Thermal Protection Modular Design for High-Speed Aircraft Engines and Optimization Based on Design of Experiments.
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| Title: | Thermal Protection Modular Design for High-Speed Aircraft Engines and Optimization Based on Design of Experiments. |
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| Authors: | Pan, Guangyan1 (AUTHOR), Zhang, Chunlei1 (AUTHOR), Yu, Xiao1 (AUTHOR) yuxiao606@163.com |
| Source: | Energies (19961073). Apr2026, Vol. 19 Issue 7, p1616. 16p. |
| Subject Terms: | *Modular design, *Experimental design, *Aerodynamic heating, *Temperature control, *Total quality management, *Hypersonic planes, *Airplane motors |
| Abstract: | High-altitude and high-speed aircraft generate substantial aerodynamic heat during flight, creating a harsh thermal environment in the engine compartment that risks overheating and burnout of control components and fuel and lubricating oil accessories. Consequently, the thermal protection system (TPS) design for engine accessories has become one of the key technologies in hypersonic vehicle design. Based on certain TBCC, this paper uses a modular active-passive integrated TPS design and employs the quality management experimental design tool to optimize the design and decouple the method proposed on the modular design boundaries. This paper is the first to combine modular design with design of experiments (DOE) tools and apply them to the TPS of high-altitude and high-speed combined power accessories. The design scheme is optimized by identifying the main influencing factors. The optimized TPS scheme decreases the performance loss by 10% and increases cooling efficiency by 22–26%. The proposed engineering method shortens the development cycle significantly and improves efficiency by 78%. The modular design method for accessory TPS provided in this paper has good engineering applicability and can be widely used in the early stages of thermal protection scheme design, scheme optimization, scheme selection, and overall thermal management of hypersonic combined power systems. [ABSTRACT FROM AUTHOR] |
| Database: | Energy & Power Source |
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| FullText | Links: – Type: pdflink Text: Availability: 1 |
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| Header | DbId: enr DbLabel: Energy & Power Source An: 192959020 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Thermal Protection Modular Design for High-Speed Aircraft Engines and Optimization Based on Design of Experiments. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Pan%2C+Guangyan%22">Pan, Guangyan</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Zhang%2C+Chunlei%22">Zhang, Chunlei</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Yu%2C+Xiao%22">Yu, Xiao</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> yuxiao606@163.com</i> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22Energies+%2819961073%29%22">Energies (19961073)</searchLink>. Apr2026, Vol. 19 Issue 7, p1616. 16p. – Name: Subject Label: Subject Terms Group: Su Data: *<searchLink fieldCode="DE" term="%22Modular+design%22">Modular design</searchLink><br />*<searchLink fieldCode="DE" term="%22Experimental+design%22">Experimental design</searchLink><br />*<searchLink fieldCode="DE" term="%22Aerodynamic+heating%22">Aerodynamic heating</searchLink><br />*<searchLink fieldCode="DE" term="%22Temperature+control%22">Temperature control</searchLink><br />*<searchLink fieldCode="DE" term="%22Total+quality+management%22">Total quality management</searchLink><br />*<searchLink fieldCode="DE" term="%22Hypersonic+planes%22">Hypersonic planes</searchLink><br />*<searchLink fieldCode="DE" term="%22Airplane+motors%22">Airplane motors</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: High-altitude and high-speed aircraft generate substantial aerodynamic heat during flight, creating a harsh thermal environment in the engine compartment that risks overheating and burnout of control components and fuel and lubricating oil accessories. Consequently, the thermal protection system (TPS) design for engine accessories has become one of the key technologies in hypersonic vehicle design. Based on certain TBCC, this paper uses a modular active-passive integrated TPS design and employs the quality management experimental design tool to optimize the design and decouple the method proposed on the modular design boundaries. This paper is the first to combine modular design with design of experiments (DOE) tools and apply them to the TPS of high-altitude and high-speed combined power accessories. The design scheme is optimized by identifying the main influencing factors. The optimized TPS scheme decreases the performance loss by 10% and increases cooling efficiency by 22–26%. The proposed engineering method shortens the development cycle significantly and improves efficiency by 78%. The modular design method for accessory TPS provided in this paper has good engineering applicability and can be widely used in the early stages of thermal protection scheme design, scheme optimization, scheme selection, and overall thermal management of hypersonic combined power systems. [ABSTRACT FROM AUTHOR] |
| PLink | https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=enr&AN=192959020 |
| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.3390/en19071616 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 16 StartPage: 1616 Subjects: – SubjectFull: Modular design Type: general – SubjectFull: Experimental design Type: general – SubjectFull: Aerodynamic heating Type: general – SubjectFull: Temperature control Type: general – SubjectFull: Total quality management Type: general – SubjectFull: Hypersonic planes Type: general – SubjectFull: Airplane motors Type: general Titles: – TitleFull: Thermal Protection Modular Design for High-Speed Aircraft Engines and Optimization Based on Design of Experiments. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Pan, Guangyan – PersonEntity: Name: NameFull: Zhang, Chunlei – PersonEntity: Name: NameFull: Yu, Xiao IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 04 Text: Apr2026 Type: published Y: 2026 Identifiers: – Type: issn-print Value: 19961073 Numbering: – Type: volume Value: 19 – Type: issue Value: 7 Titles: – TitleFull: Energies (19961073) Type: main |
| ResultId | 1 |
