US20230226900A1 - Dual structural and storage apparatus - Google Patents
Dual structural and storage apparatus Download PDFInfo
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- US20230226900A1 US20230226900A1 US18/098,041 US202318098041A US2023226900A1 US 20230226900 A1 US20230226900 A1 US 20230226900A1 US 202318098041 A US202318098041 A US 202318098041A US 2023226900 A1 US2023226900 A1 US 2023226900A1
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Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K1/00—Arrangement or mounting of electrical propulsion units
- B60K1/04—Arrangement or mounting of electrical propulsion units of the electric storage means for propulsion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D21/00—Understructures, i.e. chassis frame on which a vehicle body may be mounted
- B62D21/02—Understructures, i.e. chassis frame on which a vehicle body may be mounted comprising longitudinally or transversely arranged frame members
- B62D21/03—Understructures, i.e. chassis frame on which a vehicle body may be mounted comprising longitudinally or transversely arranged frame members transverse members providing body support
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/32—Wings specially adapted for mounting power plant
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/204—Racks, modules or packs for multiple batteries or multiple cells
- H01M50/207—Racks, modules or packs for multiple batteries or multiple cells characterised by their shape
- H01M50/213—Racks, modules or packs for multiple batteries or multiple cells characterised by their shape adapted for cells having curved cross-section, e.g. round or elliptic
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/249—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/258—Modular batteries; Casings provided with means for assembling
- H01M50/26—Assemblies sealed to each other in a non-detachable manner
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K11/00—Arrangement in connection with cooling of propulsion units
- B60K11/06—Arrangement in connection with cooling of propulsion units with air cooling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K1/00—Arrangement or mounting of electrical propulsion units
- B60K2001/003—Arrangement or mounting of electrical propulsion units with means for cooling the electrical propulsion units
- B60K2001/005—Arrangement or mounting of electrical propulsion units with means for cooling the electrical propulsion units the electric storage means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K1/00—Arrangement or mounting of electrical propulsion units
- B60K1/04—Arrangement or mounting of electrical propulsion units of the electric storage means for propulsion
- B60K2001/0405—Arrangement or mounting of electrical propulsion units of the electric storage means for propulsion characterised by their position
- B60K2001/0438—Arrangement under the floor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60Y—INDEXING SCHEME RELATING TO ASPECTS CROSS-CUTTING VEHICLE TECHNOLOGY
- B60Y2200/00—Type of vehicle
- B60Y2200/50—Aeroplanes, Helicopters
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60Y—INDEXING SCHEME RELATING TO ASPECTS CROSS-CUTTING VEHICLE TECHNOLOGY
- B60Y2200/00—Type of vehicle
- B60Y2200/50—Aeroplanes, Helicopters
- B60Y2200/51—Aeroplanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D25/00—Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
- B62D25/20—Floors or bottom sub-units
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
- B64D27/357—Arrangements for on-board electric energy production, distribution, recovery or storage using batteries
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
-
- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Definitions
- This disclosure relates generally to systems in need of storage and structural support.
- Vehicles include systems and structures that both add significant weight to the vehicle.
- the batteries can weigh over a couple of thousand pounds.
- the vehicle exhibits limited efficiency.
- the apparatus includes a housing having an outer surface, an inner surface, and at least one opened end.
- the apparatus also includes first attachment devices disposed at the outer surface and second attachment devices disposed at the outer surface.
- the second attachment devices are configured to be removably attachable to the first attachment devices.
- a structural/storage system that includes a plurality of storage elements.
- Each of the storage elements includes a housing having an outer surface, an inner surface, and at least one opened end.
- the structural/storage system further includes first attachment devices disposed at the outer surface and second attachment devices disposed at the outer surface.
- the second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
- a system that includes a load device, a power element configured to power the load device, and a plurality of storage elements.
- Each of the storage elements includes a housing having an outer surface, an inner surface, and at least one opened end.
- the storage elements include first attachment devices disposed at the outer surface and second attachment devices disposed at the outer surface.
- the second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
- FIG. 1 is a system block diagram of components of a vehicle, according to one or more examples of the present disclosure
- FIG. 2 is a perspective view of a structural and storage element used in the vehicle of FIG. 1 , according to one or more examples of the present disclosure
- FIG. 3 is a cross-sectional view of the element of FIG. 2 , according to one or more examples of the present disclosure
- FIG. 4 is a perspective view of attached structural and storage elements used in the vehicle of FIG. 1 , according to one or more examples of the present disclosure
- FIG. 5 is a cross-sectional view of the elements of FIG. 4 , according to one or more examples of the present disclosure
- FIG. 6 is a perspective view of a stacked structural and storage elements used in the vehicle of FIG. 1 , according to one or more examples of the present disclosure
- FIG. 7 is a cross-sectional view of the elements of FIG. 6 , according to one or more examples of the present disclosure.
- FIG. 8 is a perspective view of a stacked structural and storage elements used in the vehicle of FIG. 1 , according to one or more examples of the present disclosure
- FIG. 9 is a cross-sectional view of the elements of FIG. 8 , according to one or more examples of the present disclosure.
