Door for a tiltrotor proprotor pylon
An embodiment of the present invention provides a blocking door that is pivotally disposed on a fixed nacelle of a tiltrotor aircraft for pivoting between a stowed position when a proprotor pylon is in the substantially horizontal position and a protective blocking position in front of the proprotor pylon when the proprotor pylon is positioned in the non-horizontal position. In other aspects, there is provided a blocking door and a method of reducing infrared and/or radar signatures of rotorcraft with a rotatable proprotor.
1. An aircraft, comprising:
a fixed nacelle disposed on a wing of the aircraft,
a proprotor pylon disposed on the wing and rotatable relative to the fixed nacelle between a substantially horizontal position and a vertical position;
a channel with a channel floor disposed at the leading edge of the fixed nacelle that receives the proprotor pylon therein, when the proprotor pylon being arranged to rotate about an axis in the channel to the substantially horizontal position, wherein the proprotor pylon is adjacent to the channel floor and occupies the channel; and to the vertical position, wherein at least a portion of the channel is exposed; and
a blocking door pivotally disposed in the channel for pivoting between a stowed position where the blocking door is disposed on the channel floor when the proprotor pylon is in the substantially horizontal position and a blocking position that is anterior to the proprotor pylon when the proprotor pylon is positioned in the vertical position.
2. The aircraft of claim 1 , further including a linkage connected between the blocking door and the proprotor pylon, the linkage configured such that rotation of the proprotor pylon rotates the blocking door.
3. The aircraft of claim 1 , further including an actuator coupled to the blocking door and operable to rotate the blocking door.
4. The aircraft of claim 1 , wherein the blocking door includes a pivot member that is disposed on the fixed nacelle, the pivot member is anterior to the proprotor pylon when the proprotor pylon is positioned in the vertical position.
5. The aircraft of claim 4 , wherein the pivot member is a shaft.
6. The aircraft of claim 1 , wherein the blocking door is comprised of at least one of the following materials: a ceramic material, a composite material, a metallic material, or an armored material.
7. The aircraft of claim 1 , wherein the blocking door has a flat front surface.
8. The aircraft of claim 7 , wherein the blocking door further includes a first side and a second side disposed at opposite side edges of the flat front surface.
9. The aircraft of claim 1 , wherein the blocking door in the blocking position reduces at least one of the following: an infrared signature of the aircraft and a radar signature of the aircraft.
10. A method of reducing infrared and/or radar signatures of rotorcraft with a rotatable proprotor pylon received in a channel with a channel floor at a leading edge of a fixed nacelle disposed on a wing of the rotorcraft, the method comprising:
rotating a blocking door in the channel to a blocking position in front of exposed components when the proprotor pylon has been rotated relative to the fixed nacelle to a non-horizontal position in a conversion mode or a helicopter mode of operation; and
rotating the blocking door to a stowed position where the blocking door is disposed on the channel floor when the proprotor pylon is in the substantially horizontal position.
11. The method of claim 10 , wherein the blocking door is rotated to the blocking position by linking the blocking door to the proprotor pylon for rotation with the proprotor pylon.
12. The method of claim 10 , wherein the blocking door is rotated to the blocking position by an independent actuator.
13. The method of claim 10 , wherein the blocking door is made of a material comprised of at least one of the following: a ceramic material, a composite material, a metallic material, or an armored material.