DROGUE ASSEMBLY FOR AIR-TO-AIR ENGAGEMENT

Abstract

The present invention relates primarily to the field of air-to-air refueling of aircraft using an engagement between a tanker (or donor) aircraft and a receiver aircraft so that fuel may be delivered to the receiver aircraft via a fueling conduit, such as a hose or boom. The invention may also find application in other air-to-air engagement activities, such as recharging of an electric powered aircraft by delivery of an electrical recharging current to batteries of the aircraft via an electrical cable. In accordance with one aspect of the invention there is provided a drogue assembly for towing behind a donor aircraft, which drogue assembly comprises a reception coupling for engaging with a probe provided on a receiver aircraft and a drogue chute for stabilising the reception coupling when towed, wherein the drogue assembly further comprises at least one LiDAR sensor, a controller for the LiDAR and a data processor in data communication with the LiDAR for processing the sensed LiDAR data. The drogue assembly preferably includes an electrical energy storage device for powering one or more of: the LiDAR sensor, the controller and/or the data processor.

Claims

1. A drogue assembly for towing behind a donor aircraft, which drogue assembly comprises a reception coupling for engaging with a probe provided on a receiver aircraft and a drogue chute for stabilising the drogue when towed, wherein the drogue assembly further comprises at least one LiDAR sensor, a controller for the LiDAR and a data processor in data communication with the LiDAR for processing the LiDAR data.

2. A drogue assembly as claimed in claim 1 comprising an electrical energy storage device for powering LiDAR sensor, controller and data processor, such as a cell, battery or capacitor.

3. A drogue assembly as claimed in claim 2 comprising an energy converter adapted to convert kinetic energy of airflow over the drogue into electrical energy, such as a turbine and electrical generator, and wherein the electrical energy charges the energy storage device.

4. A drogue assembly as claimed in claim 3 wherein the convertor comprises a turbine and electrical generator driven by the turbine, the turbine comprising a fan attached to a generator rotor.

5. A drogue assembly as claimed in claim 3 wherein the turbine is co-axially disposed in a front region of the drogue assembly.

6. A drogue assembly as claimed in claim 1 wherein the LiDAR is configured and arranged to scan a field behind the drogue.

7. A drogue assembly as claimed in claim 6 wherein the LiDAR is adapted to generate a dot map image of an object, or part of an object, in the field of scanning.

8. A drogue assembly as claimed in claim 7 wherein the data processor comprises image recognition functionality for locating and tracking an aircraft, or part of an aircraft, in the field.

9. A drogue assembly as claimed in claim 7 wherein the data processor comprises image recognition functionality for locating and tracking the probe of the receiver aircraft.

10. A drogue assembly as claimed in claim 9 wherein the data processing system is adapted to calculate a position offset of the receiver aircraft's probe with respect to a reference point.

11. A drogue assembly as claimed in claim 10 wherein the reference point is the drogue assembly, or a portion of the drogue assembly, or especially the drogue reception coupling, or in particular an entrance of the reception coupling.

12. A drogue assembly as claimed in claim 1 wherein a drogue shifting system is provided for displacing the drogue assembly transversely in an X and/or Y direction with respect the towing Z axis of the drogue.

13. A drogue assembly as claimed in claim 12 wherein the drogue shifting system comprises one or more aerodynamic aids which are selectively deployable to cause a net force to act on the drogue assembly in the displacement direction.

14. A drogue assembly as claimed in claim 12 when dependent from claim 10 wherein the data processing system is adapted to use the offset to calculate a corrective transverse displacement direction.

15. A drogue assembly as claimed in claim 14 wherein the data processing system is adapted to apply the corrective transverse displacement direction to the drogue shifting system so as to steer the drogue assembly towards alignment with the probe.

16. A drogue assembly as claimed in claim 15 wherein the data processing system is adapted to conduct an iterative series of position offset calculations and corrective transverse displacement applications so as to cause the drogue assembly to approach the probe.

17. A drogue assembly as claimed in claim 15 wherein the data processing system is adapted to cause the reception coupling of the drogue assembly to approach the probe for engagement and latching therewith.