- FIG. 10 is a perspective view of a vehicle with structural and storage elements, according to one or more examples of the present disclosure.
- FIG. 11 is a cross-sectional view of the vehicle of FIG. 10 , according to one or more examples of the present disclosure.
- FIG. 12 is a perspective view of a portion of a vehicle with structural and storage elements, according to one or more examples of the present disclosure.
- FIG. 13 is a perspective view of a vehicle component attached to one of the structural and storage elements of the vehicle of FIG. 12 , according to one or more examples of the present disclosure
- FIG. 14 is a perspective view of an aircraft with a structural and storage system, according to one or more examples of the present disclosure.
- FIG. 15 is a cross-sectional view of a portion of the aircraft of FIG. 14 , according to one or more examples of the present disclosure
- FIG. 16 is a cross-sectional view of the structural and storage system used in the aircraft of FIG. 14 , according to one or more examples of the present disclosure
- FIG. 17 is a perspective view of a storage element, according to one or more examples of the present disclosure.
- FIG. 18 is a perspective view of the storage element of FIG. 17 being received in a modular structural element, according to one or more examples of the present disclosure
- FIG. 19 is a perspective view of the storage element of FIG. 17 being received in a modular structural element, according to one or more examples of the present disclosure
- FIG. 20 is a perspective view of the storage element of FIG. 17 received within a modular structural element, according to one or more examples of the present disclosure.
- FIG. 21 is a plan view of the storage element of FIG. 17 received within a modular structural element, according to one or more examples of the present disclosure.
- Exemplary apparatuses and systems, disclosed herein, include dual structural and storage devices that are used to provide storage and structural integrity.
- a vehicle 20 includes a load device 22 and a power source/vehicle structural system 24 that houses a stored element 30 (material (e.g., fuel) or device (e.g., batteries)).
- the power source/vehicle structural system 24 provides secure housing for the stored element 30 and provides structural integrity for the vehicle 20 .
- the stored element 30 may be fuel, fuel cells, batteries, or any system component, not limited to a power source.
- the load device 22 is any device that receives the stored element 30 (material) stored in the power source/vehicle structural system 24 or electrical power/current produced by the stored element 30 .
- the vehicle 20 may include a motor vehicle driven by wheels and/or tracks, such as, without limitation, an automobile, a truck, a sport utility vehicle (SUV), a van, and the like.
- the vehicle 20 may include a marine vessel such as, without limitation, a boat, a ship, a submarine, a submersible, an autonomous underwater vehicle (AUV), and the like.
- the vehicle 20 may include an aircraft such as, without limitation, a fixed wing aircraft, a rotary wing aircraft, a lighter-than-air (LTA) craft, and an unmanned aerial vehicle (UAV).
- SUV autonomous underwater vehicle
- the power source/vehicle structural system 24 includes a molded, machined, extruded, or digitally printed interlocking modular structural element 36 having open ends.
- the structural element 36 may be made of aluminum, magnesium, polymers, or comparable formable metals and/or plastics.
- the structural element 36 has a rectangular cross section, but other polygonal or non-polygonal shapes may be used.
- An inside surface of the structural element 36 is shaped to receive whatever stored element 30 is to be received within the structural element 36 .
- the inside surface of the illustrated structural element 36 includes contours for receiving round/cylindrical battery cells, but could be configured for rectangular battery cells, or differently shaped contents.
- orthogonally adjacent outer surfaces of the structural element 36 include one or more locking slots 40 .
- the other orthogonally adjacent outer surfaces include locking protrusion ridges 44 that are configured to be received by the locking slots 40 of other structural elements 36 that are to be attached thereto.
- the locking protrusion ridges 44 may be slid into the slots 40 or snap fitted into the slots 40 .
- Other linking structures may be used for attaching adjacent structural elements 36 .
- the structural elements 36 allow for air cooling of the batteries or other contents.
- the structural elements 36 provide dedicated open spaces for airflow between battery cells down the entire length of the interior of the structural elements 36 .
- the structural element 36 may be capped and/or sealed at the open end(s).
- the cap or seal of the structural element 36 or the structural element 36 may include access ports for electrical leads, fluid, airflow, or the like.
- an environmental management unit 26 FIG. 1
- the interlocking modular structural elements 36 may be attached at their shortest sides ( FIGS. 4 and 5 ), at their longest sides ( FIGS. 6 and 7 ), at a shortest side of the one interlocking modular structural element 36 attached to the longest side of another interlocking modular structural element 36 ( FIGS. 8 and 9 ).
- the interlocking modular structural elements 36 and the locking structures a user may attach the interlocking modular structural elements 36 according to the application (i.e., vehicle or structure).
- the structural elements 36 include beveled corner edges 42 . Other shapes may be used at the corners, such as radius or notched.
- the structural elements 36 may be attached to each other such that the beveled corner edge 42 of one of the functional elements 36 is located adjacent the beveled corner edge 42 of the adjacently attached structural element 36 , thereby forming a V-shaped groove 50 .
- the V-shaped groove 50 is configured to receive an adhesive or a weld depending upon the type of material of the structural elements 36 .
