초록 ▼

A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A central rod is disposed within the barrel. The central rod is configured to rotate with respect to the bar

A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A central rod is disposed within the barrel. The central rod is configured to rotate with respect to the barrel. A roll control input is connected to the central rod. The roll control input is configured to cause the central rod to rotate within the barrel. Output control rods are connected to the central rod. The output control rods are connected to at least one control surface of the aircraft. An air brake input is connected to the barrel. The air brake input is configured to cause the barrel to rotate about the axle to move at least one of the output control rods.

대표청구항 ▼

1. An aircraft, comprising: a mechanical control mixer coupled to the aircraft, the mechanical control mixer including: an axle mounted to a frame of the mechanical control mixer,a barrel configured to rotate about the axle, anda central rod disposed within the barrel, the central rod being configur

1. An aircraft, comprising: a mechanical control mixer coupled to the aircraft, the mechanical control mixer including: an axle mounted to a frame of the mechanical control mixer,a barrel configured to rotate about the axle, anda central rod disposed within the barrel, the central rod being configured to rotate with respect to the barrel;a roll control input connected to the central rod, the roll control input being configured to cause the central rod to rotate within the barrel;output control rods connected to the central rod, the output control rods being connected to at least one control surface of the aircraft; andan air brake input connected to the barrel, the air brake input being configured to cause the barrel to rotate about the axle to move at least one of the output control rods. 2. The aircraft of claim 1, wherein the air brake input is configured to move between a number of distinct positions. 3. The aircraft of claim 1, wherein the air brake input is configured to selectively deploy at least one flap of the aircraft. 4. The aircraft of claim 3, wherein an amount of flap deployment is determined by a position of the air brake input. 5. The aircraft of claim 1, wherein the air brake input is configured to cause the barrel to rotate about the axle to move at least two output control rods by an approximately equal distance. 6. The aircraft of claim 1, wherein at least one of the output control rods comprises a collapsible control rod. 7. A mechanical control mixer, comprising: a barrel connected to the mechanical control mixer, the barrel being configured to rotate within the mechanical control mixer in response to an air brake input; anda central rod disposed within the barrel, the central rod being configured to rotate within the barrel in response to a roll control input to control a position of at least one control surface of an aircraft. 8. The mechanical control mixer of claim 7, wherein the central rod is configured to connect to output control rods, the output control rods being connected to at least one control surface of the aircraft. 9. The mechanical control mixer of claim 8, wherein at least one of the output control rods comprises a collapsible control rod. 10. The mechanical control mixer of claim 8, wherein rotation of the barrel within the mechanical control mixer causes a force to be applied to the output control rods. 11. The mechanical control mixer of claim 7, wherein the air brake input is configured to move between a number of distinct positions. 12. The mechanical control mixer of claim 7, wherein the air brake input is configured to selectively deploy at least one flap of an aircraft. 13. The mechanical control mixer of claim 12, wherein an amount of deployment of the flap is determined by a position of the air brake input.