VIBRATECH
AUTHORIZED Honeywell HUMS and SATCOM Systems DISTRIBUTOR
Through the master distributor DSI
Information link:
Honeywell to DSI agreements
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AIRVIB® SYSTEM MANUFACTURER
WIRELESS BALANCING SYSTEM
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
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 |
2/1 |
Receive/Transmit |
Version imprimable 