- the adhesive/weld adds additional bonding between adjacently attached structural elements 36 .
- Adhesives may also be applied between the outer surfaces, the slots 40 , and/or the ridges 44 of adjacently attached structural elements 36 .
- the interlocking modular structural elements 36 may be formed into a chassis 82 for a vehicle 80 , such as, without limitation, a skateboard design.
- the strength of the interlocking modular structural elements 36 and the locking structures provide support for a body of the vehicle 80 .
- the chassis 82 may have portions of the structural elements 36 removed, such as a cutout 86 , for allowing components 90 of the vehicle 80 to pass from one side of the chassis 82 to another side of the chassis 82 .
- the components 90 may include grooves or protrusions similar to the locking slots 40 and the locking protrusion ridges 44 , thereby allowing the components 90 to be attached directly to the outer surfaces of the structural elements 36 of the chassis 82 .
- the interlocking modular structural elements 36 may be used in an aircraft 100 .
- the interlocking modular structural elements 36 may be formed to create a frame structure for components of the aircraft 100 .
- the interlocking modular structural elements 36 may form a frame structure 104 for a wing 100 . If the equipment 100 is using electric motors, such as propeller motors or ducted fan motors, the interlocking modular structural elements 36 may be used in place of traditional structural elements thereby offsetting the weight of batteries that will be inserted within the interlocking modular structural elements 36 .
- the interlocking modular structural elements 36 may be located in a wing or other airfoil at the open space on either side of lift thrust devices embedded in the wing or airfoil.
- the interlocking modular structural elements 36 may be used as to house batteries or fuel storage devices.
- the interlocking modular structural elements 36 may be round or rectangular in shape that could run the entire length of the wings and/or fuselage.
- a stored element 120 includes a plurality of individual storage devices 122 . As illustrated, the individual storage devices 122 are cylindrical and an inner surface of the structural element 36 is shaped to receive the stored element 120 and the plurality of the cylindrical storage devices 122 . Referring to FIGS.
- the stored element 120 is slidably received into the structural element 36 .
- longitudinal grooves 124 are located between some of the storage devices 122 for allowing for heating or cooling as performed by air to pass therebetween, for example.
- An apparatus comprising: a housing comprising: an outer surface; an inner surface; and at least one opened end; first attachment devices disposed at the outer surface; and second attachment devices disposed at the outer surface, the second attachment devices are configured to be removably attachable to the first attachment devices.
- the apparatus of F wherein: the first attachment devices are disposed on first and second orthogonally adjacent sides of the housing; and the second attachment devices are disposed on third and fourth orthogonally adjacent sides of the housing.
- a structural/storage system comprising: a plurality of storage elements, each of the storage elements comprising: a housing comprising: an outer surface; an inner surface; and at least one opened end; first attachment devices disposed at the outer surface; and second attachment devices disposed at the outer surface, wherein the second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
- J The system of I, wherein a cross-section of the plurality of storage elements is a polygon.
- M The system of any of K or L, wherein at least a portion of the storage elements are configured to receive a plurality of batteries within a cavity of the respective housing.
- N The system of any of I-M, wherein the housing further comprises a plurality of cooling channels between the plurality of batteries within the cavity.
- a system comprising: a load device; a power element configured to power the load device; and a plurality of storage elements, each of the storage elements comprising: a housing comprising: an outer surface; an inner surface; and at least one opened end; first attachment devices disposed at the outer surface; and second attachment devices disposed at the outer surface, wherein the second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
- T The system of R or S, wherein the load device comprises an electric motor, the power element comprises a plurality of batteries.
- instances in this specification where one element is “coupled” to another element can include direct and indirect coupling.
- Direct coupling can be defined as one element coupled to and in some contact with another element.
- Indirect coupling can be defined as coupling between two elements not in direct contact with each other but having one or more additional elements between the coupled elements.
- securing one element to another element can include direct securing and indirect securing.
- adjacent does not necessarily denote contact. For example, one element can be adjacent another element without being in contact with that element.
- the phrase “at least one of”, when used with a list of items, means different combinations of one or more of the listed items may be used and only one of the items in the list may be needed.
- the item may be a particular object, thing, or category.
- “at least one of” means any combination of items or number of items may be used from the list, but not all of the items in the list may be required.
- “at least one of item A, item B, and item C” may mean item A; item A and item B; item B; item A, item B, and item C; or item B and item C.
- “at least one of item A, item B, and item C” may mean, for example, without limitation, two of item A, one of item B, and ten of item C; four of item B and seven of item C; or some other suitable combination.
- first,” “second,” etc. are used herein merely as labels, and are not intended to impose ordinal, positional, or hierarchical requirements on the items to which these terms refer. Moreover, reference to, e.g., a “second” item does not require or preclude the existence of, e.g., a “first” or lower-numbered item, and/or, e.g., a “third” or higher-numbered item.
- a system, apparatus, structure, article, element, component, or hardware “configured to” perform a specified function is indeed capable of performing the specified function without any alteration, rather than merely having potential to perform the specified function after further modification.
