Split flight pile systems and methods

Information

  • Patent Grant
  • 10385531
  • Patent Number
    10,385,531
  • Date Filed
    Tuesday, October 4, 2016
    8 years ago
  • Date Issued
    Tuesday, August 20, 2019
    5 years ago
Abstract
A pile assembly to be driven into the ground comprises an elongate member, a drive member, and a plurality of flight members. The drive member is supported by the elongate member to facilitate axial rotation of the elongate member. The plurality of flight members is supported by the elongate member. Axial rotation of the elongate member causes the plurality of flight members to auger the elongate member into the ground. The flight members are arranged to balance the loads on the elongate member as the elongate member is driven into the ground.
Description
TECHNICAL FIELD

The present invention relates to pile systems and methods and, in particular, to pile systems configured to be augered into the ground.


BACKGROUND

Piles are common driven into the ground to provide support for structures. Depending on the nature of the structure and the nature of ground where structure is to be built, the pile can be configured in a number of different shapes and sizes and can be manufactured of a variety of different materials.


A common pile type is made of cylindrical pipe. Cylindrical pipe piles are relatively in expensive and are commonly driven into the ground using a combination of static and vibrational forces. Certain pipe piles are provided with a drive bit to allow the cylindrical pipe pile to be driven into the ground using axial rotation.


The need exists for improved pipe piles that facilitate the insertion of the pile into the ground.


SUMMARY

The present invention may be embodied as a pile assembly to be driven into the ground comprises an elongate member, a drive member, and a plurality of flight members. The drive member is supported by the elongate member to facilitate axial rotation of the elongate member. The plurality of flight members is supported by the elongate member. Axial rotation of the elongate member causes the plurality of flight members to auger the elongate member into the ground. The flight members are arranged to balance the loads on the elongate member as the elongate member is driven into the ground.


A pile assembly to be driven into the ground comprises an elongate member, a drive member, and a plurality of flight members. The elongate member is hollow and cylindrical elongate member and defines a drive end portion, a driven end portion, and a shaft portion extending between the drive end portion and the driven end portion. The drive member is arranged on the drive end portion of the elongate member to facilitate axial rotation of the elongate member. The plurality of flight members arranged on the driven end portion of the elongate member. Axial rotation of the elongate member causes the plurality of flight members to auger the elongate member into the ground. The flight members are arranged to balance the loads on the elongate member as the elongate member is driven into the ground.


The present invention may also be embodied as a method of driving a pile assembly into the ground comprising the following steps. An elongate member is provided. A drive member is supported on the elongate member. A plurality of flight members is supported on the elongate member. The drive member is engaged to axially rotate the elongate member such that the plurality of flight members auger the elongate member into the ground. The flight members are arranged to balance the loads on the elongate member as the elongate member is driven into the ground.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a perspective view of a first example pile assembly of the present invention;



FIG. 2 is a first side elevation view of the first example pile assembly;



FIG. 3 is a second side elevation view of the first example pile assembly rotated 90 degrees from the first side elevation view;



FIG. 4 is a third side elevation view of the first example pile assembly rotated 90 degrees from the second side elevation view;



FIG. 5 is a fourth side elevation view of the first example pile assembly rotated 90 degrees from the third side elevation view;



FIG. 6 is a side elevation view of a portion of FIG. 2 illustrating an offset between first and second flight members of the first example pile assembly; and



FIG. 7 is a partial, side elevation view of a second example pile assembly having no offset between first and second flight members thereof.





DETAILED DESCRIPTION

Referring initially to FIGS. 1-6 of the drawing, depicted therein is a first example pile assembly 20a constructed in accordance with, and embodying, the principles of the present invention. The first example pile assembly 20a defines a pile axis 22 and is driven into the ground 24 (FIG. 2) with the pile axis 22 at a desired orientation.


The first example pile assembly 20a comprises an elongate member 30, a drive member 32, and first and second flight members 34 and 36. As shown in FIG. 2, the drive member 32 is secured to or integrally formed with a drive end portion 40 of the elongate member 30, while the first and second flight members 34 and 36 are secured to or integrally formed with a driven end portion 42 of the elongate member 30. A shaft portion 44 of the elongate member 30 extends between the drive end portion 40 and the driven end portion 42. The example elongate member 30 is hollow and defines a central chamber 46.


