Published May 28, 2012 | Version v1
Journal article

Design of Embedded Wireless Sensor and its Soft Encapsulation for Embedded Monitoring of Helicopter Planetary Gear Set

  • 1. Laboratory of Science and Technology on Integrated Logistics Support, College of Mechatronics Engineering and Automation, National University of Defense Technology, 109 Deya Rd., Changsha, 410073 (China)

Description

Planetary gear set, as an important part of helicopter, is with the characteristics of multi-point and time-varying position engagement. For the revolution of planetary gears round sun gear, directions of vibration and pulse created by tooth damage change continuously. If an accelerometer fixed on the surface of gearbox, the angle between the directions of pulse force and accelerometer sensitivity will change continuously, which will causes that the components of pulse force on the sensitivity direction vary with time and the features of damage are very difficult to extract from the signals. Aiming at this problem, a type of embedded wireless sensor node was designed firstly, which can be fixed on the carrier of planetary gear, and acquires the damage-related vibration signals in a fixed direction of pulse force. Then, to avoid the corrosion of electronic components by the lubrication oil in gearbox, the protect restrictions of the sensor node was investigated and a kind of soft encapsulation method is applied. Finally, real vibration signal is measured and transmitted by the designed and/or encapsulated sensor node. The experiments show that the sensor can measure vibration effectively.

Availability note (English)

Available from http://dx.doi.org/10.1088/1742-6596/364/1/012079

Additional details

Publishing Information

Journal Title
Journal of Physics. Conference Series (Online)
Journal Volume
364
Journal Issue
1
Journal Page Range
[7 p.]
ISSN
1742-6596

Conference

Title
25. International congress on condition monitoring and diagnostic engineering
Acronym
COMADEM 2012
Dates
18-20 Jun 2012
Place
Huddersfield (United Kingdom)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
43100362
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
ACCELEROMETERS; CORROSION; DAMAGE; DESIGN; ENCAPSULATION; FAILED ELEMENT DETECTION; GEARS; HELICOPTERS; LUBRICATION; MECHANICAL ENGINEERING; MONITORING; PULSES; SAFETY ENGINEERING; SENSITIVITY; SENSORS; SYSTEM FAILURE ANALYSIS
Descriptors DEC
AIRCRAFT; CHEMICAL REACTIONS; DETECTION; ENGINEERING; MACHINE PARTS; MEASURING INSTRUMENTS; SYSTEMS ANALYSIS