SYSTEM OF INTEGRATED PASSAGEWAYS IN A CARBON FIBER BOOM AND METHOD THEREOF
20200404867 ยท 2020-12-31
Inventors
Cpc classification
A01M7/0042
HUMAN NECESSITIES
A01C23/04
HUMAN NECESSITIES
B32B2250/20
PERFORMING OPERATIONS; TRANSPORTING
A01G25/09
HUMAN NECESSITIES
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B2410/00
PERFORMING OPERATIONS; TRANSPORTING
B05B1/20
PERFORMING OPERATIONS; TRANSPORTING
B32B3/20
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/106
PERFORMING OPERATIONS; TRANSPORTING
B29C70/446
PERFORMING OPERATIONS; TRANSPORTING
B05B1/14
PERFORMING OPERATIONS; TRANSPORTING
B32B3/08
PERFORMING OPERATIONS; TRANSPORTING
Y10T137/8807
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
B32B3/30
PERFORMING OPERATIONS; TRANSPORTING
B05B1/083
PERFORMING OPERATIONS; TRANSPORTING
International classification
A01G25/09
HUMAN NECESSITIES
A01C23/04
HUMAN NECESSITIES
A01M7/00
HUMAN NECESSITIES
B05B1/08
PERFORMING OPERATIONS; TRANSPORTING
B05B1/14
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A spray boom includes a body having a length defined a first end and a second end thereof. The body is formed by a plurality of layers of composite material adapted to be molded together to form an inner surface and an outer surface. A hollow cavity is defined in the body internally of the inner surface, and a channel is formed in the body between the inner surface and the outer surface. The channel extends along the length and is defined between the first end and the second end.
Claims
1. A method of manufacturing a carbon fiber boom, the method comprising: providing a first boom mold and a second boom mold; placing at least a first layer of composite material in the first boom mold and the second boom mold; adding at least a second layer of composite material in the first boom mold and the second boom mold; forming a first elongated channel in between the first layer and the second layer of composite material in one of the first boom mold and the second boom mold; pressurizing the first and second boom molds to compress the first and second layers of composite material together; assembling the first and second boom molds together to form a single mold assembly; and applying heat pressure to the single mold assembly to form the carbon fiber boom.
2. The method of claim 1, further comprising forming a second elongated channel in between the first and second layers of composite material at a location spaced circumferentially from the first elongated channel.
3. The method of claim 1, wherein forming the first elongated channel comprises inserting a hollow tube between the first and second layers of composite material.
4. The method of claim 1, further comprising: depositing a plurality of layers of composite material in the first and second boom molds; and forming one or more channels between any two of the plurality of layers of composite material.
5. The method of claim 4, wherein the plurality of layers includes a third layer of composite material and a fourth layer of composite material, and wherein the third and fourth layers of composite material are different from the first and second layers of composite material.
6. The method of claim 1, wherein pressurizing the first and second boom molds comprises compressing the first and second layers of composite material together and dispersing resins.
7. The method of claim 1, further comprising: adding layers of composite material to the first and second boom molds after pressurizing the first and second boom molds; and pressurizing the added layers to compress the added layers together.
8. The method of claim 1, further comprising routing a member through the first elongated channel after applying heat pressure to the single mold assembly, wherein the member electrically, hydraulically, or pneumatically couples a first end of the carbon fiber boom to a second end thereof.
9. The method of claim 1, further comprising fabricating a thickness of the carbon fiber boom between an inner surface and outer surface thereof, wherein the thickness is greater at a location of the first elongated channel than at a location free of the channel.
10. A method of manufacturing a carbon fiber boom, the method comprising: placing a plurality of layers of composite material in one or more boom molds, wherein the plurality of layers of composite material include an outermost layer, an innermost layer, and a first intermediate layer arranged between the outermost layer and the innermost layer; forming a first elongated channel in between the outermost layer and the first intermediate layer in the one or more boom molds; and applying pressure to the one or more boom molds to compress the plurality of layers of composite material together to form the carbon fiber boom.
11. The method of claim 10, further comprising forming a second elongated channel in between the outermost layer and the first intermediate layer that is spaced from the first elongated channel.
12. The method of claim 11, further comprising forming a third elongated channel in between the outermost layer and the first intermediate layer that is spaced from the first and second elongated channels.
13. The method of claim 12, further comprising forming a fourth elongated channel in between the outermost layer and the first intermediate layer that is spaced from the first, second, and third elongated channels.
14. The method of claim 13, further comprising: forming a first thickness between the outermost layer and the innermost layer at a location absent the first elongated channel, the second elongated channel, the third elongated channel, and the fourth elongated channel; forming a second thickness between the outermost layer and the innermost layer at a location of the first elongated channel; forming a third thickness between the outermost layer and the innermost layer at a location of the second elongated channel; forming a fourth thickness between the outermost layer and the innermost layer at a location of the third elongated channel; and forming a fifth thickness between the outermost layer and the innermost layer at a location of the fourth elongated channel.
