| Literature DB >> 34947304 |
Robert Kasner1, Patrycja Bałdowska-Witos1.
Abstract
The aim of this article was to complete a methodologically original study and evaluation of the technological readiness of an innovative ribbon-blade wind turbine in accordance with NASA's TRL method. The structural form of the wind turbine unit analyzed herein, featuring a new ribbon turbine design, is distinguished by its safe durability. The circumferential speeds of the points on the turbine circumference were technologically verified positively and have a significant impact on the evaluation indicators of the conversion process, these being efficiency, unit energy consumption, and the quality of the power and energy of the wind power plant. The use of a new turbine design in the wind turbine analyzed herein, a working ribbon unit, resulted in a technological increase in efficiency from 13% to 32% and a reduction in unit internal energy consumption from 18% to 36% compared to the traditional wind turbine design. The TRL NASA-based evaluation herein, which consists of modern computer-aided engineering procedures (CAE standard) as well as IT instrumentation, and which includes nine degrees of technological readiness of an innovative ribbon windmill, falls in line with the standards for smart development based on knowledge and innovation (EU 2020 Strategy).Entities:
Keywords: innovative wind ribbon turbine; verification of the method of assessing the level of innovation readiness
Year: 2021 PMID: 34947304 PMCID: PMC8708914 DOI: 10.3390/ma14247709
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Readiness levels in accordance with the TRL method [1].
| TRL Level | Characteristics |
|---|---|
| TRL 1 | Identifying basic operating principles |
| TRL 2 | Formulating technology concept |
| TRL 3 | Proof-of-concept via experimentation |
| TRL 4 | Validating the technology in laboratory conditions |
| TRL 5 | Validating the technology in relevant environment |
| TRL 6 | Prototype demonstration in simulated environment similar to the target one |
| TRL 7 | Prototype demonstration in the target environment |
| TRL 8 | Producing the final version of the product |
| TRL 9 | Completing a test series and obtaining product conformity certificates and approvals for use |
Figure 1Construction of the rotor: geometrical shape with dimensions: 1. Main sleeve, 2. Fastening the web, 3. Main sleeve flange, 4. Flange movable sleeve, 5. Movable sleeve, 6. Front cover, and 7. Side cover. Source: own materials.
Conclusion, assessment result of TRL level 1.
| TRL 1 | Identifying basic operating principles | Positive assessment of mechanical operating principles |
Using the PN-EN 1991–1-4:2008 norm, we can define the pressure of the wind speed with the following formula.
| Dependence | Description | |
|---|---|---|
|
| (1) | where: |
| After calculating the pressure of the wind speed we can calculate the characteristic load caused by wind effects with the following formula: | ||
| (2) | where: | |
| The design load applied when determining the ultimate limit states of the construction are derived from the formula: | ||
| (3) | where: | |
| After determining the design load and surface area designated from the rotor’s ribbon we can compute the force applied to the relevant surface. The calculated force will be directed perpendicular to the surface from the calculations. This force can be derived from the following formula: | ||
| (4) | where: | |
| Knowing the resultant force on the unit area of the blade we can calculate the circumferential force needed to define the power of the turbine. To this end, we will use the following formula: | ||
| (5) | where: | |
| The next step is to calculate the rotor power for different rotational speeds, which will be determined on the basis of wind speed variation. First, we derive the rotor speed from the formula: | ||
| (6) | where: | |
| Next we may proceed to calculate the theoretical power of the rotor: | ||
| (7) | where: | |
| Finally, when taking the assumed efficiency of the system into account, the power output will be calculated: | ||
|
| (8) | where: |
Conclusion, assessment result of TRL level 2.
| TRL 2 | Formulating the solution concept | Positive assessment of the mechanical concept of the solution |
Figure 2The manufacturing model of the rotor with ribbon blades. Source: the authors’ own materials.
Figure 3(a) von Mises stresses of the rotor; (b) displacement of the loaded rotor planes. Source: the authors’ own materials.
