Pin array chamber systems and methods for releasing and capturing a moving object—space

• US 10,457,419 B2
• Filed: 08/08/2017
• Issued: 10/29/2019
• Est. Priority Date: 08/08/2017
• Status: Active Grant

• Current Assignee: Target Arm Inc.
• Original Assignee: Target Arm Inc.
• Inventors: McChesney, Jeffrey Alan
• Primary Examiner(s): McFall, Nicholas
• Assistant Examiner(s): Filosi, Terri L
• Application Number:
  US15/672,032
• Publication Number:
  US 20190047724A1
• Time in Patent Office: 812 Days
• Field of Search: 114322, 114259, 114 50, 114 51, 294 864
• CPC Class Codes: B64F 1/0299 characterized by the use of multiple devices
• CPC Class Codes: B64F 1/04 for launching aircraft
• CPC Class Codes: B64F 5/50 Handling or transporting aircraft components
• CPC Class Codes: B64G 1/646 Docking or rendezvous systems refueling in space B64G1/4024
• CPC Class Codes: B64U 2201/10 autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 70/30 for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net

Abstract

A pin array release and capture chamber system includes a chamber assembly having two parallel plates of pin arrays from which a plurality of pins extends and retract vertically opposite each other so as to release and capture a space vehicle. The pin arrays are separated from each other by a space having two vertical and two horizontal sides, and the space is sized so as to receive the space vehicle. Each pin arrays may be housed in a pin array chamber enclosure. The chamber assembly may be attached to a moving object, such as a host space vessel.

Claims

1. A pin array release and capture chamber system comprising:

two substantially parallel plates of pin arrays,

each pin array having a plurality of pins that extend and retract through the respective plate substantially perpendicular to the respective plate, the two pin arrays arranged vertically opposite each other with a space between the two pin arrays,

wherein the pins of a first pin array of the two pin arrays and the pins of a second pin array of the two pin arrays extend toward each other in an extended state and retract away from each other in a retracted state, and

wherein the space is enclosed by two vertical sides and two horizontal sides; and

wherein the two pin arrays are sized such that in the extended state more than one of the pins of each pin array comes into contact with the body of a vehicle.

2. The pin array release and capture chamber system of claim 1, further comprising two pin array chamber enclosures, each pin array chamber enclosure associated with one of the two pin arrays and into which the pins of the associated pin array are retracted in the retracted state.

3. The pin array release and capture chamber system of claim 1, is attached to a moving object.

4. The pin array release and capture chamber system of claim 3, wherein the moving object is a space vessel.

5. The pin array release and capture chamber system of claim 1, is stationary with respect to the vehicle.

6. The pin array release and capture chamber system of claim 1, wherein the vehicle is manned.

7. The pin array release and capture chamber system of claim 1, wherein the vehicle is unmanned.

8. The pin array release and capture chamber system of claim 1, wherein the vehicle is space debris.

9. The pin array release and capture chamber system of claim 1, wherein the vehicle is an object in space.