VACUUM EXCAVATION FOR LOCAL TRANSMISSION SYSTEM AND METHOD
20240279903 ยท 2024-08-22
Inventors
- William Zbytniewski (Hauppauge, NY, US)
- Ali Asmari (Selden, NY, US)
- G. Gregory Penza (Old Field, NY, US)
Cpc classification
E02F3/8825
FIXED CONSTRUCTIONS
E02F3/8891
FIXED CONSTRUCTIONS
E21B7/18
FIXED CONSTRUCTIONS
International classification
Abstract
A system and a method for vacuum excavation of local transmission are provided. The system for vacuum excavation of local transmission may include an end effector coupled to a vacuum hose. The end effector may include a manifold coupled to one or more valves and one or more pipes, each coupled to one of the one or more valves. The excavator head may include a nozzle array coupled to the one or more pipes, wherein the nozzle array may include one or more nozzles, each coupled to one of the one or more pipes. The one or more valves may be controlled to actuate individually, as a subset, or collectively, thus changing an air pattern exhausted from the nozzles.
Claims
1. A system for vacuum excavation of local transmission, comprising: an end effector coupled to a vacuum hose; the end effector comprising: a manifold coupled to one or more valves; one or more pipes coupled to the one or more valves; and an excavator head including a nozzle array coupled to the one or more pipes, wherein the nozzle array includes one or more nozzles, each coupled to a pipe of the one or more pipes.
2. The system of claim 1, wherein the manifold further comprises a top plate coupled to a bottom plate.
3. The system of claim 2 further comprising: an inlet coupled to the top plate of the manifold; and the one or more valves each being coupled to the bottom plate of the manifold.
4. The system of claim 3 further comprising: a pressure regulator coupled to the manifold.
5. The system of claim 3, further comprising: a channel within the bottom plate of the manifold, wherein the channel is designed to direct air received from the inlet.
6. The system of claim 1, wherein the one or more valves are provided in a form of a pilot solenoid valve.
7. The system of claim 1, wherein the one or more valves are provided in a form of an air logic control valve.
8. The system of claim 1, wherein the one or more nozzles are each configured to exhaust air at a supersonic speed.
9. The system of claim 1, wherein the one or more valves are configured such that only one nozzle of the one or more nozzles exhausts air at one time.
10. The system of claim 1, wherein the one or more valves are configured such that only two nozzles of the one or more nozzles exhausts air at one time.
11. The system of claim 10, wherein the two nozzles are positioned opposite from each other on the nozzle array.
12. A method for vacuum excavation of local transmission comprising: providing one or more nozzles in a form of a nozzle array; providing one or more valves, wherein each of the one or more nozzles is coupled to a respective valve of the one or more valves; actuating the one or more valves such that air is exhausted from the one or more nozzles, wherein the air agitates material to be excavated; and providing suction through a vacuum hose to vacuum the agitated material.
13. The method of claim 12, wherein a single valve of the one or more valves is actuated at a time.
14. The method of claim 12, wherein two valves of the one or more valves is actuated at a time.
15. The method of claim 12 further comprising: providing a delay between actuating a first set of the one or more valves and actuating a second set of the one or more valves.
16. The method of claim 12 further comprising: providing a delay between actuating a first valve of the one or more valves and actuating a second valve of the one or more valves.
17. A system for vacuum excavation of local transmission, comprising: an end effector coupled to a vacuum hose, the end effector comprising: an inlet coupled to a top plate of a manifold; one or more valves coupled to a bottom plate of the manifold; one or more pipes each coupled to a valve of the one or more valves; and an excavator head including a nozzle array, wherein the nozzle array includes one or more nozzles, each coupled to a pipe of the one or more pipes.
18. The system of claim 17, further comprising a pressure regulator coupled to the bottom plate of the manifold.
19. The system of claim 17, wherein the one or more nozzles further comprise: a converging portion of a nozzle provided between a first end of the nozzle and a throat portion of the nozzle; and a diverging portion of the nozzle provided between a second end of the nozzle and the throat portion of the nozzle.
20. The system of claim 19, wherein the converging portion has a first diameter at the first end of the nozzle and a second diameter at the throat portion of the nozzle, wherein the first diameter is larger than the second diameter; and wherein the diverging portion of the nozzle has a third diameter at the throat portion of the nozzle and a fourth diameter and the second end of the nozzle, wherein the third diameter is smaller than the fourth diameter.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0016] The accompanying drawings, which are incorporated in and form a part of this specification, illustrate embodiments of the invention and, together with the description, serve to explain the principles of embodiments of the invention:
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[0031] Before explaining the disclosed embodiment of the present invention in detail, it is to be understood that the invention is not limited in its application to the details of the particular arrangement shown, since the invention is capable of other embodiments. Exemplary embodiments are illustrated in referenced figures of the drawings. It is intended that the embodiments and figures disclosed herein are to be considered illustrative rather than limiting. Also, the terminology used herein is for the purpose of description and not for limitation.
