System for tactical balloon launch and payload return

• US 8,061,648 B2
• Filed: 02/26/2009
• Issued: 11/22/2011
• Est. Priority Date: 02/26/2008
• Status: Active Grant

• Current Assignee: Timothy T. Lachenmeier
• Original Assignee: Timothy T. Lachenmeier
• Inventors: Lachenmeier, Timothy T.
• Primary Examiner(s): Chambers; Troy
• Application Number:
  US12/379,692
• Publication Number:
  US 20090224094A1
• Time in Patent Office: 999 Days
• Field of Search: 244/24, 244 30- 33, 244/62, 244/115, 244/116
• US Class Current: 244/33
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 10/30 Lighter-than-air aircraft, e.g. aerostatic aircraft
• CPC Class Codes: B64U 10/50 Glider-type UAVs, e.g. with parachute, parasail or kite for landing B64U70/83
• CPC Class Codes: B64U 20/80 Arrangement of on-board electronics, e.g. avionics systems or wiring
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2101/31 for surveillance
• CPC Class Codes: B64U 70/20 for releasing or capturing UAVs in flight by another aircraft

Abstract

A system is disclosed whereby a sensor, communication device, or other payload may be lofted to an operational altitude and maintained over an area of interest for some time by a relatively inexpensive and disposable buoyant aircraft, then returned intact to its point of origin or another desired location by a reusable but also relatively inexpensive non-buoyant aircraft. Automatic unpiloted control is used for all stages of flight, including ascent, loiter, return, and landing Specialized equipment can be provided to simplify launch procedures, reducing the number of personnel required to operate the system.

Claims

1. A launch apparatus for a multi-cell balloon system comprising:

a fabric launch bag which protects a tow balloon of said multi-cell balloon system from high winds while filling said tow balloon with lifting gas, and subsequently which quickly releases said tow balloon into the air;

a deployment bag which during launch and initial ascent compactly contains a main balloon attached to said tow balloon of said multi-cell balloon system, said deployment bag and main balloon together forming a packed main balloon, and subsequently which deploys said main balloon in a controlled fashion at an appropriate altitude; and

a launch cradle which prior to launch supports said packed main balloon and a payload to be carried aloft by said multi-cell balloon system, maintaining the buoyant and non-buoyant elements in proper orientation, to one another as the launch apparatus moves around with the wind, and which during launch releases said packed main balloon and payload at an appropriate angle as said tow balloon rises.

2. The launch apparatus of claim 1, further comprising an adjustable bottom fitting on said packed main balloon, whereby the length and therefore volume of said main balloon may be set as appropriate for a particular flight.

3. The launch apparatus of claim 1, wherein said launch bag implements its quick-release function by incorporating a seam that is held closed during filling by a fastener running the length of said seam, wherein said fastener is quickly and easily pulled apart for launch.

4. The launch apparatus of claim 1, wherein said launch bag further comprises means for adjusting its circumference and therefore volume, thereby controlling fill volume of said tow balloon.

5. The launch apparatus of claim 1, wherein said launch bag includes weighted inflatable members, and additional ballast pockets incorporated into the bag.

6. The launch apparatus of claim 3, further comprising means whereby the flow of gas filling said tow balloon is automatically stopped when the amount of gas has reached the preset fill volume.