- the system, apparatus, structure, article, element, component, or hardware “configured to” perform a specified function is specifically selected, created, implemented, utilized, programmed, and/or designed for the purpose of performing the specified function.
- “configured to” denotes existing characteristics of a system, apparatus, structure, article, element, component, or hardware which enable the system, apparatus, structure, article, element, component, or hardware to perform the specified function without further modification.
- a system, apparatus, structure, article, element, component, or hardware described as being “configured to” perform a particular function may additionally or alternatively be described as being “adapted to” and/or as being “operative to” perform that function.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Transmission Devices (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
Apparatuses and systems for more efficient construction and operations of a vehicle. A structural/storage system that includes a plurality of storage elements. Each of the storage elements includes a housing having an outer surface, an inner surface, and at least one opened end. The structural/storage system further includes first attachment devices disposed at the outer surface and second attachment devices disposed at the outer surface. The second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
Description
- This application claims the benefit of U.S. Provisional Patent Application Nos. 63/361,693, filed Jan. 14, 2022, and 63/361,792, filed Jan. 24, 2022, which are incorporated herein by reference.
- This disclosure relates generally to systems in need of storage and structural support.
- Vehicles include systems and structures that both add significant weight to the vehicle. In the case of an electric vehicle, the batteries can weigh over a couple of thousand pounds. Thus, along with all the other structural elements of a vehicle, the vehicle exhibits limited efficiency.
- Apparatuses are disclosed for more efficient operations of a vehicle. In one embodiment, the apparatus includes a housing having an outer surface, an inner surface, and at least one opened end. The apparatus also includes first attachment devices disposed at the outer surface and second attachment devices disposed at the outer surface. The second attachment devices are configured to be removably attachable to the first attachment devices.
- In another embodiment, a structural/storage system that includes a plurality of storage elements. Each of the storage elements includes a housing having an outer surface, an inner surface, and at least one opened end. The structural/storage system further includes first attachment devices disposed at the outer surface and second attachment devices disposed at the outer surface. The second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
- In still another embodiment, a system that includes a load device, a power element configured to power the load device, and a plurality of storage elements. Each of the storage elements includes a housing having an outer surface, an inner surface, and at least one opened end. The storage elements include first attachment devices disposed at the outer surface and second attachment devices disposed at the outer surface. The second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
- The described features, structures, advantages, and/or characteristics of the subject matter of the present disclosure may be combined in any suitable manner in one or more examples and/or implementations. In the following description, numerous specific details are provided to impart a thorough understanding of examples of the subject matter of the present disclosure. One skilled in the relevant art will recognize that the subject matter of the present disclosure may be practiced without one or more of the specific features, details, components, materials, and/or methods of a particular example or implementation. In other instances, additional features and advantages may be recognized in certain examples and/or implementations that may not be present in all examples or implementations. Further, in some instances, well-known structures, materials, or operations are not shown or described in detail to avoid obscuring aspects of the subject matter of the present disclosure. The features and advantages of the subject matter of the present disclosure will become more fully apparent from the following description and appended claims or may be learned by the practice of the subject matter as set forth hereinafter.
- In order that the advantages of the subject matter may be more readily understood, a more particular description of the subject matter briefly described above will be rendered by reference to specific examples that are illustrated in the appended drawings. Understanding that these drawings, which are not necessarily drawn to scale, depict only certain examples of the subject matter and are not therefore to be considered to be limiting of its scope, the subject matter will be described and explained with additional specificity and detail through the use of the drawings, in which:
-
FIG. 1 is a system block diagram of components of a vehicle, according to one or more examples of the present disclosure; -
FIG. 2 is a perspective view of a structural and storage element used in the vehicle ofFIG. 1 , according to one or more examples of the present disclosure; -
FIG. 3 is a cross-sectional view of the element ofFIG. 2 , according to one or more examples of the present disclosure; -
FIG. 4 is a perspective view of attached structural and storage elements used in the vehicle ofFIG. 1 , according to one or more examples of the present disclosure; -
FIG. 5 is a cross-sectional view of the elements ofFIG. 4 , according to one or more examples of the present disclosure; -
FIG. 6 is a perspective view of a stacked structural and storage elements used in the vehicle ofFIG. 1 , according to one or more examples of the present disclosure; -
FIG. 7 is a cross-sectional view of the elements ofFIG. 6 , according to one or more examples of the present disclosure; -
FIG. 8 is a perspective view of a stacked structural and storage elements used in the vehicle ofFIG. 1 , according to one or more examples of the present disclosure; -
