VIBRATECH

AUTHORIZED Honeywell HUMS and SATCOM Systems DISTRIBUTOR 

Through the master distributor DSI 

Information link:

Honeywell to DSI agreements

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AIRVIB II® & AIRVIB® SYSTEMS MANUFACTURER

WIRED / WIRELESS BALANCING SYSTEMS

CONTACT US

Address in FRANCE

VIBRATECH
213 Avenue CASTILLON
83370 Saint Aygulf
FRANCE
Tel: +33 (0) 494 81 72 13
Fax: +33 (0) 494 81 72 59
Email:
contact(at)vibratech.fr

NEW Address in CHINA

VIBRATECH International

Medical Device Industrial Park

Office 535, Block A, 5th Floor,

Shekou - Nanshan District

Shenzhen 518067

People’s Republic of China

Intl.TEL/FAX: +86 755 2602 8817 

Local TEL/FAX:+86 755 2602 8817 

website: www.vibratech-intl.cn

Mail : contact(at)vibratech-intl.cn

 

维特振动科技(深圳)有限公司

深圳市南山区蛇口南海大道1019号南山医疗器械产业园A栋5层535号

政编码:518067

我们中国区办公室网站链接:www.vibratech-intl.cn

 

    

 

HUMS 1134

For Light Helicopters, Fixed-wing aircraft and turbine engines

    

Brochure 1134
Zing_HUMS_1100-1200-1400.pdf
Document Adobe Acrobat [1.4 MB]

 

 

Enregistrement de l'état de santé, surveillance et diagnostic.

Diagnostic avancé du groupe motopropulseur.
Plage dynamique supérieure à 100db.

Réglage du sillage et équilibrage du rotor.

Traitement avancé des événements et des enregistrements.
Reconnaissance des régimes de vol.
Surveillance de l'état de santé du moteur.
Programme de surveillance des opérations de l'hélicoptère. (HOMP / FDM / FOQA) et Système de Positionnement Global (GPS).
Interface de communication sans fil802.11.
Système inertiel intégré utilisant les capteurs MEMS et GPS.

Trois supports de processeurs intégrés partitionnés DO-178B pour l'évolution des fonctions et des systèmes logiciels.
Jusqu'à 8 Go de mémoire Compact Flash pour véhicule ou pour l'enregistrement de données de vol.

 

 

 

Health monitoring, diagnostics and recording.

Advanced drive train diagnostics.

Greater than 100db dynamic range.

Advanced rotor track and balance.

Event processing and recording.

Flight regime recognition.

Engine health monitoring.

Helicopter Operation Monitoring Program (HOMP/FDM/FOQA) support.

Global Positioning System (GPS).

802.11 wireless communication interface.

Integrated inertial system using MEMS and GPS sensors.

Three embedded processors support partitioned DO-178B software functions and systems growth.

Up to 8 Gbytes of compact flash (non-crash survivable) for vehicle or flight data recording.

 

 

•Dimensions:  7.62" X 4.88" X 1.75“ with mounting bracket

•Weight:  2.44 lbs
•Environmental:  MIL-STD-810F for aircraft environments,  DO-160D compliant
•EMI/RFI:  MIL-STD-461E
•Temperature range:  -41ºC – 71ºC
•Input Power:  +28 VDC standard to MIL-STD-704A/D (12-32 VDC operation)
•Power Consumption < 15W
•MTBF exceeds 45,989 hours per MIL-HDBK-217 ground benign
•Interconnection:  MIL 38999 connectors
•Enclosure: Light Weight Machined Aluminum

 

 CHANNEL TYPE QTY COMMENTS
Processors 1
2

533MHz Geode

450 MHz PowerPC 405

XtremeDSP  1 DSP processing in Virtex4 FPGA
RAM 1
2

256Mbyte SDRAM for GEODE Processor

128Mbyte SDRAM for PowerPCs

Flash Memory 1 Compact Flash IDE 128Mbyte to 8 Gbyte 
802.11 Wireless 1 (Optional through additional Module)
Accelerometer Channels 12 (24)

1.5 to 96kHz Bandwidth (8 simultaneous)

6 Charge Mode Interface

Tachometer Channels

 

4 (5) High Speed A/D based adaptive tachometer 
* 1additional tach using jumper selection
General Purpose Analog or Discrete 32(0) General purpose analog/discrete interface *Accels may be substituted using jumper selection 
Discrete Output 2 High current drive capability
Analog Output 8 Precision Output
Blade Tracker 1 Compatible with  iBT/E-UTD & FasTrak Blade Trackers
Firewire  1 *Either Blade Tracker or Fire Wire
Universal Serial Bus 1 1.1 compliant
CAN 1 *Either CAN bus or USB
MIL-STD-1553 1 Dual Redundant (Optional)
RS-232/485 2 9600 to 115kBaud
Ethernet 2 10/100 BaseT 
Inertial/GPS/Flash 1 Optional Card 
ARINC 429

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