Figure 3 1 and Table 3 2 Terminal bolts for negative and positive terminals torque should not exceed 65 in lbs 7 3 Nm Use of PTFE ETFE TFE Teflon or Tefzel insulated wire is recommended for aircraft use Recomme...

Страница 14: ...13 Manual Number 9018047 Revision L January 6 2022 Figure 3 1 Connector Locations Negative Terminal Vent Port Comm Connector Positive Terminal Label Nameplate ...

Страница 15: ...ting connectors in accordance with the proper Wire Size and Type Table 3 1 Connector Locations Figure 3 3 and Quick Disconnect Power Receptacle Figure 3 4 Figure 3 3 Figure 3 4 Connector Locations Quick Disconnect Power Receptacle Vent Port Comm Connector Quick Disconnect Power Receptacle A C B D F G E Positive Power Pin Negative Ground Pin Pin Pin Function 28VDC power in aircraft ground Power Rec...

Страница 16: ...that the TB17 be operated with the vent tube in place when installed in the aircraft The vent is located on the top of the unit has a diameter of 1 0 inch 25 4 mm and is 0 75 inches 19 mm tall Use the vent tube and attachment hardware as supplied in the Vent Kit P N 9018049 Contact True Blue Power for potential alternatives The vent tube should be properly and securely attached to an aircraft exit...

Страница 17: ... load greater than 35mA The unit will recycle hourly and test for these conditions in order to remain active or transition to Sleep Mode Additionally grounding the heater enable switch 2 and 4 units only will also transition the battery into Active Mode Providing Aircraft Power When the aircraft s power generation systems are offline or fail the unit will provide immediate power to the equipment l...

Страница 18: ...eater is disabled Heater is disabled Battery is in Active Mode Heater is enabled See below Heater enable pin is grounded 2 4 Units only N A Heater is enabled Heater enable pin is open 2 4 Units only Note Battery may be in Sleep Mode or Active Mode N A Heater is disabled Table 4 1 Heater Operation Condition When the heater is enabled it is active on when the temperature of the battery is below 10 C...

Страница 19: ...w up to 37 5A before the charge limiting activates and then restricts the input to a maximum of 34A Even at the charge limit rate of 34A a fully depleted unit will completely recharge in about 30 minutes In typical applications the unit is likely to be fully re charged from the aircraft power generation system within several minutes following an engine start 4 3 ACTIVE MONITORING When in Active Mo...

Страница 20: ...rmation to the cockpit or crew through its communication outputs see section 4 3 In Flight Monitoring Typically all annunciations from the unit should be inactive during flight However CHARGE and HEATER signals may be observed depending on the state of the unit and do not represent a hazard or loss of function An indication of the FAULT signal or independent monitoring of the RTD sensors could req...

Страница 21: ...battery from maintaining its air tight seal If any wear is apparent which has not compromised the case inspect the battery area of the aircraft for any signs of improper installation C Visually inspect the power terminals and Communication connector Verify that no connectors are loose and there are no signs of damage wear or corrosion D If any of the above conditions are present the unit must be e...

Страница 22: ...rn to Service A Recharge the unit per section 5 2 2 B Measure and verify that the voltage on the unit s power terminals is greater than 27 6 VDC A unit shall never be returned to service if the voltage is less than this value C Re install the unit in the aircraft including securing it via proper hold downs mating the electrical connections and verifying proper vent attachment D Record service acti...

Страница 23: ...ned periods of time is possible but may increase the self discharge rate or result in some permanent loss of capacity Storage temperatures above 50ºC 122 F are to be avoided 5 5 END OF LIFE Estimated life for the TB17 Advanced Lithium ion Battery is expected to exceed six 6 years The unit has reliably demonstrated over 13 000 engine starts and subsequent charge cycles The cells themselves are desi...

Страница 24: ...otorcraft Category U Curve G Explosion 9 Category H Waterproofness 10 Category W Fluids 11 Category F Sand and Dust 12 Category S Fungus 13 Category F Salt Fog 14 Category S Magnetic Effect 15 Category Z Power Input 16 Category B RI Voltage Spike 17 Category A Audio Freq Conducted Susceptibility 18 Category B Induced Signal Susceptibility 19 Category ZC Radio Frequency Susceptibility 20 Category R...

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