Missile for implanting actuator in a room or building

Patent metadata

Field	Value
Publication number	US-9423223-B2
Application number	US-201514828514-A
Country	US
Kind code	B2
Filing date	Aug 17, 2015
Priority date	Nov 2, 2012
Publication date	Aug 23, 2016
Grant date	Aug 23, 2016

Abstract

A new form of missile, for implantation of an actuator within a wall or building, is provided. In some aspects of the invention, the missile comprises an enclosed actuator, deployed upon successful implantation of the missile in a target wall. Preferably, the missile comprises stops and piercing grips to secure the missile within the target wall, and encourage the proper degree of penetration and a mounting position enabling the deployment of the actuator(s) comprised within the missile. In some embodiments, the actuator can be remotely actuated by control system and user commands.

First claim

I claim:

1. A missile system for breaching, mounting and deploying an actuator within a wall, comprising:
a streamlined piercing tip;
a main body;
a sensor connected for communications with a control system; and
a actuator, other than said sensor, configured to carry out operations after said sensor senses proper mounting of said main body within a wall;
wherein said control system governs said operations and said sensor.

2. The missile system of claim 1 , comprising:
a control unit configured to detect said proper mounting and activate and deploy said actuator.

3. The missile system of claim 2 , wherein said sensor comprises
a trigger configured to indicate when said proper mounting has occurred.

4. The missile system of claim 3 , wherein said trigger aids in decelerating said missile with force-biasing comprised in said trigger tending to move said trigger toward an untriggered position.

5. The missile system of claim 2 , wherein a remote GUI is configured to control said actuator.

6. The missile system of claim 2 , wherein said control system is also in communication with a user after mounting of said control system in a wall, and wherein said system presents said user with a GUI configured to monitor and control activity within a target room via said sensor or said actuator.

7. The missile system of claim 6 , wherein said actuator and control system react to sensed data within a target room autonomously.

8. The missile system of claim 2 , wherein said actuator comprises a non-lethal personnel-disabling weapon.

9. The missile system of claim 2 , wherein said actuator comprises a camera.

10. A missile system for breaching, mounting and deploying an actuator within a wall, comprising:
a streamlined piercing tip;
a main body;
an actuator configured to carry out operations after proper mounting of said main body within a wall; and
a control unit configured to detect said proper mounting and activate and deploy said actuator;
wherein said actuator comprises a camera.

11. The system of claim 10 , comprising grasping claws configured to serve as fins when at least part of the system is in flight.

12. The system of claim 10 , wherein part of an outer housing of said piercing tip comprises hinged leaves, configured to house and expose at least part of said actuator.

13. The system of claim 10 , wherein said system comprises at least one communications antenna and said control unit and a user may manipulate said actuator by issuing commands.

14. The system of claim 10 , wherein at least some of said operations are selected based on data gathered by said actuator.

15. A missile system for breaching, mounting and deploying an actuator within a wall, comprising:
a streamlined piercing tip;
a main body;
a sensor connected for communication with a control system; and
an actuator configured to carry out operations after proper mounting of said main body within a wall;
wherein said sensor comprises:
a trigger configured to indicate when said proper seating has occurred.

16. The missile system of claim 15 , wherein said trigger aids in decelerating said missile with force-biasing comprised in said trigger tending to move said trigger toward an untriggered position.

17. System of claim 15 , wherein said system comprises a control unit configured to detect said proper mounting and activate and deploy said actuator;
wherein said control system is also in communication with a user after mounting of said control system in a wall; and
wherein said system presents said user with a GUI configured to monitor and control activity within a target room via said sensor or said actuator.

Assignees

• Beckman Christopher V

Inventors

• Beckman Christopher V

Classifications

• F42B15/01

  Arrangements thereon for guidance or control ({steering arrangements F42B10/60}; aircraft flight control B64C; guidance systems other than those installed aboard F41G7/00, F41G9/00; locating by use of radio or other waves G01S; flight control in general G05D1/00; computer aspects G06]) · CPC title

• F42B12/02 Primary

  characterised by the warhead or the intended effect · CPC title

• F42B12/52

  Fuel-air explosive devices · CPC title

• F42B12/36

  for dispensing materials; for producing chemical or physical reaction; for signalling {; for transmitting information} · CPC title