15. The method of claim 14, wherein each of the second thickness, the third thickness, the fourth thickness, and the fifth thickness is at least 1.5 times greater than the first thickness.
16. The method of claim 15, wherein each of the second thickness, the third thickness, the fourth thickness, and the fifth thickness is at least 2.0 times greater than the first thickness.
17. The method of claim 11, wherein the plurality of layers of composite material include a second intermediate layer arranged between the first intermediate layer and the innermost layer and a third intermediate layer arranged between the second intermediate layer and the innermost layer.
18. A method of manufacturing a one-piece carbon fiber boom, the method comprising: arranging a plurality of layers of composite material in one or more boom molds, wherein the plurality of layers of composite material include an outermost layer, an innermost layer, and a first intermediate layer positioned between the outermost layer and the innermost layer; forming a first elongated channel in between the outermost layer and the first intermediate layer in the one or more boom molds; and applying pressure to the one or more boom molds to compress the plurality of layers of composite material together to form the one-piece carbon fiber boom.
19. The method of claim 18, wherein the plurality of layers of composite material include a second intermediate layer arranged between the first intermediate layer and the innermost layer and a third intermediate layer arranged between the second intermediate layer and the innermost layer.
20. The method of claim 18, further comprising: forming a second elongated channel in between the outermost layer and the first intermediate layer that is spaced from the first elongated channel; forming a third elongated channel in between the outermost layer and the first intermediate layer that is spaced from the first and second elongated channels; and forming a fourth elongated channel in between the outermost layer and the first intermediate layer that is spaced from the first, second, and third elongated channels.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] The above-mentioned aspects of the present disclosure and the manner of obtaining them will become more apparent and the disclosure itself will be better understood by reference to the following description of the embodiments of the disclosure, taken in conjunction with the accompanying drawings, wherein:
[0014]
[0015]
[0016]
[0017]
[0018]
[0019] Corresponding reference numerals are used to indicate corresponding parts throughout the several views.
DETAILED DESCRIPTION
[0020] For the purposes of promoting an understanding of the principles of the present disclosure, reference will now be made to the embodiments described herein and illustrated in the drawings and specific language will be used to describe the same. It will nevertheless be understood that no limitation of the scope of the present disclosure is thereby intended, such alterations and further modifications in the illustrated devices and methods, and such further applications of the principles of the present disclosure as illustrated therein being contemplated as would normally occur to one skilled in the art to which the present disclosure relates.
[0021] Referring to
[0022] A fixed or floating center frame 114 is coupled to a front or a rear of the main frame 102. In
[0023] A plurality of spray nozzles 116 can be mounted along a fluid distribution pipe or spray pipe (not shown) that is mounted to the spray boom assembly 112 and fluidly coupled to the tank 110. Each nozzle 116 can have multiple spray outlets, each of which conducts fluid to a same-type or different-type of spray tip. The nozzles 116 on the spray boom assembly 112 can be divided into boom frames or wing structures such as 124, 126, 128, 130, 132, 134, and 136 (or collectively spray section(s)). In
[0024] The spray boom assembly 112 may be further divided into a first or left boom 120 and a second or right boom 122. In
[0025] As shown in
[0026] In a conventional spray boom assembly, a tilt actuator may be provided for tilting each boom with respect to the center frame. In
[0027] Referring to
[0028] In
[0029] The first boom frame 202 may include a yoke or other means for coupling to a center frame or other structure of a boom system. Moreover, the first boom frame 202 is shown having an ear or protruding portion 214 for pivotally coupling to an ear or protruding portion 216 of the second boom frame 204. As shown, a fastener or other coupling means may pivotally couple the protruding portions to one another to permit pivotal movement therebetween. The same type of design or structure may be incorporated to allow pivotal movement between the second boom frame 204 and the third boom frame 206.
[0030] As shown in
[0031] If the cable is an electrical cable or wire, it may allow for electrically coupling a sensor (not shown) or other electrical component on the different boom frames to a controller or other electrical component. For example, there may be a position sensor or global positioning sensor located at the end of the third boom frame 206. This sensor may be in communication with a controller for controlling the position and movement of the boom 200. Since the carbon boom 200 in
[0032] For purposes of this disclosure, a linking member or coupling member may be used throughout for describing hydraulically, electrically, or pneumatically coupling one end of the boom frame to the other end. In
[0033] Although not shown in
[0034] While the coupling of a plurality of boom frames is shown in
[0035] As described above, the carbon fiber boom frame 300 may be formed by a plurality of layers. Here, the boom frame 300 may be formed by a first layer 308, a second layer 310, a third layer 312, a fourth layer 314, and a fifth layer 316. The first layer 308 may be the innermost layer of material forming the boom frame 300, whereas the fifth layer 316 may be the outermost layer of material. While only five layers are shown and described with respect to this embodiment, it is within the scope of this disclosure that the carbon fiber boom frame 300 may be formed by any number of layers necessary to achieve a desired thickness, t.sub.1. The layers may, for example, be carbon fiber or fiberglass sheets or layers of material. As will be describe below, the layers or sheets may form the carbon fiber boom via a hand-laying process or other known process. Each layer may include the same material as the other layers, or in some embodiments, one or more layers may comprise a different type of material from the other layers. Once the layers are stacked upon one another, the thickness, t.sub.1, of the boom frame 300 is formed.
