Method and apparatus for transporting wind turbine blades
10024299 ยท 2018-07-17
Assignee
Inventors
Cpc classification
B60P3/40
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/49764
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
F03D13/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T29/49815
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
Y10T29/49826
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
Y02E10/72
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
Y10T29/49947
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
International classification
B60P3/40
PERFORMING OPERATIONS; TRANSPORTING
F03D13/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A system for transporting wind turbine blades includes a frame assembly for retaining a set one or more wind turbine blades and a plurality of inflatable devices coupled to the frame assembly.
Claims
1. A method of transporting a set of one or more wind turbine blades, comprising: releasably attaching the set of one or more wind turbine blades to a frame assembly; supporting a portion of the set of one or more wind turbine blades by inflating a plurality of inflatable devices coupled to the frame assembly determining if leakage has occurred for the plurality of inflatable devices during transport of the set of one or more wind turbine blades; and re-inflating the plurality of inflatable devices from a source in response to a determination that leakage has occurred for the plurality of inflatable devices during transport of the set of one or more wind turbine blades.
2. The method according to claim 1, wherein the releasably attaching the set of one or more wind turbine blades to the frame assembly comprises: supporting at least a portion of the one or more wind turbine blades with a flexible tension member.
3. The method according to claim 1, further comprising: releasably attaching a mechanical fastener to an end of one of the one or more wind turbine blades via a support bracket.
4. The method according to claim 1, further comprising: releasably attaching an enclosure component to the frame assembly to form an enclosure.
5. The method according to claim 1, further comprising: releasably attaching the frame assembly to a support structure, wherein the support structure is coupled to a mode of transportation.
6. The method according to claim 1, further comprising: detaching the frame assembly from the support structure; detaching an enclosure component from the frame assembly; detaching a mechanical fastener attaching an end of one of the one or more wind turbine blades to a support bracket; deflating the plurality of inflatable devices; and detaching the set of one or more wind turbine blades from the frame assembly.
Description
DESCRIPTION OF THE DRAWINGS
(1) The novel features believed characteristic of the invention are set forth in the appended claims. However, the invention itself, as well as a preferred mode of use, and further objectives and advantages thereof, will best be understood by reference to the following detailed description when read in conjunction with the accompanying drawings, wherein:
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(8) While the assembly and method of the present application is susceptible to various modifications and alternative forms, specific embodiments thereof have been shown by way of example in the drawings and are herein described in detail. It should be understood, however, that the description herein of specific embodiments is not intended to limit the invention to the particular embodiment disclosed, but on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the spirit and scope of the process of the present application as defined by the appended claims.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
(9) In the interest of clarity, not all features of an actual implementation are described in this specification. It will of course be appreciated that in the development of any such actual embodiment, numerous implementation-specific decisions will be made to achieve the developer's specific goals, such as compliance with system-related and business-related constraints, which will vary from one implementation to another. Moreover, it will be appreciated that such a development effort might be complex and time-consuming but would nevertheless be a routine undertaking for those of ordinary skill in the art having the benefit of this disclosure.
(10) Referring to
(11) Frame assemblies 202-208 include inflatable devices for supporting and securing blades 210 and 212 and tower section 214. The inflatable devices are not shown in
(12) Referring to
(13) System 300 may also include enclosure component 318, which may be referred to as top rack 318. Bottom rack 302 may be used without top rack 318 when an enclosure is not required, such as when transporting a tower section. For example, bottom rack 302 may be substantially similar to either of frame assemblies 206 and 208 in
(14) Racks 302 and 318 may be connected by connectors 320-326. For example, connectors 320-326 may be standard IBC's 320-326 and corner castings similar to those used to connect stacked containers in intermodal transportation. Although
(15) Inflatable devices 308-316, or air bags 308-316, may be attached to bottom rack 302 and/or top rack 318. Air bags 308-316 may be inflated to the proper pressure and size to secure the various shapes of components to be protected within frame assembly 302 or an enclosure. The shape of air bags 308-316 may be pre-formed to specific shapes when inflated. The shape of air bags 308-316 may also be variable when inflated, depending on requirements of the shape of the components to be secured within frame assembly 302 or an enclosure. Air bags 308-316 may be used as a self-sustaining protective cradle or pillow surrounding the particular shape of the components being secured for transportation movement. Air bags 308-316 may be inflatable to fit all sizes and shapes of blades and tower components. In one embodiment, differences in sizes and shapes of blades may be accommodated by the degree of inflation for air bags 308-316. Air bags 308-316 may provide sufficient pressure to properly restrain a blade, tower section, or other component while providing a flexible and safe means of cradling the components without the use of specific mechanical fasteners. Air bags 308-316 have more flexibility than mechanical fasteners to accept an array of different shapes and sized components.