18. A drogue assembly as claimed in claim 1 wherein the LiDAR and data processor is adapted to establish a dot map of an object in the LiDAR field, and especially an aircraft in the LiDAR field.

19. A drogue assembly as claimed claim 18 wherein the LiDAR and data processor are adapted to provide transverse (X, Y axis) and distance (Z axis) information for the dots.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Following is a description by way of example only and with reference to the figures of the drawings of one mode for putting the present invention into effect.

[0015] FIG. 1 is a schematic side view of a drogue assembly in accordance with the present invention, shown in advance of the nose of a receiver aircraft.

[0016] FIG. 2 is a two dimensional representation of a dot map image of the receiver aircraft in a LiDAR field behind the drogue of the invention.

[0017] FIG. 3 is a flow chart of the processes carried out by the data processing system used in operating the drogue of the invention.

DETAILED DESCRIPTION OF EMBODIMENT(S)

[0018] In FIG. 1 a drogue assembly in accordance with the present invention is shown as 10. The drogue assembly comprises a body portion 11 which has a (convex) curved conical form. A twin-bladed turbine generator unit 9 is accommodated in a front region of the body portion, and co-axially located. The body portion has a nose region 12 at the apex of the cone. A coaxially attached refueling hose 13 is attached to the apex of the cone. The hose 13 leads to a tanker aircraft (not shown, but in direction Z). The nose region is provided with a bore (not shown) through which to deliver fuel from the hose through the body portion. An inner region of the body portion is configured as a probe reception coupling (not shown), such couplings being well known in the art. For example U.S. Pat. No. 9,950,804 (Mouskis) discloses a suitable reception coupling. Others are of course known in the art and may be used instead. The reception coupling is adapted to engage with the probe 20 of a receiver aircraft 21 (nose portion only shown). The reception coupling latches with the incoming probe and provides fluid communication between the fuel hose 13 and the probe. In this way fuel can be transferred along the hose from a tanker aircraft, via the reception coupling to the probe (which feeds a fuel tank of the receiver aircraft 21).

[0019] A rear end region of the body portion is provided with a rear facing LiDAR laser projector 14. The LiDAR is adapted to scan within a rectangular pyramidal detection field 15 behind the drogue, as shown by the dashed lines in FIG. 1 and the outer dashed lines in FIG. 2. There may be a single LiDAR transmitter and receiver pair, or an array of multiple sensors. A generally frusto-conical chute canopy 18 of conventional configuration is attached to a rear rim region 19 of the drogue body portion. The chute provides drag which aerodynamic stability and maintains a tension in the hose which facilitates controlled uncoiling to deploy the hose from the tanker aircraft, and stable winching-in to the tanker aircraft of the hose after use.

[0020] The body portion of the drogue assembly has an internal compartment 16 for accommodating microprocessor circuitry and a battery device. Also present are four steering flaps 22 (three of four are visible in FIG. 1) which are circumferentially spaced apart around a waist region of the drogue body portion. The flaps each have a generally wedge-shaped form, with a slightly concave outer (hypotenuse) surface. An underside of each flap is attached to an associated linear actuator (not shown). A leading edge 23 of each flap is pivotably attached to the waist region surface. The trailing edge region 24 of each flap may swing out about the leading edge pivot. Thus each flap may be selectively actuated so as to be deployed into the airstream when the drogue assembly is being towed. The deployed flap 22 locally increases drag, causing a reaction in the drogue which shifts the drogue laterally in the X-Y plane depending upon the orientation of the body portion and which flap is activated. (Strictly speaking the X-Y ‘plane’ is spherical, but with a very large radius compared to the lateral movement). The flaps may be deployed in adjacent pairs to provide diagonal shifting, or individually to provide orthogonal shifting and travel.

