Govindaraju et al., 2026 - Google Patents
Thermal Management System in Commercial Aircraft: A Case Study on Passenger Egress SystemGovindaraju et al., 2026
- Document ID
- 3449697937804488129
- Author
- Govindaraju P
- Nanjundegowda H
- Publication year
- Publication venue
- AeroCON 2026 375443
External Links
Snippet
It is known fact that Thermal management systems are essential to the safety, operational efficiency, and structural integrity of present-day commercial aircraft. Very critical insulation and thermal protection materials are utilized across various aircraft zones to mitigate …
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies
- Y02T50/67—Relevant aircraft propulsion technologies
- Y02T50/671—Measures to reduce the propulsor weight
- Y02T50/672—Measures to reduce the propulsor weight using composites
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP3732126B2 (en) | Thermal defense structure | |
| EP2447508B1 (en) | Fireproof systems in aircraft engines | |
| US8844643B2 (en) | Fireproof systems with local heat shields for aircraft engines | |
| US10974840B2 (en) | Heat shield for signature suppression system | |
| US20150175272A1 (en) | Reinforced primary structure for an attachment pylon | |
| US20120082808A1 (en) | Method for installing heat shielding on a fixed internal structure of a jet engine nacelle | |
| US10934028B2 (en) | In-situ passivation and insulation layer for a flexible thermal protection system (FTPS) | |
| CA3068140A1 (en) | Acoustic structure for gas turbine engine | |
| Govindaraju et al. | Thermal Management System in Commercial Aircraft: A Case Study on Passenger Egress System | |
| Kozomara et al. | Experimental investigation of UAS rotors and ice protection systems in appendix C icing conditions | |
| Chávez et al. | Evaluation of the fire resistance of protected carbon/epoxy laminates in small-scale experiments | |
| US4431697A (en) | Laser hardened missile casing structure | |
| US9556370B2 (en) | Optimized heat-protection material | |
| US8236413B2 (en) | Combination structural support and thermal protection system | |
| Liu et al. | Improve heat resistance of composite engine cowlings using ceramic coating materials, experimental design and testing | |
| Mohammed | A Review of New Composite Materials for Thermal Protection in an Aero-Engine Application | |
| Guntumadugu et al. | Properties and Application of Ablative Material | |
| Mooij | Thermal Protection Systems | |
| Tsukahara et al. | Advanced thermal protection systems for reusable launch vehicles | |
| Keller et al. | Smart thermal protection systems | |
| RU2771553C1 (en) | Complex heat-protective coating of metal structures of the airframe of high-speed aerial vehicles | |
| US6486233B1 (en) | Ablator composition | |
| Trushlyakov et al. | On the issue of selecting burned materials in rocket vehicle designs | |
| US20260108911A1 (en) | Intumescent directed energy protection | |
| Huang et al. | The inverse problem in zero linear ablation of aluminizing carbon composites under high heat flux |