Method and apparatus for automated launch, retrieval, and servicing of a hovering aircraft

• US 8,453,966 B2
• Filed: 02/09/2010
• Issued: 06/04/2013
• Est. Priority Date: 02/12/2009
• Status: Active Grant

• Current Assignee: Aerovel Corporation
• Original Assignee: Aerovel Corporation
• Inventors: McGeer, Brian T., Von Flotow, Andreas H.
• Primary Examiner(s): Ellis, Christopher P
• Assistant Examiner(s): Badawi, Medhat
• Application Number:
  US12/702,935
• Publication Number:
  US 20110024559A1
• Time in Patent Office: 1,211 Days
• Field of Search: 244/110.F, 244/110.C, 244/63
• US Class Current: 244/110.F
• CPC Class Codes: B64C 25/68 Arrester hooks
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64F 1/02 for arresting aircraft, e.g. nets or cables
• CPC Class Codes: B64F 1/04 for launching aircraft
• CPC Class Codes: B64F 1/06 using catapults
• CPC Class Codes: B64F 1/12 for anchoring aircraft
• CPC Class Codes: B64F 1/125 Mooring or ground handling devices for helicopters
• CPC Class Codes: B64F 1/28 Liquid-handling installations specially adapted for fuelling stationary aircraft
• CPC Class Codes: B64F 5/00 Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
• CPC Class Codes: B64F 5/40 Maintaining or repairing aircraft
• CPC Class Codes: B64U 10/10 Rotorcrafts
• CPC Class Codes: B64U 10/17 Helicopters flying platforms B64U10/13
• CPC Class Codes: B64U 30/40 Empennages, e.g. V-tails foldable or collapsible UAVs B64U20/50
• 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
• CPC Class Codes: B64U 70/70 Launching or landing using catapults, tracks or rails launching from storage containers B64U70/50
• CPC Class Codes: B64U 80/25 for recharging batteries; for refuelling

Abstract

An aircraft capable of thrust-borne flight can be automatically retrieved, serviced, and launched using equipment suitable for use on a small vessel, or a base with similarly limited space or irregular motion. For retrieval, the aircraft drops a weighted cable, and pulls it at low relative speed into a broad aperture of a base apparatus. Continued translation of the aircraft may pull the cable clear of the apparatus, in which case it can continue in free flight and return for another retrieval attempt. Alternatively, the cable will be dragged along guiding surfaces of the apparatus into and through a slot or similar channel, until its free end is captured. The aircraft, having thus become anchored to the base station, is then pulled down by the cable into a receptacle. Guiding surfaces of the receptacle adjust the position and orientation of a probe on the aircraft, while directing the probe to mate with a docking fixture. Once mated to the fixture, the cable can be released and stored aboard the aircraft; the aircraft can be automatically shut down; and fueling or other servicing can be completed through appropriate connectors in the docking fixture. The aircraft can remain docked as needed, and when desired, be automatically started and tested in preparation for launch. It can then be released into free flight. A full ground-handling cycle can thus accomplished with simple and economical apparatus. It can be used with low risk of damage, and only moderate piloting accuracy.

Claims

1. An aircraft base retrieval apparatus for retrieving an aircraft from free flight, said apparatus comprising:

a cable holder configured to hold a point or fixture on a cable attached to an aircraft;

one or more linear or curvilinear cable-guiding surfaces forming a horizontal or substantially horizontal aperture configured to admit the cable and to guide the cable into the cable holder;

a docking receptacle; and

a base docking device configured to mate with an aircraft docking device attached to the aircraft.

2. The aircraft base retrieval apparatus of claim 1, wherein the cable holder is configured to release the cable.

3. The aircraft base retrieval apparatus of claim 1, wherein the one, or more linear or curvilinear guiding surfaces which form the aperture are rotatable about a vertical or principally vertical axis to accommodate variations in approach direction of the aircraft.

4. The aircraft base retrieval apparatus of claim 1, wherein the base docking device and the guiding surfaces are tiltable to accommodate variations in the orientation of the cable between the cable holder and the aircraft, or to set the appropriate aircraft orientation for launch.

5. The aircraft base retrieval apparatus of claim 1, which includes one or more connectors, which can be connected and disconnected to the aircraft to transfer fluid or electricity to the aircraft.

6. The aircraft base retrieval apparatus of claim 1, which includes a measuring device configured to measure a three-dimensional position of the aircraft relative to the aircraft base retrieval apparatus.

7. The aircraft base retrieval apparatus of claim 1, which includes a measuring device configured to measure an orientation of the aircraft relative to the aircraft retrieval base retrieval apparatus.

8. The aircraft base retrieval apparatus of claim 1, wherein the cable holder includes a one-way gate configured to permit entry of the cable into, but to prevent inadvertent release of the cable from the cable holder.