FIG. 9 is a cross-sectional view of the elements ofFIG. 8 , according to one or more examples of the present disclosure; -
FIG. 10 is a perspective view of a vehicle with structural and storage elements, according to one or more examples of the present disclosure; -
FIG. 11 is a cross-sectional view of the vehicle ofFIG. 10 , according to one or more examples of the present disclosure; -
FIG. 12 is a perspective view of a portion of a vehicle with structural and storage elements, according to one or more examples of the present disclosure; -
FIG. 13 is a perspective view of a vehicle component attached to one of the structural and storage elements of the vehicle ofFIG. 12 , according to one or more examples of the present disclosure; -
FIG. 14 is a perspective view of an aircraft with a structural and storage system, according to one or more examples of the present disclosure; -
FIG. 15 is a cross-sectional view of a portion of the aircraft ofFIG. 14 , according to one or more examples of the present disclosure; -
FIG. 16 is a cross-sectional view of the structural and storage system used in the aircraft ofFIG. 14 , according to one or more examples of the present disclosure; -
FIG. 17 is a perspective view of a storage element, according to one or more examples of the present disclosure; -
FIG. 18 is a perspective view of the storage element ofFIG. 17 being received in a modular structural element, according to one or more examples of the present disclosure; -
FIG. 19 is a perspective view of the storage element ofFIG. 17 being received in a modular structural element, according to one or more examples of the present disclosure; -
FIG. 20 is a perspective view of the storage element ofFIG. 17 received within a modular structural element, according to one or more examples of the present disclosure; and -
FIG. 21 is a plan view of the storage element ofFIG. 17 received within a modular structural element, according to one or more examples of the present disclosure. - Reference throughout this specification to “one example,” “an example,” or similar language means that a particular feature, structure, or characteristic described in connection with the example is included in at least one example of the present disclosure. Appearances of the phrases “in one example,” “in an example,” and similar language throughout this specification may, but do not necessarily, all refer to the same example. Similarly, the use of the term “implementation” means an implementation having a particular feature, structure, or characteristic described in connection with one or more examples of the present disclosure, however, absent an express correlation to indicate otherwise, an implementation may be associated with one or more examples.
- Reference throughout this specification to “one embodiment” “an embodiment” or similar language means that a particular structure or characteristic feature described in connection with the embodiment is included in at least one embodiment of the disclosed invention. Furthermore, the described structures or characteristics of the invention may be combined in any suitable manner in one or more embodiments. In the following description, numerous specific details are provided to give a thorough understanding of embodiments of the disclosed invention. One skilled in the relevant art will recognize, however, that the invention may be practiced without one or more of the specific details, or with other methods, components, materials, and so forth. In other instances, well-known structures, materials, or operations are not shown or described in detail to avoid obscuring aspects of the invention.
- Exemplary apparatuses and systems, disclosed herein, include dual structural and storage devices that are used to provide storage and structural integrity.
- Referring to
FIG. 1 , in various embodiments, avehicle 20 includes aload device 22 and a power source/vehiclestructural system 24 that houses a stored element 30 (material (e.g., fuel) or device (e.g., batteries)). The power source/vehiclestructural system 24 provides secure housing for thestored element 30 and provides structural integrity for thevehicle 20. In various embodiments, thestored element 30 may be fuel, fuel cells, batteries, or any system component, not limited to a power source. Theload device 22 is any device that receives the stored element 30 (material) stored in the power source/vehiclestructural system 24 or electrical power/current produced by thestored element 30. - Given by way of non-limiting example, in various embodiments the
vehicle 20 may include a motor vehicle driven by wheels and/or tracks, such as, without limitation, an automobile, a truck, a sport utility vehicle (SUV), a van, and the like. Given by way of further non-limiting examples, in various embodiments thevehicle 20 may include a marine vessel such as, without limitation, a boat, a ship, a submarine, a submersible, an autonomous underwater vehicle (AUV), and the like. Given by way of further non-limiting examples, in various embodiments thevehicle 20 may include an aircraft such as, without limitation, a fixed wing aircraft, a rotary wing aircraft, a lighter-than-air (LTA) craft, and an unmanned aerial vehicle (UAV). - Referring to
FIGS. 2 and 3 , in various embodiments the power source/vehiclestructural system 24 includes a molded, machined, extruded, or digitally printed interlocking modularstructural element 36 having open ends. Thestructural element 36 may be made of aluminum, magnesium, polymers, or comparable formable metals and/or plastics. - In various embodiments, referring to
FIG. 3 , thestructural element 36 has a rectangular cross section, but other polygonal or non-polygonal shapes may be used. An inside surface of thestructural element 36 is shaped to receive whatever storedelement 30 is to be received within thestructural element 36. The inside surface of the illustratedstructural element 36 includes contours for receiving round/cylindrical battery cells, but could be configured for rectangular battery cells, or differently shaped contents. - In various embodiments, orthogonally adjacent outer surfaces of the
structural element 36 include one ormore locking slots 40. The other orthogonally adjacent outer surfaces include lockingprotrusion ridges 44 that are configured to be received by the lockingslots 40 of otherstructural elements 36 that are to be attached thereto. The lockingprotrusion ridges 44 may be slid into theslots 40 or snap fitted into theslots 40. Other linking structures may be used for attaching adjacentstructural elements 36. - In various embodiments, the