[0036] In
[0037] A second passageway or channel 320 may be formed at another location in the boom frame 300. This second passageway or channel 320 may also be formed along the entire length of the boom frame 300, and as shown, a linking member 322 (e.g., wiring, piping, or other electrical, hydraulic or pneumatic lines) may be routed through the passageway or channel 320. In one example, the linking member 322 may include a hydraulic hose that supplies a liquid substance from a tank to one or more nozzles located on the boom frame 300. In another example, the linking member 322 may include an electrical wire or cable that electrically couples a sensor to a main controller for controlling a boom height. Other examples are possible with this configuration.
[0038] Moreover, while only two passageways are shown, it is within the scope of this disclosure that any number of passageways or channels may be formed inbetween layers of the boom frame 300. In
[0039] As also shown in
[0040] In
[0041] In
[0042] As shown in
[0043] Similar to the boom frame 300 of
[0044] In
[0045] It is also shown that the thickness of the boom frame 400 may increase at the location of each channel or passageway such that a bulge may be formed. In
[0046] The thickness of the boom frame may also be greater at the locations of the second channel 420, the third channel 434, and the fourth channel 436. For instance, a second bulge 428 may be formed by the second channel 420, a third bulge 430 may be formed by the third channel 434, and a fourth bulge 432 may be formed by the fourth channel 436. The thickness, t.sub.3, at the second channel 420, the thickness, t.sub.4, at the third channel 434, and the thickness, t.sub.5, at the fourth channel 436 may be greater than the overall thickness, t.sub.1, of the boom frame. In one non-limiting example, the thickness at each channel may be at least 1.5 to 2.0 times the thickness of the overall thickness.
[0047] As described above, each of the boom frames shown in
[0048] It is within the scope of this disclosure that there may be any number of passageways or channels formed in the boom frame. Each channel and passageway may be spaced from one another to provide structural integrity to the carbon fiber boom.
[0049] Turning to
[0050] In a first block 502 of
[0051] In a third block 506, a first outer layer or layers may be deposited or laid in one or both molds. While a hand-laying process is described herein, there may be other methods for placing the layers of material in the molds. Any known process may be used. Once the first outer layer or layers is placed in the mold(s), the method 500 may advance to block 508 where a cavity or channel may be formed. Here, the layers may be rounded for forming the channel or passageway. Alternatively, or in addition, in block 510 a hollow PVC or composite tube or pipe may be integrated between layers. A wire or cable may be later routed through the hollow tube or pipe. Additional layers may be added to the mold in block 512 on top of first laid layers. The channels or passageways formed in block 508 may be formed the entire length of the boom mold. Moreover, each channel or passage formed inbetween layers may be spaced from adjacent channels or passages by a desired distance to provide structural integrity to the boom.
[0052] Once block 512 is completed, the method may advance to block 514 where the molds may be vacuum-pressurized in an enclosure. In one example, each mold may be placed in a bag and then vacuum-pressurized. During this process, the layers may be compressed together and resins dispersed between layers in block 516. The bag or enclosure may be removed after block 516 is executed. In block 518, additional layers may be added to each mold, and blocks 514 and 516 may be repeated as necessary.
[0053] Once the first and second molds have the desired amount of layers, the method 500 advances to block 520 where the molds are assembled to one another to form a single mold assembly. The single mold assembly may be vacuum-pressurized in block 522. The entire mold may also be placed in an Autoclave in block 524 and heat pressure is applied to the mold. The heat pressure may further join the two molds together. After block 524 is completed, the method 500 may advance to block 526 where the molds are removed from the newly formed boom structure. The formed boom structure in block 526 may have a shape of the two molds, and further curing and final processing may be executed in block 528 to form the final carbon fiber boom.
[0054] The carbon fiber boom is now formed with the integrated channels or passageways formed between the stacked layers of composite material. Although not shown in
[0055] In view of the above, a carbon fiber boom or boom frame may be manufactured with integrated channels or passages to allow cables, hoses, wires, tubes, and the like to pass through the internal channels without being routed and coupled externally to the boom. The addition of jumper cables, wires, or piping may be necessary to couple adjacent boom frames to one another, and an example of this is shown in
[0056] While exemplary embodiments incorporating the principles of the present disclosure have been described herein, the present disclosure is not limited to such embodiments. Instead, this application is intended to cover any variations, uses, or adaptations of the disclosure using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this disclosure pertains.