@Turan09
I image translated these so it might be rough but you can probably analyze information given.
Design of the building of the selection of jet engines and supply of test platforms
Achievement
Annual achievement
Total
100%
100%
History
05/10/2017
10/2019
Expiry date
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clerk
E is the management of
The main objectives of this project are:. Establish and improve the performance of logistics centers. • Increasing the percentage of local content in non-oil sectors. • Facilitate doing business (from an organizational point of view)
Particular). | . Transfer and localization of the technology of building designs and testing of engines
The jet.
. performance
The project is a structural design of jet engines with the processing, supply and installation of its test platforms, to reach the test building and analysis of the overall performance of all turboprop engines, by national cadres trained and qualified in cooperation with the Brazilian company Turbo Machine to contribute to the achievement of the objectives of the "Vision Saudi Arabia 2030" . The test engine building consists of two test platforms with a double control room, where the building is designed with modern specifications with soundproof walls to reduce the noise level to the lowest level within the perimeter of the building, and the control room is equipped with full digital touch screens and connected to 60 channels high-speed To transfer data from the test platform to the displays, in addition it is equipped with double and bulletproof windows. Note that this building will be located in the research station of King Abdulaziz City for Science and Technology in the eye and a total area of 10,000 square meters.
Highlights:. Finished designs and blueprints needed to set up a test building
Fully jet engines. • Receive all components (control system and data collection units)
Sensors, connectors, displays) test building.
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1: 40 pm Mon ۲۱ October
C ۱۱%
,
Achievement
Annual achievement
Total
100%
80%
01/01/2017
08/07/2019
\ History
starting date
Finished
High air pressure rate up to (2
. 3:
1) At each stage, instead of (1
. 6: 1) in normal air compressor. It is worth mentioning that the project has been implemented at all stages by trained and qualified national cadres in cooperation with the Brazilian company Turbo Machine, in order to contribute to the achievement of the objectives of the vision of Saudi Arabia
2030
The project is a research, development and manufacture of turboprop engine
TKF - 500 Turbofan) has a Tandem Blades Compressor and a low fuel consumption (SFC). This engine can be used in several applications, such as: private aircraft, small personal aircraft, drones, guided missiles. The engine has been carefully selected for its advanced technical specifications
. 35
The total weight (96 kN)
The engine speed reaches 0. 9 times the speed of sound, where the maximum number of engine cycles to (27000)
rpm). The dimensions of the engine are (1005 mm), and the outer diameter (360)
mm). | The project also includes two different types of air compressors: Type I: Conventional Axial Compressor Type II: Tandem Blades Axial Compressor Compressor.
The project aims to. Study, design and manufacture of turbo-type engines
Fan), especially those with a dual pneumatic compressor
Tandem Blades Compressor. . Training and qualifying national cadres of engineers and technicians to become
Specialists in the field of jet engines. • Increasing the percentage of local content in non-oil sectors. • Transfer and localization of jet engine technology to build national potential.
Highlights: The completion of the manufacture of all components and parts of the first industrial model of the turbocharged engine
TKF - 500 Turbofan.
29
King Abdulaziz City for Science and Technology
The intellectual property is also apparently 100% Saudi
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VISION 203O
Turbofan engine
Kingdom of Saudi Arabia
TKF-500
Developed and lost in conjunction with the company TurboMachine Brazil
Intellectual property rights are fully Saudi
Patented for blade axial compressor technology
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Technical characteristics of the 500-TRF turbocharged engine
2030
Kingdom of Saudi Arabia
It has a maximum thrust of 545 kg
It is characterized by the technology of axial compressors synonymous with blades
Turbofan
Single shaft The maximum engine speed is mach 0.95
Works in all difficult and in operational conditions
Temperatures between (-40 to 55) degrees Celsius
It features a combination of hot gases with cool air
Integrated Digital Engine Control (FADEC)
Low fuel consumption of 380 kg / h at top speed