Brake-control system for accelerating freely falling objects to a moving craft's speed

• US 5,014,997 A
• Filed: 02/22/1990
• Issued: 05/14/1991
• Est. Priority Date: 03/20/1989
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Sanders Associates, INC. (BAE Systems Plc)
• Inventors: Smith, John A., Carlson, Mark A.
• Primary Examiner(s): Grieb, William H.
• Application Number:
  US07/483,107
• Time in Patent Office: 446 Days
• Field of Search: 273/360, 273/361
• US Class Current: 273/360
• CPC Class Codes: B64D 1/00 Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight with respect to weapon sights devices F41G takes precedence, parachutes per se B64D17/00; ejectable seats B64D25/10; ejectable capsules B64D25/12; refuelling during flight B64D39/00; launching apparatus for projecting projectiles or missiles F41F1/00, F41F7/00; rocket or torpedo launchers F41F3/00
• CPC Class Codes: F41J 9/10 towed

Abstract

In a moving craft connected by a towline to an ejected and freely falling object, a brake control system determines when to engage a brake that accelerates the object to the moving craft'"'"'s speed by retarding the deployment of the towline without exceeding its rated working load. The control system continually monitors the velocity and the total deployed distance of the ejected object. When a point in a velocity-distance state-space plane corresponding to the monitored velocity and the monitored total deployed distance of the ejected object has reached a switching curve (48), the control system actuates a brake (74). The switching curve (48) is the locus of intersection points (38, 40, 42, and 44) of a plurality of pairs of curves, each pair consisting of a free-fall trajectory (23, 24, 26, and 28) and a brake trajectory (30, 32, 34, and 36) and being associated with a different craft velocity. The free-fall trajectory is the trajectory that the object follows after it has been ejected from the craft and is falling away from the craft under the influence of drag. The brake trajectory is the trajectory by which the brake system causes the object to stop at the desired deployment distance.

Claims

1. A method of controlling the deployment of a towline connecting a moving craft to an ejected object, the method comprising the steps of:

a. allowing the object to fall freely from the craft;

b. continuously monitoring the velocity and the total deployed distance of the object relative to the moving craft as it is falling freely;

c. continuously determining whether a point in a velocity-distance state-space plane defined by the monitored velocity and the monitored total deployed distance of the object has reached a switching curve, the switching curve comprising a locus of points of intersection of a plurality of free-fall trajectories of the object with a corresponding plurality of brake trajectories of the object, each of the plurality of free-fall trajectories being the trajectory followed by the object at a different velocity of the moving craft, each of the plurality of brake trajectories being the trajectory followed by the object, for a different craft speed, when a given brake system is engaged to retard the deployment of the towline; and

d. in response to a determination that the point in the velocity-distance state-space plane defined by the monitored velocity and total deployed distance has reached the switching curve, engaging the given brake system to retard the deployment of the towline.

2. A method as defined in claim 1 wherein:

a. the towline has a rated breaking tension; and

b. the given brake system applies to the towline a tension less than the breaking tension when it is engaged.

3. For controlling the deployment of a towline connecting a moving craft to an ejected and object, an object-deployment system comprising:

a. sensor means for continuously monitoring the total deployed distance of the object and the velocity of the object with respect to the craft and for generating an indication thereof;

b. a brake system, adapted for application of a brake signal thereto, for engaging in response to the brake signal to retard the deployment of the towline; and

c. means responsive to the sensor means for continuously determining whether a point in a velocity-distance state-space plane defined by the monitored velocity and the monitored total deployed distance has reached a switching curve in the velocity-distance state-space plane and for generating a brake signal if it has, the switching curve comprising a locus of points of intersection of a plurality of free-fall trajectories of the object with a corresponding plurality of brake trajectories of the object, each of the plurality of free-fall trajectories being the trajectory followed by the object at a different velocity of the moving craft, each of the plurality of brake trajectories being the trajectory followed by the object, for a different craft speed, when the brake system is engaged to retard the deployment of the towline.

4. An object-deployment system as defined in claim 3 wherein:

a. the towline has a rated breaking tension; and

b. the brake system applies a tension less than the breaking tension when it is engaged.

5. An object-deployment system as defined in claim 3 wherein:

a. the system further includes a rotatably mounted reel about which the towline is wound in such a manner that the towline deploys as the reel rotates and the towline stops deployment when the reel stops rotating; and

b. the brake system comprises means for retarding the rotation of the reel when the brake system engages.

6. An object-deployment system as defined in claim 5 wherein:

a. the reel further includes a brake-engagement surface; and

b. the brake system comprises;

i. a brake body;

ii. a solenoid attached to the brake body and operable between an engaged state, in which it urges the brake body against the brake-engagement surface to apply frictional force thereto to tend to retard rotation of the reel, and a disengaged state, in which it refrains from urging the brake body against the brake-engagement surface; and

iii. means responsive to the brake signal to operate the solenoid to its engaged state in response to reception of the brake signal.

7. An object-deployment system as defined in claim 6 wherein:

a. the brake body is generally frustoconical; and

b. the brake-engagement surface shaped complimentarily to the brake body.