DETAILED DESCRIPTION
[0032] The following discussion is presented to enable a person skilled in the art to make and use embodiments of the invention. Various modifications to the illustrated embodiments will be readily apparent to those skilled in the art, and the generic principles herein can be applied to other embodiments and applications without departing from embodiments of the invention. Thus, embodiments of the invention are not intended to be limited to embodiments shown, but are to be accorded the widest scope consistent with the principles and features disclosed herein. The following detailed description is to be read with reference to the figures, in which like elements in different figures have like reference numerals. The figures, which are not necessarily to scale, depict selected embodiments and are not intended to limit the scope of embodiments of the invention. Skilled artisans will recognize the examples provided herein have many useful alternatives and fall within the scope of embodiments of the invention.
[0033] Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the attached drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein are for the purpose of description and should not be regarded as limiting. For example, the use of including, comprising, or having and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items.
[0034] As used herein, unless otherwise specified or limited, the terms mounted, connected, supported, and coupled and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, unless otherwise specified or limited, connected and coupled are not restricted to physical or mechanical connections or couplings.
[0035] As used herein, unless otherwise specified or limited, at least one of A, B, and C, and similar other phrases, are meant to indicate A, or B, or C, or any combination of A, B, and/or C. As such, this phrase, and similar other phrases can include single or multiple instances of A, B, and/or C, and, in the case that any of A, B, and/or C indicates a category of elements, single or multiple instances of any of the elements of the categories A, B, and/or C.
[0036] As shown in
[0037] The VELTS system 100 may further include an end effector 300 disposed at a first end thereof and an excavator head 400 disposed at a second end thereof. The end effector 300 may be provided on and circumscribe an exterior of the vacuum hose 200. In some embodiments where the vacuum hose 200 is provided in the form of a cylindrical tube, the end effector 300 may be provided in the form of a cylindrical disk or tube that is concentric to the vacuum hose 200.
[0038] The end effector 300 may include an inlet assembly 310 protruding outwardly therefrom. The inlet assembly 310 is designed to accept compressed air from an external compressor (not shown). The inlet assembly 310 may further include a compressor coupling 312 at a terminal end such that the inlet assembly 310 may be coupled to an external source providing compressed air. The compressor coupling 312 may be provided in the form of a standard compressor connection or other suitable connection.
[0039] The end effector 300 may also include a manifold 320. The manifold 320 is designed to regulate and/or direct the air received from the inlet assembly 310 toward and into one or more valves 330. The manifold 320 is defined by a top plate 322 (see
[0040] The VELTS system 100 may further include one or more pipes 340 extending between the one or more valves 330 and the excavator head 400. The excavator head 400 may be coupled to the pipes 340 through one or more third fittings 344 (see
[0041]
[0042] Referring to
[0043] As shown in
[0044] Each of the one or more second openings 326 may be coupled to a respective valve 330 using a second fitting 316 (see
[0045] The one or more valves 330 may be actuated by an operator, automatically via software, or using air logic operated controls. For example, the operator may actuate one or more of the valves 330 using a control box 900, discussed in more detail with respect to
[0046] Each of the one or more valves 330 may be coupled to a respective conduit or pipe 340 (see
[0047] In some aspects, the bottom plate 324 may also include one or more third openings 328. The third opening(s) 328 may be smaller than each of the one or more second openings 326 and disposed between two of the second openings 326. Some or each of the third openings 328 may be coupled to a pressure regulator 350 (see
[0048]
[0049] Referring to
[0050] Referring to the example embodiment shown in
[0051]
[0052] Returning to
[0053] The third portion 450 may be defined by a second inner profile 452 that also generally corresponds to an exterior shape of the vacuum hose 200 similar to the first inner profile 432. However, the third portion 450 may also include a flange 451 on a terminal end thereof that protrudes inwardly toward a center of the excavator head 400 such that the flange 451 may overlap with a bottom portion of the vacuum hose 200, to secure and/or seal the vacuum hose 200 to the base of the second portion.
[0054] Referring to
[0055] In some embodiments, both the first inner surface 436 and the first outer surface 438 may be provided in a concave shape. In some aspects, the first inner surface 436 and the first outer surface 438 may be provided in the form of other shapes or curvatures.
