TH72515B - The anchor is fixed to the ground. - Google Patents

Abstract

DC60 (20/09/56) Ground anchor (1) used for stabilizing sloped parts, anchoring or A similar feature consists of a body (10), a pilot (30) connected to the end. The underside of the fuselage (10) was made in a detachable manner, and several wings (40, 40a) were hinged and fixed to the perimeter of the fuselage (10) in such a way that the spurs are pivoted; the wings (40, 40a) are hinged in Multiple swivel features extend outward from the body (10) when the ground anchor (1) is gradually pulled back from its stable position in the passage. which provides a large protruding area to create a wider cone Therefore, it can have a stronger bond. anchoring force Requirements can be achieved by having an anchor (1) penetrate into the soil with a smaller depth. (1) more than one such The units are interlocked to increase the number of wings (40, 40a) that span out to provide a conical cutting top. plus and more solid The ground anchor (1) is used to stabilize the slope. anchor or A similar feature is assembled with the body. (10) pilot (30) that is connected to the end the bottom of the fuselage (10) in such a way that it is removable and several wings (40,40a) that are hinged and fixed to the periphery of the body (10) in such a way that the spur can be rotated Wings (40,40a) attached to the folding craft Multiple spurs will extend outward from the body (10) when the ground anchor (1) is touched. Gradually pulled back from its stable position in the passageway. which provides a large protruding area to create a wider cone Therefore, it can have a stronger bond. anchoring force Requirements can arise by having a ground anchor (1) penetrate into the soil with a smaller depth. (1) more than one such The units are interlocked to increase the number of wings (40,40a) that span out to provide a cone-cut top. plus and more solid

Claims (1)

Disclaimer (all) which will not appear on the advertisement page: Amendment 17/09/2018 Claims 1. Ground anchor (1) used for stabilizing slopes, anchoring and related work characteristics. The ground anchor (1) is composed of a body (10) which consists of a pipe (11) at its bottom end. Intermediate body (15) above the junction (11), several radial protrusions (12) spaced symmetrically in an angular manner around the nape of the aforementioned bodies (10). Spreads outward from the periphery of the body between the aforementioned (10) to receive the wings (40, 40a) in a pivoting manner, where such radial protrusions (12) are also provided with a stop to The limit (14) is placed between the adjacent radial protrusions (12) to restrict the wings (40, 40a) that are attached to the fold in such a way that the pivoting pivots extend beyond the axis. The upper torso (16) above the mid torso (15), where the upper torso (16) is provided with a connection mechanism for connecting the ends. One side of the overhang Cable in a detachable manner Or for a lock with an anchor fixed in the ground (1), another similar unit; The mechanism also serves to connect the ground anchor thrusters in a removable manner to Thrust the anchor in the ground (1) into the pass that was pierced, neglected; Where the connection mechanism will include An overhang (17) arranged for connecting the ground anchor thrusters (19) in a removable manner to join the outer thread at the end of the shaft. Extend the cable (through an anchor bolt or the like) or for a ground anchor (1) to another pilot unit (30) connected to the connector (11) as mentioned in The detachable appearance at the lower end of the body (10) and several wings (40, 40a) with ears (41) spaced a pair of gaps towards their lower ends, where Ears (41), each one with a hole through the bed (42), is joined together as much as a propeller (43, 43a) that goes upward from the ear (41). The top of the impeller (43, 43a) ends with an air crest (45, 45a), where several wings (40, 40a) are hinged and fixed to several radial protrusions (12). The fuselage (10) with a mechanism for fixing in such a way that the pivot can rotate and have the same number of wings (40, 40a) as the number of sections. ---------- 1. Anchor fixed straight. Ground (1) used to stabilize slopes, anchoring and related work characteristics. Involved Where the anchor is fixed on the ground (1), it will be included Torso (10) which includes The head pipe (11) at the bottom end of it Intermediate body (15) above the aforementioned connector (11) Multiple radial overhangs (12) spaced symmetrically in an angular manner around the Torso (10) such And spread out from the outside of the body between the middle (10) to get the wings. (40,40a) in a pivot rotation Where such radius (12) protrusions, which are also provided with a stop to Restrict (14) shall be between the adjacent radial protrusions (12) to limit the wings (40,40a) to be Mounted on the folds in such a way that it rotates on the pivot, extending beyond its desired position. The upper torso (16) above the middle body (15). The upper body (16) is provided with a connecting mechanism for connection to one end of the overhang. Cable in a detachable manner It is possible or not for locking with an anchor in the ground (1), another similar unit, with the mechanism still in the act of connecting the thrusters to the ground in a detached manner. Got for The anchor pinned the ground (1) into the pass that was pierced. Where the connection mechanism will include An overhang (17) arranged for connecting the ground anchor thrusters (19) in a removable manner to join the outer thread at the end of the shaft. Filed Cable (through the latch Helix or the like), or another for locking ground (1). The pilot (30) is connected to such connector (11) in a detachable manner at the bottom end of the The body (10) and several wings (40,40a) with ears (41) spaced one pair of gaps to its lower end, where the ears (41) each with The holes through the nava (42) will join together as much as the propellers (43,43a) run upwards. From the ear (41) such pair And the upper part of the propeller (43,43a) ends with an air top (45,45a), with several wings (40,40a) hinged and fixed to the radial overhang (12). Many such parts of the fuselage (10) with a mechanism for fixing in such a way that the pivot can rotate and have the same number of wings (40,40a) as the number of parts. Radial protrusion (12), and where the mechanism for attaching the wings (40,40a) to the periphery of the body (10) is included. Having radial protrusions (12) that lie between the ears (41) that are spaced from each other and have a through hole (13) on the overhang. Such radial (12) is positioned in conjunction with the through hole (42) on the ear (41) that spaced such a gap.