Published July 1, 2018 | Version v1
Journal article

Design of electro-mechanical actuator for medium sized helicopter and a test platform for its testing and verification

  • 1. Singidunum University, Danijelova 32, Belgrade (Serbia)
  • 2. University of Belgrade, Faculty of Mechanical Engineering, Kraljice Marije 16, Belgrade (Serbia)

Description

This paper presents the design of an electro-mechanical actuator that is used for actuation of a medium sized helicopter. The designed actuator consists of a commercially available electro-mechanical cylinder EMC40 from Rexroth Bosch and a brushless DC motor EC45 from maxon motor. Cylinder and the motor are connected by a custom-made gearbox, which allows for their parallel axial mount. In addition to the actuator, the paper describes a test platform that can be used to emulate the forces generated by an actual helicopter. Designed test platform consists of a torsional spring and an AC motor with excentre. Frequency regulator is used to achieve the desired frequency of the force. Experimental results obtained by testing the designed actuator on the test platform are also given in the paper. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/393/1/012008

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
393
Journal Issue
1
Journal Page Range
[7 p.]
ISSN
1757-899X

Conference

Title
10. International Symposium Machine and Industrial Design in Mechanical Engineering
Acronym
KOD 2018
Dates
6-8 Jun 2018
Place
Novi Sad (Serbia)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52094336
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
ACTUATORS; CYLINDERS; DESIGN; HELICOPTERS; MOTORS; SPRINGS; TESTING; VERIFICATION
Descriptors DEC
AIRCRAFT; ENGINES; MACHINE PARTS