Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission
Abstract
One of the persistent challenges in helicopter design is the mitigation of vibration originating from transmission systems, where gear housings play a critical role in both structural integrity and dynamic response. Although numerous approaches have been investigated for vibration reduction, limited attention has been given to the use of Triply Periodic Minimal Surface (TPMS)-based lattice structures in aerospace transmission applications. Addressing this gap, the present study evaluates the vibration and structural performance of gear housings designed with Gyroid, Diamond, and Schwarz topologies. The housings were fabricated using additive manufacturing techniques, and their dynamic behavior was experimentally assessed on a custom-designed test rig. Vibration signals acquired from accelerometer sensors were processed through FFT, RMS, and envelope analysis methods. Complementary to the experimental campaign, finite element analysis was employed to investigate stress distributions across the geometries. The results demonstrated that the Gyroid structure provided the most favorable dynamic response, yielding the lowest RMS value along the Z-axis (2.61 m/s²), while the Schwarz structure exhibited the lowest stress value (3.46 MPa). Overall, the findings highlight that TPMS-based lattice housings have the potential to attenuate vibration propagation through their multi-layered cellular topology while maintaining adequate structural strength. This suggests that such geometries may serve as promising alternatives to conventional solid gear housings in helicopter transmission systems, thereby contributing to both weight reduction and vibration control in aerospace applications.
Keywords
References
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Details
Primary Language
English
Subjects
Dynamics, Vibration and Vibration Control
Journal Section
Research Article
Publication Date
December 31, 2025
Submission Date
November 21, 2024
Acceptance Date
October 18, 2025
Published in Issue
Year 2025 Volume: 11 Number: 3
APA
Sağlam, Y., & Gökçe, H. (2025). Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission. Gazi Journal of Engineering Sciences, 11(3), 465-480. https://izlik.org/JA88GC28EN
AMA
1.Sağlam Y, Gökçe H. Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission. GJES. 2025;11(3):465-480. https://izlik.org/JA88GC28EN
Chicago
Sağlam, Yusuf, and Harun Gökçe. 2025. “Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission”. Gazi Journal of Engineering Sciences 11 (3): 465-80. https://izlik.org/JA88GC28EN.
EndNote
Sağlam Y, Gökçe H (December 1, 2025) Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission. Gazi Journal of Engineering Sciences 11 3 465–480.
IEEE
[1]Y. Sağlam and H. Gökçe, “Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission”, GJES, vol. 11, no. 3, pp. 465–480, Dec. 2025, [Online]. Available: https://izlik.org/JA88GC28EN
ISNAD
Sağlam, Yusuf - Gökçe, Harun. “Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission”. Gazi Journal of Engineering Sciences 11/3 (December 1, 2025): 465-480. https://izlik.org/JA88GC28EN.
JAMA
1.Sağlam Y, Gökçe H. Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission. GJES. 2025;11:465–480.
MLA
Sağlam, Yusuf, and Harun Gökçe. “Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission”. Gazi Journal of Engineering Sciences, vol. 11, no. 3, Dec. 2025, pp. 465-80, https://izlik.org/JA88GC28EN.
Vancouver
1.Yusuf Sağlam, Harun Gökçe. Examination of Vibration Behaviors of Lattice Structures in Helicopter Transmission. GJES [Internet]. 2025 Dec. 1;11(3):465-80. Available from: https://izlik.org/JA88GC28EN