(16) Furthermore, inflatable devices 308-316 may be able to accept inflation from an outside source if leakage were to occur. For example, air could be provided by the air brake systems on trains, trucks, and other vehicles. Additionally, system 300 may also include an integral inflation source (not shown), which may enable inflation of inflatable devices 308-316 prior to loading inflatable devices 308-316 on a vehicle that provides an outside inflation source.
(17) Bottom rack 302 may be coupled to support structure 328, which may be referred to as support plate 328, with a plurality of twist-lock devices (not shown), such as IBC's. Support plate 328 may be coupled to a railcar, such as railcars 216 and 218 in
(18) Referring now to
(19) Referring now to
(20) Referring now to
(21) A method for transporting blades 106 is now described. At a transportation point of origin, blades 304 and 306 are attached to frame assembly 302. Blades 416 and 418 may be supported with flexible tension members 412 and 414. Deflated inflatable devices 402-410 are inflated to become inflatable devices 308-316 supporting a portion of blades 304 and 306. For additional support, mechanical fasteners 510 and 512 may be attached to an end of blade 514 via support brackets 506 and 508. Enclosure component 318 may be attached to frame assembly 302 to form an enclosure. Frame assembly 302 is attached to support structure 328, and support structure 328 is coupled to a mode of transportation, such as a railcar, a truck, a ship, or another vehicle. At this step in the method, a turbine blade is securely supported and ready for transportation.
(22) During transport of a turbine blade, a determination may be made whether leakage has occurred for the inflatable devices. If leakage has occurred, the inflatable devices may be re-inflated from a source associated with the mode of transportation, such as from the air brakes for a truck or a railcar, or from an integral source of inflation.
(23) At a transportation point of destination, steps that correspond to the steps performed at the transportation point of origin may be performed in a reverse order. Frame assembly 302 is detached from support structure 328. Enclosure component 318 is detached from frame assembly 302. Mechanical fasteners 510 and 512 attached to support brackets 506 and 508 are detached from an end of blade 514. Inflatable devices 308-316 are deflated to become deflated inflatable devices 402-410. Blades 416 and 418 are lifted from flexible tension members 412 and 414. Of course, the steps in the method may be performed in a different order. Although systems and methods have been described with respect to transporting large wind turbine blades, it should be understood that the systems and the methods may be used to transport other lengthy objects, such as highway overpass beams.
(24) It is evident by the foregoing description that the subject application has significant benefits and advantages, including: (1) air bags enable one system to be used for different sizes of components; (2) air bags easily conform to different shaped components; (3) air bags can be used in many modes of transportation; (4) air bags reduce costs required for the redesigning of shipping components when blade designs change; (5) air bags offer better protection of transported components; and (6) air bags enable simple installation and removal processes for components.
(25) The particular embodiments disclosed above are illustrative only, as the invention may be modified and practiced in different but equivalent manners apparent to those skilled in the art having the benefit of the teachings herein. It is therefore evident that the particular embodiments disclosed above may be altered or modified, and all such variations are considered within the scope and spirit of the invention. Accordingly, the protection sought herein is as set forth in the description. Although the present invention is shown in a limited number of forms, it is not limited to just these forms, but is amenable to various changes and modifications without departing from the spirit thereof.