structural elements 36 allow for air cooling of the batteries or other contents. For example, thestructural elements 36 provide dedicated open spaces for airflow between battery cells down the entire length of the interior of thestructural elements 36. - In various embodiments, once the stored
element 30 is received within thestructural element 36, thestructural element 36 may be capped and/or sealed at the open end(s). The cap or seal of thestructural element 36 or thestructural element 36 may include access ports for electrical leads, fluid, airflow, or the like. In the example of batteries being sealed within thestructural element 36, an environmental management unit 26 (FIG. 1 ) may control environmental conditions, such as, without limitation, heating, cooling, or humidity, within thestructural elements 36 based on status of the contents (e.g., batteries). - Referring to
FIGS. 4-9 , in various embodiments, the interlocking modularstructural elements 36 may be attached at their shortest sides (FIGS. 4 and 5 ), at their longest sides (FIGS. 6 and 7 ), at a shortest side of the one interlocking modularstructural element 36 attached to the longest side of another interlocking modular structural element 36 (FIGS. 8 and 9 ). Using the interlocking modularstructural elements 36 and the locking structures (the lockingslots 30 and the blocking protrusion ridges 44) a user may attach the interlocking modularstructural elements 36 according to the application (i.e., vehicle or structure). - In various embodiments, referring to
FIGS. 3, 5, and 7 , thestructural elements 36 include beveled corner edges 42. Other shapes may be used at the corners, such as radius or notched. Thestructural elements 36 may be attached to each other such that thebeveled corner edge 42 of one of thefunctional elements 36 is located adjacent thebeveled corner edge 42 of the adjacently attachedstructural element 36, thereby forming a V-shapedgroove 50. The V-shapedgroove 50 is configured to receive an adhesive or a weld depending upon the type of material of thestructural elements 36. The adhesive/weld adds additional bonding between adjacently attachedstructural elements 36. Adhesives may also be applied between the outer surfaces, theslots 40, and/or theridges 44 of adjacently attachedstructural elements 36. - Referring to
FIGS. 10 and 11 , in various embodiments, the interlocking modularstructural elements 36 may be formed into achassis 82 for avehicle 80, such as, without limitation, a skateboard design. The strength of the interlocking modularstructural elements 36 and the locking structures provide support for a body of thevehicle 80. - In various embodiments, referring to
FIGS. 12 and 13 , thechassis 82 may have portions of thestructural elements 36 removed, such as acutout 86, for allowingcomponents 90 of thevehicle 80 to pass from one side of thechassis 82 to another side of thechassis 82. Thecomponents 90 may include grooves or protrusions similar to the lockingslots 40 and the lockingprotrusion ridges 44, thereby allowing thecomponents 90 to be attached directly to the outer surfaces of thestructural elements 36 of thechassis 82. - In various embodiments, referring to
FIGS. 14-16 , the interlocking modularstructural elements 36 may be used in anaircraft 100. In particular, the interlocking modularstructural elements 36 may be formed to create a frame structure for components of theaircraft 100. For example, the interlocking modularstructural elements 36 may form aframe structure 104 for awing 100. If theequipment 100 is using electric motors, such as propeller motors or ducted fan motors, the interlocking modularstructural elements 36 may be used in place of traditional structural elements thereby offsetting the weight of batteries that will be inserted within the interlocking modularstructural elements 36. - In various embodiments, referring to
FIGS. 17-21 , the interlocking modularstructural elements 36 may be located in a wing or other airfoil at the open space on either side of lift thrust devices embedded in the wing or airfoil. The interlocking modularstructural elements 36 may be used as to house batteries or fuel storage devices. The interlocking modularstructural elements 36 may be round or rectangular in shape that could run the entire length of the wings and/or fuselage. Referring toFIG. 17 , a storedelement 120 includes a plurality ofindividual storage devices 122. As illustrated, theindividual storage devices 122 are cylindrical and an inner surface of thestructural element 36 is shaped to receive the storedelement 120 and the plurality of thecylindrical storage devices 122. Referring toFIGS. 18-20 , the storedelement 120 is slidably received into thestructural element 36. Referring toFIG. 21 , once the storedelement 120 is fully received within thestructural element 36, longitudinal grooves 124 are located between some of thestorage devices 122 for allowing for heating or cooling as performed by air to pass therebetween, for example. - A. An apparatus comprising: a housing comprising: an outer surface; an inner surface; and at least one opened end; first attachment devices disposed at the outer surface; and second attachment devices disposed at the outer surface, the second attachment devices are configured to be removably attachable to the first attachment devices.
- B. The apparatus of A, wherein a cross-section of the housing is a polygon.
- C. The apparatus of any of A or B, wherein the housing is configured to provide structural support for a system.
- D. The apparatus of C, wherein the housing is configured to receive a plurality of batteries within a cavity.
- E. The apparatus of D, wherein the housing further comprises a plurality of cooling channels between the plurality of batteries within the cavity.
- F. The apparatus of any of A-E, wherein the housing comprises a rectangular cross section.
- G. The apparatus of F, wherein: the first attachment devices are disposed on first and second orthogonally adjacent sides of the housing; and the second attachment devices are disposed on third and fourth orthogonally adjacent sides of the housing.
- H. The apparatus of any of A-G, wherein the housing comprises beveled corners.