Conclusion, assessment result of TRL level 3.
| TRL 3 | Validating the proof-of-concept experimentally | Positive assessment, concept experimentally valid |
Material properties of steel AISI 304.
| The Chemical Composition of Steel AISI 304 | ||||||||
|---|---|---|---|---|---|---|---|---|
| Element | Iron | Chrome | Nickel | Manganese | Silicon | Coal | Potassium | Sulfur |
| Participation, % | 66–74 | 18–20 | 8–10.5 | Max 2 | Max 1 | 0.08 | 0.045 | 0.03 |
| Properties of steel AISI 304 | ||||||||
| Properties | The value of the metric unit | |||||||
| Density | 7.9 × 103 | kg·m−3 | ||||||
| Modulus of elasticity | 193 | GPa | ||||||
| Thermal expansion (20 °C) | 17.2 × 10−6 | °C −1 | ||||||
| Specific heat capacity | 502 | J·(kg·K)−1 | ||||||
| Thermal conductivity | 16.2 | W· (m·K) −1 | ||||||
| Electrical resistance | 7.2 × 10−7 | Ohm·m | ||||||
| Tensile strength | 520 | MPa | ||||||
| Yield point | 210 | MPa | ||||||
| Elongation | 45 | % | ||||||
| Hardness | <215 | HB | ||||||
| Melting temperature | 1400–1450 | °C | ||||||
Figure 4(a) distribution of first principal stresses on the ribbon surfaces; (b) distribution of the safety coefficient on the ribbon surfaces. Source: the authors’ own materials (based on M.M. Szarek).
Conclusion, assessment result of TRL levels 4 and 5.
| TRL 4 | Validating the technology in laboratory conditions | Positive assessment, elements of technology verified in laboratory conditions |
| TRL 5 | Validating the technology in simulated operational conditions | Positive assessment in laboratory conditions as simulated operational conditions |
Figure 5The real object with a list of components and materials for LCA.
Figure 6(a) Validation of the ribbon rotor manufacturing technology; (b) Results of the analysis and evaluation of the manufacture and disposal of rotor materials using the LCA procedure.
Results of the assessment of environmental emissions of innovative wind farms.
| Wind Power Plant | Global Warming (GWP100), kg CO2 eq | Renewable Wind Energy, MJ |
|---|---|---|
| Double Bladed | 70.2 | 3.76 |
| Three Bladed | 77.8 | 4.7 |
| Four bladed | 93.3 | 5.64 |
| Five Bladed | 109 | 6.58 |
| Six Bladed | 124 | 7.52 |
Figure 7Wind power plant of a modernized ribbon-blade wind turbine under real conditions. Source: the authors’ own materials (based on R. Kasner).
Figure 8Geodetic inventory of wind turbine test stations: (1) wind power research positions; (2) environmental parameters measurement station; (3) telecommunication sewage system for monitoring. Source: the authors’ own materials (based on R. Kasner).
Figure 9The completed tube construction of the wind turbine tower (1) and wind measurement stations (2). Source: the authors’ own materials (based on R. Kasner).
Figure 10Assembly of the wind turbines at the testing station (a) the testing station of the wind turbines (b). Source: the authors’ own materials (based on R. Kasner).
Figure 11Installation monitoring and verifying the environmental parameters of the performance of a modernized ribbon-blade wind turbine. The installation verifying the environmental parameters of the modernized ribbon wind turbine is the end of the telecommunication sewage system monitoring (point 3—Figure 8). Source: the authors’ own materials (based on R. Kasner).
