MULTIPLE VEHICLE SYSTEM
20230227155 · 2023-07-20
Inventors
- Ernestine Fu (Superior Township, MI, US)
- Grey Parker (West Bloomfield, MI, US)
- Prasanna Natarajan (Aldie, VA, US)
- Matt Korich (Superior Township, MI, US)
- Jacob Viau (Superior Township, MI, US)
- David Wilson (Superior Township, MI, US)
- John Suh (Palo Alto, CA, US)
- David Byron (Southfield, MI, US)
- Mark Lister (Superior Township, MI, US)
Cpc classification
Y02T10/70
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B64D2221/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
B64C37/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A combination two vehicle system is provided that includes a land-based vehicle configured for traversal over ground and an aerial vehicle configured for travel through air, where the aerial vehicle is configured to detachably couple with the land-based vehicle. The aerial vehicle includes stabilizing legs to provide stability for take-off or landing. A method of operating the vehicle system includes steps of: providing the land-based and the aerial vehicle having the stabilizing legs, and aerially transporting the vehicle system including the land-based vehicle and the aerial vehicle, where the stabilizing legs provide stability for take-off or landing. In addition, the land-based vehicle may transport a removable cargo pod, which the aerial vehicle may independently retrieve from the land-based vehicle.
Claims
1. A vehicle system comprising: a land-based vehicle component; and an aerial vehicle component having a plurality of stabilizing legs, wherein the land-based vehicle and aerial vehicle components are releasably coupled, and wherein the stabilizing legs are configured to provide stability for take-off or landing.
2. The vehicle system of claim 1 wherein the land-based vehicle component and aerial vehicle component are coupled by multiple engagements.
3. The vehicle system of claim 1 wherein the aerial vehicle component comprises a connection mechanism for detachable coupling with the land-based vehicle component.
4. The vehicle system of claim 1 wherein the land-based vehicle component and the aerial vehicle component are coupled via a data communication connection.
5. The vehicle system of claim 1, wherein the land-based vehicle and the aerial vehicle are coupled via an electrical connection.
6. The vehicle system of claim 5, wherein the electrical connection is configured to provide a power transmission between the land-based vehicle component and the aerial vehicle component, wherein the power transmission is configured to charge a battery of the land-based vehicle component.
7. The vehicle system of claim 1, wherein the land-based vehicle component comprises a removable cargo pod.
8. The vehicle system of claim 7, wherein the aerial vehicle component is configured to travel with the removable cargo pod independent of the land-based vehicle.
9. The vehicle system of claim 8 wherein the aerial vehicle component comprises a unit to retrieve the removable cargo pod from the land-based vehicle.
10. The vehicle system of claim 1 wherein the aerial vehicle component comprises a fixed wing.
11. The vehicle system of claim 1 wherein the aerial vehicle component comprises a rotary wing.
12. A vehicle system comprising: a land-based vehicle component; and an aerial vehicle component having a plurality of stabilizing legs, wherein the land-based vehicle and aerial vehicle components are configured to be operated in combination or separately, and wherein the stabilizing legs are configured to provide stability for take-off or landing.
13. A method of operating a vehicle system comprising, (a) providing a vehicle system that comprises (i) a land-based vehicle component and (ii) an aerial vehicle component having a plurality of stabilizing legs; and (b) aerially transporting the vehicle system that comprises the (i) land-based vehicle component and (ii) aerial vehicle component, wherein the stabilizing legs are configured to provide stability for take-off or landing.
14. The method of claim 13 wherein the (i) land-based component and (ii) aerial vehicle component are releasably engaged during the aerial transporting.
15. The method of claim 13 wherein following the aerial transporting the vehicle system is operated as a ground vehicle.
16. The method of claim 15 wherein the (i) land-based component and (ii) aerial vehicle component are releasably engaged during the ground vehicle operation.
17. The method of claim 15 wherein the (i) land-based component and (ii) aerial vehicle component are disengaged during the ground vehicle operation.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0023] The accompanying drawings, which are incorporated in and form a part of the Description of Embodiments, illustrate various embodiments of the subject matter and, together with the Description of Embodiments, serve to explain principles of the subject matter discussed below. Unless specifically noted, the drawings referred to in this Brief Description of Drawings should be understood as not being drawn to scale. Herein, like items are labeled with like item numbers.
[0024]
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
[0031]
[0032]
DETAILED DESCRIPTION
[0033] As discussed, we now provide a multiple vehicle system that comprises an aerial vehicle and a land-based vehicle. That is, the present systems are capable of flight (aerial travel) as well as robust ground travel. Preferred vehicle systems include a combination two vehicle system including an aerial vehicle and a land-based vehicle. In certain preferred aspects, the constituent vehicles of the combination two vehicle system are configured for cooperative transport, such that the aerial vehicle is configured to convey the land-based vehicle during aerial travel for delivery to a desired location. In accordance with some embodiments, the aerial vehicle and the land-based vehicle are operable to provide cooperative or symbiotic operations.