[0021] In use, the LiDAR transmitter sends flashes of light in a field ‘cone’ 15 extending rearwards of the drogue. The laser will scan in a raster across the field 15. Upon the light hitting an object (e.g. the receiver aircraft), some of the light will be reflected back towards the LiDAR receiver/sensor. The microprocessor can determine the range of the surface that the light reflected off by logging the time taken for the light dot to travel out and return. The processors can thus, during a complete scan cycle, build-up plot a three dimensional point cloud by combining thousands of these reflections. Thus a live image of the environment around the trailing components is built up. So, in use the LiDAR sensor 14 builds-up a dot map image 25 of the receiver aircraft, as shown in FIG. 2. The microprocessor's software is programmed to recognise an aircraft shape, and can also resolve and detect a refueling probe (as indicated by the inset dashed square 26 in FIG. 2). The microprocessor may include probe position information for specific aircraft, to help derive the probe position. In this way the incoming receiver aircraft 21 can be tracked, as can the probe, in the X-Y plane, and along the Z direction (distance away from the drogue).

[0022] Object detection software recognises the 3D image of the receiver aircraft and will locate the probe. The sensors are capable of detecting the probe/aircraft with no dependency on time of day or weather conditions. Software will process the data from the sensors and identify the probe/aircraft, simultaneously calculate distance from the drogue. This information can be transmitted by an on-board RF transmitter to the tanker or receiver aircraft. The control flaps can be manually or automatically operated to steer the drogue towards the aircraft's probe in response position information from the LiDAR. The dot map image may be used to facilitate the manual guidance of the drogue by control flap actuation, and may be of particular use at night.

[0023] A preferred version of the invention does away with the need to communicate to the tanker or receiver aircraft. In this version the data processing unit in the drogue body portion is programmed and configured to automatically guide the drogue towards the probe, and ultimately into engagement with the reception coupling. In this preferred aspect of the invention the microprocessor system is programmed to guide the drogue autonomously by sending actuation signals to the flap actuators. An initial step comprises the drogue assembly autonomously guiding itself towards the aircraft, and then as the aircraft comes close, switching to a mode in which the drogue is autonomously guided towards the expected position of the probe free end. As the drogue assembly approaches closer to the probe, sufficient dot resolution may permit the probe to be resolved so as to guide the reception coupling entrance in the rear portion of the drogue assembly to the probe.

[0024] FIG. 3 is a chart which represents schematically the components of the automated guidance system for sensing the position of a receiver aircraft and its probe relative to a refueling drogue assembly. There is turbine device 1 for harvesting energy from the passing airflow (see item 9 in FIG. 1). This is installed so as to use airflow to generate electricity which feeds a battery unit 3 for storing the harvested electrical charge, and powering the other components integrated into the drogue assembly. The battery provides a stable power supply to the linear actuators which serve as the flap actuation mechanism 2 for the control flaps (22 in FIG. 1). There is a data processing unit 4 which is also powered by the battery. The LiDAR sensor 5 is integrated into the rear end of the drogue body portion. This is positioned and directed to be able to scan a field backwards towards where a receiver aircraft would approach. The microprocessor 4 received signals from the LiDAR receiver that allows it to build a 3D point cloud image from the received data (and with the known transmitted signal data and raster timing). This point cloud image is analysed to determine how far away a receiver aircraft is from a datum point, such as the drogue body portion. It can also establish the spatial relationship of the probe with respect to the receiver aircraft. Based on this analysis an appropriate control flap (or flaps) is actuated so as to shift the drogue towards the probe. A feedback loop establishes whether the shifting response is appropriate and, if not, corrective control flap action can be taken. The drogue in this way gradually converges with the probe, so that the reception coupling latches onto the probe free end as it enters the aligned reception coupling. The pilot will of course still be involved in the docking process by gradually closing on the drogue along the Z-direction and generally maintaining steady alignment.

[0025] In the aforementioned autonomous embodiment, the entire system is confined within the drogue body portion. The use of batteries (and/or an optional turbine generator) means that there is no need for external power sources (such as from the tanker aircraft via the power cabling along the hose). There is no need for communication to the tanker and no communication with the receiver aircraft. The probe and drogue docking is automatic, and avoids the need for equipment to be added to the tanker aircraft or to the receiver aircraft. So the present inventors have with the present invention removed the need for a probe and drogue refueling system to have guidance components integrated into the tanker or receiver aircraft. This avoids the need for expensive certification of modifications and allows the system to be retrofitted to existing fleets of tankers simply by replacing the drogue assembly.