Northrop/Grumman Switchblade aircraft, page 1

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]

Originally posted by longbow

Originally posted by cimmeriusThis is very innovative. Extremely clever. But it would seem that the wing cross-section geometry would be tricky, providing lift in forward and backward configuration. Where are the control surfaces? OK I can see them in the drawing. But how would they work when the wing is swept forward?

There is no need for much lift when the wing are folded because the aircraft is traveling very fast (Mach 3) - so it's the tiny leading edges (previously trailing) are creating more than enough lift (and have also lover drag).

Actually aircraft's body would produce much of its lift.
(one kind of "lifting body" is already used in planes like F-14)

And why the hell you need control surfaces?
www.globalsecurity.org...

And I remember reading somewhere that even movable nozzles could be eliminated using injection of high pressure air to deflect/control engine exhaust... which would make engine nozzles much simpler, lighter and magnitude stealthier.

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