[0034] The terms “aerial vehicle” and “aerial vehicle component” are generally used interchangeably herein. The terms “land-based vehicle” and “land-based vehicle component” also are generally used interchangeably herein.
[0035] Referring now to the drawings,
[0036] In some embodiments, aerial vehicle 110 is able to convey land-based vehicle 120 to an otherwise inaccessible or difficult to access location, either due to limits on ground access or travel time. For example, the destination may be located in a remote region without access by roads, or the destination may be far enough away such that ground access would not be possible for timely conveyance of land-based vehicle 120. In other examples, the destination may be difficult to access on the ground due to current conditions, such as natural disasters, weather conditions, military conflict zones, or other forms of civil unrest. Combination two vehicle system 100 is capable of delivering land-based vehicle 120 for ground operations using aerial vehicle 110.
[0037] It should be appreciated that various design considerations and optimizations are taken into account when designing combination two vehicle system 100 based on potential use cases. For example, since aerial vehicle 110 is configured to convey a land-based vehicle 120 through the air to a destination, and potentially to convey additional cargo of land-based vehicle 120 and/or aerial vehicle 110 such as in cargo unit 112, land-based vehicle 120 should be as preferably light weight and strong.
[0038] As shown in
[0039] As further shown in
[0040]
[0041] In accordance with various embodiments, aerial vehicle 110 is capable of remote operation, autonomous operation, or a combination of remote and autonomous operation. For example, a user may be able to remotely control operation of aerial vehicle 110, such as from a command center. In other examples, aerial vehicle 110 is configured to operate autonomously, such that a destination is provided and aerial vehicle 110 is capable of self-navigating to the destination.
[0042] In some embodiments, aerial vehicle 110 is powered using hybrid power including a combination of combustion and electrical power sources. In such embodiments, the combustion component of the hybrid power source can charge a battery of the electrical power source during operation. The hybrid power source can also be used as a charging station for land-based vehicle 120, either during air travel or on the ground, when land-based vehicle 120 is coupled to aerial vehicle 110.
[0043] Aerial vehicle 110 is capable of performing short takeoffs and landings. In some embodiments, aerial vehicle 110 is capable of performing substantially vertical takeoffs and landings, but this may be difficult in certain situation, e.g., where aerial vehicle 110 is carrying land-based vehicle 120 and/or another heavy payload. In some embodiments, aerial vehicle 110 is capable of hovering at a substantially steady position during operation (e.g., is a drone).
[0044] Aerial vehicle 110 includes a connection mechanism for detachably coupling to land-based vehicle 120. In some embodiments, aerial vehicle 110 is configured to engage the connection mechanism with land-based vehicle 120 by approaching land-based vehicle 120 vertically or laterally from one direction.
[0045]
[0046] In certain aspects, land-based vehicle 120 is capable of navigating extreme and rugged terrain that is typically unnavigable for conventional automobiles or off-road vehicles. For example, nesting leg units 320 are capable of providing walking travel for land-based vehicle 120 as disclosed in U.S. Pat. Application Publication No. 2020/02161271. In designing land-based vehicle 120, and nesting leg units 320 (or any other mechanism for providing walking travel), four metrics of motion capabilities should be considered: [0047] the height of any step onto which land-based vehicle 120 might need to climb; [0048] the steepness of any angle which land-based vehicle 120 might need to traverse; [0049] the height and width (e.g., depth) of an obstacle over which land-based vehicle 120 might need to traverse; and [0050] the width (e.g., depth) of any gap which land-based vehicle 120 might need to step over. As should be understood, these exemplary metrics are considerations for designing the ground traversal abilities of land-based vehicle 120, and might be dependent or based on potential locations for usage of land-based vehicle 120. For example, these four metrics would be different for different climates and terrains, as well as urban or wilderness terrains.
[0051] Various other factors should also be considered in designing land-based vehicle 120. For example, as land-based vehicle 120 is designed for use in different extreme environments, land-based vehicle 120 should be designed to withstand environments of both hot and cold temperatures, should be able to withstand rain and water damage, and be able to traverse different types of ground (e.g., sand, snow, ice, brush, water, etc.) In some embodiments, land-based vehicle 120 may be used on the surface of the moon or other planets, such as Mars, and should be designed according to those environments.
[0052] In accordance with various embodiments, land-based vehicle 120 is capable of remote operation, autonomous operation, or a combination of remote and autonomous operation. For example, a user may be able to remotely control operation of land-based vehicle 120, such as from a command center. In other examples, land-based vehicle 120 is configured to operate autonomously, such that a destination is provided and land-based vehicle 120 is capable of self-navigating to the destination.
