PITCH AND FOLD MECHANISM FOR A TILTABLE ROTOR USABLE IN AN AIRCRAFT CAPABLE OF HELICOPTER AND PROPELLER MODES OF OPERATION

• 1. 用于围壳转子、特别是直升机转子的可变俯仰转子桨叶 [P] . 中国专利： CN1298588C . 2007.02.07
• 2. 用于围壳转子、特别是直升机转子的可变俯仰转子桨叶 [P] . 中国专利： CN1572654A . 2005-02-02
• 3. PITCH AND FOLD MECHANISM FOR A TILTABLE ROTOR USABLE IN AN AIRCRAFT CAPABLE OF HELICOPTER AND PROPELLER MODES OF OPERATION [P] . CA870454A . 1971-05-11

  机译： 可在直升机和螺旋桨工作模式的飞机上使用的可倾斜转子的俯仰和折叠机构

• 4. PITCH AND FOLD MECHANISM FOR A TILTABLE ROTOR USABLE IN AN AIRCRAFT CAPABLE OF HELICOPTER AND PROPELLER MODES OF OPERATION [P] . 法国专利： FR1602500A . 1970-11-30

  机译： 可在直升机和螺旋桨工作模式的飞机上使用的可倾斜转子的俯仰和折叠机构

• 5. PITCH AND FOLD MECHANISM FOR A TILTABLE ROTOR USABLE IN AN AIRCRAFT CAPABLE OF HELICOPTER AND PROPELLER MODES OF OPERATION [P] . 美国专利： US3528630A . 1970-09-15

  机译： 可在直升机和螺旋桨工作模式的飞机上使用的可倾斜转子的俯仰和折叠机构

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