- I. A structural/storage system comprising: a plurality of storage elements, each of the storage elements comprising: a housing comprising: an outer surface; an inner surface; and at least one opened end; first attachment devices disposed at the outer surface; and second attachment devices disposed at the outer surface, wherein the second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
- J. The system of I, wherein a cross-section of the plurality of storage elements is a polygon.
- K. The system of any of I or J, wherein the plurality of storage elements are configured to provide structural support for an associated system.
- L. The system of K, wherein the associated system includes a vehicle.
- M. The system of any of K or L, wherein at least a portion of the storage elements are configured to receive a plurality of batteries within a cavity of the respective housing.
- N. The system of any of I-M, wherein the housing further comprises a plurality of cooling channels between the plurality of batteries within the cavity.
- O. The system of any of I-N, wherein the housing comprises a rectangular cross section.
- P. The system of P, wherein: the first attachment devices are disposed on first and second orthogonally adjacent sides of the housing; and the second attachment devices are disposed on third and fourth orthogonally adjacent sides of the housing.
- Q. The system of any of O or P, wherein the housing comprises beveled corners.
- R. A system comprising: a load device; a power element configured to power the load device; and a plurality of storage elements, each of the storage elements comprising: a housing comprising: an outer surface; an inner surface; and at least one opened end; first attachment devices disposed at the outer surface; and second attachment devices disposed at the outer surface, wherein the second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
- S. The system of R, wherein the storage elements are configured to provide structural support for the system.
- T. The system of R or S, wherein the load device comprises an electric motor, the power element comprises a plurality of batteries.
- With respect to the appended claims, those skilled in the art will appreciate that recited operations therein may generally be performed in any order. Also, although various operational flows are presented in a sequence(s), it should be understood that the various operations may be performed in other orders than those which are illustrated or may be performed concurrently. Examples of such alternate orderings may include overlapping, interleaved, interrupted, reordered, incremental, preparatory, supplemental, simultaneous, reverse, or other variant orderings, unless context dictates otherwise. Furthermore, terms like “responsive to,” “related to,” or other past-tense adjectives are generally not intended to exclude such variants, unless context dictates otherwise.
- In the above description, certain terms may be used such as “up,” “down,” “upper,” “lower,” “horizontal,” “vertical,” “left,” “right,” “over,” “under” and the like. These terms are used, where applicable, to provide some clarity of description when dealing with relative relationships. But, these terms are not intended to imply absolute relationships, positions, and/or orientations. For example, with respect to an object, an “upper” surface can become a “lower” surface simply by turning the object over. Nevertheless, it is still the same object. Further, the terms “including,” “comprising,” “having,” and variations thereof mean “including but not limited to” unless expressly specified otherwise. An enumerated listing of items does not imply that any or all of the items are mutually exclusive and/or mutually inclusive, unless expressly specified otherwise. The terms “a,” “an,” and “the” also refer to “one or more” unless expressly specified otherwise. Further, the term “plurality” can be defined as “at least two.” Moreover, unless otherwise noted, as defined herein a plurality of particular features does not necessarily mean every particular feature of an entire set or class of the particular features.
- Additionally, instances in this specification where one element is “coupled” to another element can include direct and indirect coupling. Direct coupling can be defined as one element coupled to and in some contact with another element. Indirect coupling can be defined as coupling between two elements not in direct contact with each other but having one or more additional elements between the coupled elements. Further, as used herein, securing one element to another element can include direct securing and indirect securing. Additionally, as used herein, “adjacent” does not necessarily denote contact. For example, one element can be adjacent another element without being in contact with that element.
- As used herein, the phrase “at least one of”, when used with a list of items, means different combinations of one or more of the listed items may be used and only one of the items in the list may be needed. The item may be a particular object, thing, or category. In other words, “at least one of” means any combination of items or number of items may be used from the list, but not all of the items in the list may be required. For example, “at least one of item A, item B, and item C” may mean item A; item A and item B; item B; item A, item B, and item C; or item B and item C. In some cases, “at least one of item A, item B, and item C” may mean, for example, without limitation, two of item A, one of item B, and ten of item C; four of item B and seven of item C; or some other suitable combination.
- Unless otherwise indicated, the terms “first,” “second,” etc. are used herein merely as labels, and are not intended to impose ordinal, positional, or hierarchical requirements on the items to which these terms refer. Moreover, reference to, e.g., a “second” item does not require or preclude the existence of, e.g., a “first” or lower-numbered item, and/or, e.g., a “third” or higher-numbered item.
- As used herein, a system, apparatus, structure, article, element, component, or hardware “configured to” perform a specified function is indeed capable of performing the specified function without any alteration, rather than merely having potential to perform the specified function after further modification. In other words, the system, apparatus, structure, article, element, component, or hardware “configured to” perform a specified function is specifically selected, created, implemented, utilized, programmed, and/or designed for the purpose of performing the specified function. As used herein, “configured to” denotes existing characteristics of a system, apparatus, structure, article, element, component, or hardware which enable the system, apparatus, structure, article, element, component, or hardware to perform the specified function without further modification. For purposes of this disclosure, a system, apparatus, structure, article, element, component, or hardware described as being “configured to” perform a particular function may additionally or alternatively be described as being “adapted to” and/or as being “operative to” perform that function.