Conclusion, assessment result of TRL levels 6 and 7.
| TRL 6 | Production and demonstration of a prototype in a simulated environment similar to the target one | Assessment positive, prototype produced by professional wind turbine producer |
| TRL 7 | Demonstration of the prototype in target operational conditions | Assessment positive, Prototype demonstrated in the target conditions of a laboratory |
Summary of wind speed pressure distribution and ribbon-blade surface area. Source: the authors’ own materials.
| Lp. | Area | Speed | Wind Speed Pressure | Characteristic Load | Design Load |
|---|---|---|---|---|---|
| 1 | 0.105481 | 6 | 22 | 40 | 52 |
| 2 | 0.118495 | 12 | 89 | 159 | 207 |
| 3 | 0.105481 | 18 | 199 | 359 | 466 |
| 4 | 0.118495 | 24 | 354 | 638 | 829 |
| 5 | 0.105481 | 29 * | 517 | 931 | 1210 |
| 6 | 0.118495 | 35 | 753 | 1356 | 1763 |
| 7 | 0.105481 | 41 | 1034 | 1861 | 2419 |
| 8 | 0.118495 | 47 | 1359 | 2445 | 3179 |
* marks the beginning of critical speeds and dangerous winds.
Summary of the distribution of theoretical forces on the surface of the ribbon blades as well as the rotational speed and theoretical power on the rotor that were obtained. Source: the authors’ own materials.
| Lp. | Speed | Resultant Force | Circumferential Force | Revolutions | Theoretical Power |
|---|---|---|---|---|---|
| 1 | 6 | 46 | 33 | 21 | 0.08 |
| 2 | 12 | 186 | 131 | 41 | 0.63 |
| 3 | 18 | 418 | 295 | 62 | 2.13 |
| 4 | 24 | 743 | 525 | 83 | 5.04 |
| 5 | 29 * | 1084 | 767 | 100 | 8.89 |
| 6 | 35 | 1579 | 1117 | 121 | 15.63 |
| 7 | 41 | 2167 | 1533 | 141 | 25.13 |
| 8 | 47 | 2848 | 2014 | 162 | 37.86 |
* marks the beginning of critical speeds and dangerous winds.
Summary of the distribution of the effective forces on the surface of the ribbon blades and the rotational speeds and effective power on the rotor. Source: the authors’ own materials.
| Lp. | Speed | Circumferential Force | Revolutions | Theoretical Power |
|---|---|---|---|---|
| 1 | 6 | 26 | 21 | 0.06 |
| 2 | 12 | 105 | 41 | 0.50 |
| 3 | 18 | 236 | 62 | 1.70 |
| 4 | 24 | 420 | 83 | 4.03 |
| 5 | 29 * | 613 | 100 | 7.11 |
| 6 | 35 | 893 | 121 | 12.1 |
| 7 | 41 | 1226 | 141 | 20.1 |
| 8 | 47 | 1611 | 162 | 30.9 |
* marks the beginning of critical speeds and dangerous winds.
Figure 12(a) Theoretical power as a function of speed; (b) Effective power as a function of speed. Source: the authors’ own materials.
Conclusion, assessment result of TRL levels 8 and 9.
| TRL 8 | Producing the final version of the product | Assessment conditionally positive, a final version of the product was completed |
| TRL 9 | Completion of a test series and obtaining product conformity certificates and approvals for use | No assessment |
Levels and post-test readiness assessments in accordance with the TRL method.
| TRL Level | Characteristics | Evaluation |
|---|---|---|
| TRL 1 | Identifying basic operating principles | Positive, high |
| TRL 2 | Formulating the solution concept | Positive, high |
| TRL 3 | Validating the proof-of-concept experimentally | Positive, high |
| TRL 4 | Validating the technology in laboratory conditions | Positive, high |
| TRL 5 | Validating the technology in simulated operational conditions | Positive, high |
| TRL 6 | Production and demonstration of a prototype in a simulated environment similar to the target one | Positive, high |
| TRL 7 | Demonstration of the prototype in target operational conditions | Positive, high |
| TRL 8 | Producing the final version of the product | Assessment conditionally positive, a final version of the product was completed |
| TRL 9 | Completion of a test series and obtaining product conformity certificates and approvals for use | No assessment |