I was looking for a secret black projet and I found this one.
It is a stealth swing-wing aircraft with variable wing geometry developed by both Northrop and Grumman before they merged together. It has all
advantages of forward swept wing but has also the speed and range of normal wing.
"It is a bomber, a fighter, and a high-speed plane all in one. It accomplishes this by using a unique swing-wing design. The wings are attached to
its fuselage (body) at a pivot point toward the back of the plane. When the wings are fully extended, the plane can fly slowly to drop bombs precisely
on their targets or land on short runways. When the wings are swept farther forward, the aircraft takes advantage of the maneuverability that
forward-swept wings offer, and becomes an agile fighter. When the wings are swept fully forward, the trailing edge of the wing becomes the leading
edge, and the aircraft turns into a delta shape perfect for dashing away at speeds up to Mach 3."
In this configuration the plane can fly very low to precisely droping the bombs at its targets.
With its wings swept farther forward, the aircraft becomes extremely maneuverable for AA combat
When the wings are swept fully forward, the trailing edge of the wing becomes the leading edge, and the Switchblade can dash away at speeds up to Mach
3.
That means, the Switchblade can carry out multiple missions just by reconfiguring itself in flight.
The Switchblade is going to replace the F-111 fighter-bomber, which was permanently retired in 1995. The F-111 was a medium-sized bomber that could
defend itself like a fighter and speed away at more than 1600 miles an hour.
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In November 1999, the Switchblade was patented by the Northrop Grumman Corporation: U.S. Patent 5,984,231. It states, "An aircraft with a variable
forward-sweep wing and the method of configuring the wing in an optimal position for a desired flight regime. The variable forward-sweep wing is
positionable from an essentially unswept position to a full-forward sweep position. In the unswept position the wing is approximately orthogonal to a
fuselage centerline, while in the full-forward sweep position the wing has approximately a delta wing planform[platform]. Moreover, as the wing
position changes from the unswept position to the full-forward sweep position the trailing edge becomes the leading edge. In addition, the
aforementioned apparatus may be used in a method to configure the aircraft for flight in a desired flight regime. This method includes moving the wing
to an optimal position for the desired flight regime."
Patent drawings
More pics :
Sources :
area51
air attack
popular mechanics
[edit on 5-9-2004 by longbow]
[edit on 5-9-2004 by longbow]