[0056] The third portion 450 of the excavator head 400 may be defined by one or more substantially similar segments. The third portion 450 segments each may include a curvilinear second wall 454 having a second inner surface 456 (see
[0057] In some embodiments, such as the ones illustrated in
[0058] Referring to
[0059] Referring to
[0060] The second end 520 of the nozzle 500 is provided as an exhaust to release air externally (e.g., toward a pit for excavation). A diverging portion 522 may be provided between the second end 520 and the throat portion 530. The diverging portion 522 may transition the third diameter from the throat portion 530 toward the second diameter at the second end 520. The diverging portion 522 may include one or more conical portions 524 and one or more ring portions (not shown) each having a progressively larger diameter toward the second end 520.
[0061] The nozzles 500 are designed to exhaust air at a high speed (such as sonic or supersonic speed), creating air lances. Air from the external compressor may be injected into the nozzles 500 at a lower speed (e.g., a subsonic speed below Mach 1). As the air moves from the converging portion 512 toward the throat portion 530, the air may be compressed due to a change in volume and may start to increase in velocity and may drop in pressure. At the throat portion 530, the air may reach a critical point called choked flow, resulting in the velocity of the air increasing to sonic speed (about Mach 1) at the throat portion 530. As the air moves from the divergent portion 522 toward the second end 520, the air may further increase in velocity and may drop in pressure. As the air reaches the second end 520 and exhausts therefrom, the air may reach supersonic speeds. Thus, the speed of the air lance may depend on the design of the nozzle(s) 500, as well as the external compressor.
[0062] The first end 510 of the nozzle 500 may be configured to accept compressed air at between about 200 pounds per square inch (psi) to about 400 psi, between about 250 psi to about 350 psi, about 300 psi, or about 350 psi.
[0063] The first end 510 of the nozzle 500 may also be configured to accept compressed air up to about 1,300 cubic feet per minute (cfm), between about 700 cfm to about 1,300 cfm, between about 800 cfm to about 1,200 cfm, between about 900 cfm to about 1,100 cfm, about 900 cfm, about 1,000 cfm, or about 1,100 cfm. In an example embodiment, the external compressor may be configured to provide compressed air at about 350 psi and about 900 cfm.
[0064] The second end 520 of the nozzle 500 may be configured to exhaust air at a high speed, such as about Mach 1, about Mach 1.5, about Mach 2, about Mach 2.5, about Mach 3, about Mach 3.5, about Mach 4, about Mach 4.5, about Mach 5, or at a speed exceeding Mach 5.
[0065] Referring to
[0066] The control box 900 may be connected to the valves 330 through hard-wire or wireless protocols. For example, a plug connector (not shown) may be provided on the end effector 300 to accept a connection plug from the control box 900. As described above, in some embodiments, the VELTS system 100 can be operated hands-free using air-logic controls.
[0067] The control box 900 may further include a power source (not shown) of the first interface 910, such as a battery or a power plug to provide power to the control box 900. Moreover, the control box 900 may also include one or more indicators such as audible alarms, lights, displays, haptics, icons, etc. In some embodiments, the one or more indicators can be configured, monitored, and/or initiated using a notification module (not shown).
[0068] In some embodiments, an application running on a remote device (such as a cellular phone or a tablet) or software running on a computer (such as a personal computer or a laptop computer) may be used to control the VELTS system 100 in addition to, or lieu of, the control box 900. In some aspects, the control may be performed using a wireless communication protocol(s) (e.g., Wi-Fi, Bluetooth, Zigbee, cellular, MQTT, RFID, etc.)
[0069] The housing 940 for the control box 900 may be provided in the form of a durable material, such as a waterproof or water-resistant and shock-resistant thermoplastic, or similar hard shell material to protect the interfaces and/or controls. In some aspects, the housing 940 may be provided in the form of a rubber or metal housing.
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[0074] The one or more valves 330 may be controlled to actuate in an open state for a first time duration, and an off state for a second time duration. For example, the one or more valves 330 may be controlled to actuate for about 1 second in the open state and 0 seconds in the off state, resulting in continuous or substantially continuous air exhaustion. Likewise, the one or more valves 330 may be controlled to actuate in the open state for about 1 second on and about 1 second in the off state, about 2 seconds on and 0 seconds off, about 2 seconds on and about 1 second off, about 2 seconds on and about 2 seconds off. As can be appreciated, other variations are also possible and are within the spirit of this disclosure.
[0075] Although
[0076] Specific embodiments of a VELTS system 100 according to the present disclosure have been described for the purpose of illustrating the manner in which the invention can be made and used. It should be understood that the implementation of other variations and modifications of this invention and its different aspects will be apparent to one skilled in the art, and that this invention is not limited by the specific embodiments described. Features described in one embodiment can be implemented in other embodiments. The subject disclosure is understood to encompass the present invention and any and all modifications, variations, or equivalents that fall within the spirit and scope of the basic underlying principles disclosed and claimed herein.