1. Yuriy, G. Split torque gearbox for rotary wing aircraft with translational thrust system: US 7413142B2. 2008-08-19.
2. Ketel. M. Mechanical transmission of helicopters [M].[S.l.]:[s.n.], (1983).
3. Todd, A. G., & Mansfield, T. X. Torque split gearbox for rotary wing aircraft: US 2015/0060596A1. 2005-03-05.
4. Arthur E. P., Dwaine R. B., Elwood, G., et al. Ultralight coaxial rotor aircraft: US 7198223B2. 2007-04-03.
5. Scott, B., & David, W. B. Leveraging geometry optimization tools to reduce component weight, development cost, and design schedule. In Proceedings of AHS 72nd Annual Forum. [S.l.]: [s.n.] (2016).