- The present subject matter may be embodied in other specific forms without departing from its spirit or essential characteristics. The described examples are to be considered in all respects only as illustrative and not restrictive. All changes which come within the meaning and range of equivalency of the claims are to be embraced within their scope.
Claims (20)
1. An apparatus comprising:
a housing comprising:
an outer surface;
an inner surface; and
at least one opened end;
first attachment devices disposed at the outer surface; and
second attachment devices disposed at the outer surface, the second attachment devices are configured to be removably attachable to the first attachment devices.
2. The apparatus of claim 1 , wherein a cross-section of the housing is a polygon.
3. The apparatus of claim 1 , wherein the housing is configured to provide structural support for a system.
4. The apparatus of claim 3 , wherein the housing is configured to sealably receive a plurality of batteries within a cavity.
5. The apparatus of claim 4 , wherein the housing further comprises a plurality N of cooling channels between the plurality of batteries within the cavity.
6. The apparatus of claim 1 , wherein the housing comprises a rectangular cross section.
7. The apparatus of claim 6 , wherein:
the first attachment devices are disposed on first and second orthogonally adjacent sides of the housing; and
the second attachment devices are disposed on third and fourth orthogonally adjacent sides of the housing.
8. The apparatus of claim 6 , wherein the housing comprises beveled corners configured to receive an adhesive.
9. A structural/storage system comprising:
a plurality of storage elements, each of the storage elements comprising:
a housing comprising:
an outer surface;
an inner surface; and
at least one opened end;
first attachment devices disposed at the outer surface; and
second attachment devices disposed at the outer surface,
wherein the second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
10. The system of claim 9 , wherein a cross-section of the plurality of storage N elements is a polygon.
11. The system of claim 10 , wherein the plurality of storage elements are configured to provide structural support for an associated system.
12. The system of claim 11 , wherein the associated system includes a vehicle.
13. The system of claim 12 , wherein at least a portion of the storage elements are configured to receive a plurality of batteries within a cavity of the respective housing.
14. The system of claim 13 , wherein the housing further comprises a plurality of cooling channels between the plurality of batteries within the cavity.
15. The system of claim 9 , wherein the housing comprises a rectangular cross section.
16. The system of claim 15 , wherein:
the first attachment devices are disposed on first and second orthogonally adjacent sides of the housing; and
the second attachment devices are disposed on third and fourth orthogonally adjacent sides of the housing.
17. The system of claim 15 , wherein the housing comprises beveled corners configured to receive an adhesive.
18. A system comprising:
a load device;
N a power element configured to power the load device; and
a plurality of storage elements, each of the storage elements comprising:
a housing comprising:
an outer surface;
an inner surface; and
at least one opened end;
first attachment devices disposed at the outer surface; and
second attachment devices disposed at the outer surface,
wherein the second attachment devices of a first one of the plurality of storage elements are configured to be removably attachable to the first attachment devices of a second one of the plurality of storage elements.
19. The system of claim 18 , wherein the storage elements are configured to provide structural support for the system.
20. The system of claim 18 , wherein the load device comprises an electric motor, the power element comprises a plurality of batteries.
Priority Applications (1)
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US18/098,041 US20230226900A1 (en) | 2022-01-14 | 2023-01-17 | Dual structural and storage apparatus |
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US18/098,016 Pending US20230331381A1 (en) | 2022-01-14 | 2023-01-17 | Aircraft with lift thrust system concealed in an airfoil |
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US2646945A (en) * | 1950-09-05 | 1953-07-28 | John A Perry | Airplane wing structure |
US2936969A (en) * | 1955-06-08 | 1960-05-17 | Rolls Royce | Jet sustained and propelled aircraft |
US3752417A (en) * | 1972-06-23 | 1973-08-14 | P Lagace | Aircraft using lifting fans |
US5320305A (en) * | 1992-07-22 | 1994-06-14 | Lockheed Corporation | Propulsion system for an aircraft providing V/STOL capability |
US9714090B2 (en) * | 2015-06-12 | 2017-07-25 | Sunlight Photonics Inc. | Aircraft for vertical take-off and landing |
US10737797B2 (en) * | 2017-07-21 | 2020-08-11 | General Electric Company | Vertical takeoff and landing aircraft |
EP3470332B1 (en) * | 2017-10-13 | 2020-04-22 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A multirotor aircraft with an airframe and at least one wing |
US11142308B2 (en) * | 2018-12-29 | 2021-10-12 | Bogdan Tudor Bucheru | Semi-open fluid jet VTOL aircraft |
US11279479B2 (en) * | 2020-03-28 | 2022-03-22 | Textron Innovations Inc. | Fluidic yaw control systems for use in hover |
US11001377B1 (en) * | 2020-05-21 | 2021-05-11 | Horizon Aircraft Inc. | Aircraft airfoil and aircraft having the same |
US11548621B1 (en) * | 2021-11-04 | 2023-01-10 | Horizon Aircraft Inc. | Aircraft airfoil having an internal thrust unit, and aircraft having the same |
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