Mobile aircraft launcher

• US 6,457,673 B1
• Filed: 08/16/2000
• Issued: 10/01/2002
• Est. Priority Date: 08/16/2000
• Status: Expired due to Term

• Current Assignee: AAI Corporation (Textron Inc)
• Original Assignee: AAI Corporation (Textron Inc)
• Inventors: Miller, Steve
• Primary Examiner(s): Swiatek, Robert P.
• Application Number:
  US09/639,159
• Time in Patent Office: 776 Days
• Field of Search: 244/63, 124/61, 446/429, 446/430
• US Class Current: 244/63
• CPC Class Codes: B64F 1/06 using catapults

Abstract

A mobile aircraft launcher includes a towable, tiltable, wheeled trailer, a launch beam comprising a plurality of sections hinged to one another, an aircraft-engaging shuttle mounted on the launch beam, and a shuttle-moving drive arrangement mounted on the trailer. The launch beam is mounted on the trailer and is movable between a folded, transport condition, in which the beam sections are generally side-by-side, and a launch condition, in which the beam sections are colinear. In the colinear arrangement, a portion of the launch beam extends forward of the trailer, that portion being supportable entirely through the trailer.

Claims

1. A mobile aircraft launcher comprising:

a wheeled trailer adapted to be towed by a land vehicle and to be tilted to launch an aircraft;

a launch beam mounted on the trailer, the launch beam comprising a plurality of beam sections hinged to one another, the launch beam being movable between a folded, transport condition, in which the beam sections are generally side-by-side, and a launch condition, in which the beam sections are colinear to define a continuous rectilinear beam;

an aircraft-engaging shuttle mounted on the launch beam for movement along the length of the launch beam;

a shuttle-moving drive arrangement mounted on the trailer; and

at least one jack secured to the trailer and adjustable between a) a first adjustment condition, in which the jack supports the launch beam in a horizontal attitude to facilitate the movement of the launch beam between its folded, transport condition and its launch condition, and b) a second adjustment condition, in which the wheeled trailer tilts, and the launch beam is in an inclined position for launch,

wherein the launch beam has a portion extending forward of the trailer with respect to the direction of launch when the beam sections are colinear, said portion being supportable entirely through the trailer when the beam sections are colinear.

2. The mobile aircraft launcher of claim 1, wherein the at least one jack is mounted on a rearward end of the trailer with respect to the direction of launch.

3. The mobile aircraft launcher of claim 2, further comprising a jack mounted on a forward end of the trailer with respect to the direction of launch.

4. The mobile aircraft launcher of claim 1, wherein the at least one jack is movable between a first position, in which the at least one jack is in contact with a ground surface supporting the trailer, and a second, retracted position, in which the at least one jack is clear of the ground surface.

5. The mobile aircraft launcher of claim 1, further comprising a towing member secured to and extending from the trailer for connection to a towing vehicle, the towing member extending farther from the trailer than the beam sections extend from the trailer in the folded, transport condition of the launch beam.

6. The mobile aircraft launcher of claim 1, further comprising means for releasably maintaining the beam sections in their generally side-by-side condition.

7. The mobile aircraft launcher of claim 1, wherein each of the beam sections has opposite ends, the ends of each of the beam sections, in the folded, transport condition of the launch beam, lying in substantially the same vertical plane as the ends of the other beam sections.

8. The mobile aircraft launcher of claim 7, wherein the launch beam comprises four beam sections.

9. The mobile aircraft launcher of claim 1, wherein the trailer has a single wheel axle, the trailer being tiltable about the single wheel axle.

10. The mobile aircraft launcher of claim 1, further comprising at least one launch beam jack for supporting a rear end of the launch beam in the inclined position for launch, the launch beam jack being releasably mounted on the trailer during transport of the launcher.

11. The mobile aircraft launcher of claim 1, wherein, in the horizontal attitude of the launch beam, the launch beam is no more than about 5 feet above a ground surface supporting the trailer.

12. A mobile aircraft launcher, comprising:

a wheeled trailer adapted to be towed by a land vehicle and to be tilted to launch an aircraft;

a launch beam mounted on the trailer, the launch beam comprising a plurality of beam sections hinged to one another, the launch beam being movable between a folded, transport condition, in which the beam sections are generally side-by-side, and a launch condition, in which the beam sections are colinear to define a continuous rectilinear beam;

an aircraft-engaging shuttle mounted on the launch beam for movement along the length of the launch beam;

a shuttle-moving drive arrangement mounted on the trailer; and

means secured to the trailer for selectively a) supporting the launch beam in a horizontal attitude to facilitate the movement of the launch beam between its folded, transport condition and its launch condition, and b) permitting the launch beam to move to an inclined position for launch,

wherein the launch beam has a portion extending forward of the trailer with respect to the direction of launch when the beam sections are colinear, said portion being supportable entirely through the trailer when the beam sections are colinear.

13. The mobile aircraft launcher of claim 12, wherein the trailer has a single wheel axle, the trailer being tiltable about the single wheel axle.

14. A method of deploying from a folded, transport condition to a launch condition a mobile aircraft launcher having

a launch beam defined by a plurality of beam sections hinged to one another, the beam sections being generally side-by-side in the folded, transport condition, and the beam sections being colinear to define a continuous rectilinear beam in the launch condition;

an aircraft-engaging shuttle mounted on the launch beam for movement along the length of the launch beam; and

a shuttle-moving drive arrangement,

the method comprising;

supporting the launch beam in a horizontal attitude;

pivoting the beam sections relative to one another from their generally side-by-side positions to their colinear positions in which a portion of the launch beam extends forward of the trailer with respect to the direction of launch while the launch beam is supported in the horizontal attitude;

during the step of pivoting, supporting said portion of the launch beam entirely through the trailer; and

moving the launch beam to an inclined position for launch.

15. The method of claim 14, further comprising securing the beam sections in their colinear positions while the launch beam is supported in the horizontal attitude.