Peregrine Systems TXA201 Скачать руководство пользователя страница 6

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Peregrine – Proprietary Data

Document No.

Title

Page

E-TX-21-0014 Rev IR Installation Manual, TXA201 Triaxial Accelerometer

Location

The accelerometer should be mounted within 12 feet longitudinally and 6 feet laterally of

the aircraft center of gravity to avoid erroneous readings due to aircraft rotational

maneuvers.

Weight: 10 Oz.

Center of Gravity: See Figure 3 below

Dimensions

Figure 2: TXA201 Dimensions

Содержание TXA201

Страница 1: ...SION STATUS Rev Description Approved Date IR Initial Release T Bailey 7 7 22 Export Control Notice The technical data contained herein is controlled under the U S Export Administration Regulations EAR...

Страница 2: ...N 8 3 1 TSO 8 3 2 Application 8 3 3 Environmental 8 3 4 Installation Approval 9 4 TESTING 9 4 1 Fault Indication 9 4 2 Pre Installation Check 9 4 3 Functional Test Procedure 9 4 4 Post Installation Ch...

Страница 3: ...Center of Gravity DC Direct Current DO Document Order EQ Equipment Qualification ESD Electro Static Discharge FAA Federal Aviation Administration FDR Flight Data Recorder FSO Full Scale Offset MDL Mas...

Страница 4: ...designed to meet ARINC 542A mounting specifications and is sealed to prevent moisture incursion This accelerometer may be utilized as an input to flight data recorder FDR systems such as the Curtiss...

Страница 5: ...to the accelerometer prior to delivery The placard includes a serial number of the format 0000 with the serial number of the first unit being 1001 The placard also serves as an anti tamper device The...

Страница 6: ...ial Accelerometer 6 Location The accelerometer should be mounted within 12 feet longitudinally and 6 feet laterally of the aircraft center of gravity to avoid erroneous readings due to aircraft rotati...

Страница 7: ...5000mV DOWN 3g 200mV FWD 1g 5000mV AFT 1g 200mV RIGHT 1g 5000mV LEFT 1g 200mV Axial Null VERTICAL 1800 mV LONGITUDINAL 2600 mV LATERAL 2600 mV Excitation 18 TO 32 VDC 28 VDC nominal Supply Current 30...

Страница 8: ...tested to Category B Vibration 8 0 Equipment tested to Category S and H aircraft zone 1 for fixed wing aircraft fuselage using vibration test curves C3 and R Explosive Atmosphere 9 0 Equipment identi...

Страница 9: ...rformed using the following procedure Requirements 28VDC Power Supply DC Voltmeter Tooling fixtures or other items that will allow the accelerometer to be rested on each of its six faces in a flat and...

Страница 10: ...a is properly received and is within expected parameters Table 2 Test Orientations and Outputs Axis Orientation Position Arrow UP Gravity Output and Range Vertical 3 0g Pin C 1 800 0036 VDC 1 1g Pin C...

Страница 11: ...and a cotton cloth or swabs A soft bristled brush may also be used 5 3 Repair The TXA201 Accelerometer contains no user serviceable parts and is not designed to be adjusted or repaired by field person...