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/393/1/012008Additional details
Identifiers
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