[0053] In some embodiments, land-based vehicle 120 includes cargo pod 330 as shown in
[0054]
[0055] In some embodiments, aerial vehicle 110 includes a hoist and cable for lowering and raising connection mechanism 410. For example, deployment or recovery of land-based vehicle 120 may be in a location where aerial vehicle 110 is unable to land (e.g., dense trees or heavy winds). Aerial vehicle 110 can hover over the destination and deploy or recover land-based vehicle by lowering and raising connection mechanism 410 using the hoist and cable. Connection mechanism 410 can be released (for deployment) or engaged (for retrieval) when land-based vehicle 120 is on the ground. Another example of a use for hoist and cable deployment and retrieval is into a cave or pit that is inaccessible by ground travel.
[0056]
[0057] As illustrated, second location 520 is inaccessible via ground access from first location 510 due to the extreme terrain (e.g., mountains and forest) between first location 510 and second location 520. It should be appreciated that second location 520 may be inaccessible via ground access from first location 510 for other reasons, such as distance (e.g., travel time is too long for ground access), weather conditions, natural disasters (e.g., forest fires, floods, earthquakes), military conflict, or other forms of civil unrest.
[0058] It should be appreciated that various types of ground operations can be performed by land-based vehicle 120. For instance,
[0059] In some embodiments, land-based vehicle 120 includes a battery for storing and providing power to connected devices. In one embodiment, aerial vehicle 110 is configured to charge the battery of land-based vehicle 120 (e.g., during air travel). In some embodiments, land-based vehicle 120 includes solar panels for charging the battery.
[0060]
[0061] In some embodiments, aerial vehicle 110 can retrieve cargo pod 710 (e.g., using a connection mechanism 720) including the collected goods or materials and deliver cargo pod 710 to another destination while land-based vehicle 120 continues collection. In some examples, land-based vehicle 120 has more than one cargo pod 710 or aerial vehicle 110 can delivery another cargo pod 710 to land-based vehicle 120, such that the ground operation can continue while aerial vehicle 110 transports the first cargo pod 710 to another destination.
[0062]
[0063] In such use cases, aerial vehicle 110 can scan the terrain and perform mapping of areas of interest (e.g., areas of travel by land-based vehicle 120). Aerial vehicle 110 can transmit the information about the terrain, such as mapping information, to land-based vehicle 120. Land-based vehicle 120 may then use this information in addition to any information it has or is capable of obtaining on its own, to supplement the navigation of land-based vehicle 120 over the terrain. This symbiotic use case of aerial vehicle 110 supplementing the navigation information of land-based vehicle 120 is particularly useful in extreme environments where the terrain may be unknown. For example, this may be particularly useful in exploration of the moon or other planets.
[0064]
[0065] In such use cases, aerial vehicle 110 can hover or fly over land-based vehicle 120 and act as an intermediary device for supporting data communications between land-based vehicle 120 and the remote command post. Aerial vehicle 110 can maintain a location in the air over land-based vehicle 120 above the natural features that might be blocking or disrupting data communication between land-based vehicle 120 and the remote command post, thereby improving the data connection between land-based vehicle 120 and the remote command post. This symbiotic use case of aerial vehicle 110 supplementing the data communication capabilities of land-based vehicle 120 is particularly useful in rugged terrain.
[0066] What has been described above includes examples of the subject disclosure. It is, of course, not possible to describe every conceivable combination of components or methodologies for purposes of describing the subject matter, but it is to be appreciated that many further combinations and permutations of the subject disclosure are possible. Accordingly, the claimed subject matter is intended to embrace all such alterations, modifications, and variations that fall within the spirit and scope of the appended claims.
[0067] In particular and in regard to the various functions performed by the above described components, devices, systems and the like, the terms (including a reference to a “means”) used to describe such components are intended to correspond, unless otherwise indicated, to any component which performs the specified function of the described component (e.g., a functional equivalent), even though not structurally equivalent to the disclosed structure, which performs the function in the herein illustrated exemplary aspects of the claimed subject matter.
[0068] The aforementioned systems and components have been described with respect to interaction between several components. It can be appreciated that such systems and components can include those components or specified sub-components, some of the specified components or sub-components, and/or additional components, and according to various permutations and combinations of the foregoing. Sub-components can also be implemented as components communicatively coupled to other components rather than included within parent components (hierarchical). Additionally, it should be noted that one or more components may be combined into a single component providing aggregate functionality or divided into several separate sub-components. Any components described herein may also interact with one or more other components not specifically described herein.
[0069] In addition, while a particular feature of the subject innovation may have been disclosed with respect to only one of several implementations, such feature may be combined with one or more other features of the other implementations as may be desired and advantageous for any given or particular application. Furthermore, to the extent that the terms “includes,” “including,” “has,” “contains,” variants thereof, and other similar words are used in either the detailed description or the claims, these terms are intended to be inclusive in a manner similar to the term “comprising” as an open transition word without precluding any additional or other elements.
[0070] Thus, the embodiments and examples set forth herein were presented in order to best explain various selected embodiments of the present invention and its particular application and to thereby enable those skilled in the art to make and use embodiments of the invention. However, those skilled in the art will recognize that the foregoing description and examples have been presented for the purposes of illustration and example only. The description as set forth is not intended to be exhaustive or to limit the embodiments of the invention to the precise form disclosed.