More specifically, the example elongate member 30 is a cylindrical hollow member defining an outer surface 50, an inner surface 52, a drive end surface 54, and a driven end surface 56. A threaded surface portion 58 of the inner surface 52 is formed at the drive end portion 40 of the elongate member 30. The example drive end surface 54 is circular as best shown in FIG. 1. The example driven end surface 56 comprises a first portion 56a, a second portion 56b, a third portion 56c, and a fourth portion 56d. As perhaps best shown by a comparison of FIGS. 2-6, in the example elongate member 30 the first and third portions 56a and 56c of the driven end surface 56 are laterally spaced from and substantially parallel to the pile axis 22. A comparison of FIGS. 2-6 further shows that, in the example elongate member 30, the second and fourth portions 56b and 56d of the driven end surface 56 are laterally spaced from and angled with respect to the pile axis 22.


The intersections of the first and second portions 56a and 56b of the driven end surface 56 defines a first point 60a, while the intersections of the third and fourth portions 56c and 56d of the driven end surface 56 defines a second point 60b. Associated with the first and second points 60a and 60b are first and second tooth portions 62a and 62b of the elongate member 30. The tooth portions 62a and 62b of the elongate member 30 are formed in the driven end portion between the first and second flight members 34 and 36 and the driven end surface 56.


Referring again to FIGS. 2-6, it can be seen that the example first flight member 34 defines a first lead surface 70, a first perimeter surface 72, a first engaging surface 74, a first rear surface 76, and a first trailing surface 78. Similarly, the example second flight member 36 defines a second lead surface 80, a second perimeter surface 82, a second engaging surface 84, a second rear surface 86, and a second trailing surface 88. The first and second flight members 34 and 36 are metal plates that are welded to the outer surface 50 of the elongate member 30.


Referring for a moment back to FIG. 1, it can be seen that the drive member 32 comprises a collar portion 90 and a drive portion 92. The drive portion 92 defines at least one drive surface 94. The example drive portion 92 is a hex drive defining six drive surfaces 94. The drive portion 92 is secured to the collar portion 90 and the collar portion 90 is secured to the drive end portion 40 of the elongate member 30 such that the drive surfaces 94 allow the drive member 32 to be axially rotated about the pile axis 22.


As is apparent from a comparison of FIGS. 2-6, the example first and second flight members 34 and 36 are symmetrically arranged about a longitudinal reference plane (not shown) defined by the pile axis 22. In particular, the example first and second flight members 34 and 36 are identical helical structures and are each arranged entirely on opposite sides of the reference plane. The example flight members 34 and 36 are semi helical or partially helical in that they extend only partly around the circumference of the example cylindrical elongate member 30. In the example pile assembly 20a, the example flight members 34 and 36 each extend approximately 180 degrees around the circumference of the example elongate member 30. Further, FIG. 6 illustrates that the example first and second flight members 34 and 36 are offset from each other along the pile axis by a distance D.


The flight members 34 and 36 also need not be identical. Further, the flight members 34 and 36 may each extend less or more than 180 degrees around the circumference of the elongate member 30. Further, while two flight members 34 and 36 are used in the example pile assembly 20a, more than two flight members may be used.


Further, a second example pile assembly 20b is shown in FIG. 7. The second example pile system 20b is in all most similar to the first example pile assembly 20a and will be described herein only to the extent that the two pile assemblies differ. In particular, FIG. 7 illustrates that, in the second example pile system 20b, the flight members 34 and 36 are not offset from each other.


In use, the pile assembly 20a or 20b is supported with the driven end portion 42 in contact with the ground 24 and the drive end portion 40 arranged such that the pile axis 22 is at a desired angular relationship with vertical and/or horizontal. The driven end portion 42 is then axially rotated (typically be engaging the drive member 32) such that the tooth portions 62a and 62b initiate insertion of the pile assembly 20a or 20b into the ground 24. After a few turns, the first lead surface 70 and then the second lead surface 80 engage the ground 24. Continued axial rotation of the elongate member 30 causes the first and second flight members 34 and 36 to auger the pile assembly 20a or 20b into the ground 24. FIGS. 3 and 5 illustrate that the lead surfaces 70 and 80 may be angled with respect to the pile axis 22 to enhance the ability of the lead surfaces 70 and 80 to cut into the ground 24.


The use of two or more flight members such as the flight members 34 and 36 balances the loads on the elongate member 30 created by the engagement of the flight members 34 and 36 with the ground 24 as the pile assembly 20a or 20b is being augered into the ground 24. The desired angular relationship between vertical and/or horizontal is more easily maintained with the balanced forces created by the example first and second flight members 34 and 36. Again, different shapes, numbers, and arrangements of flight members may be used to obtain a balanced force as the pile assembly 20a or 20b is being augered into the ground 24 until the drive member 32 is at or near a surface of the ground 24.


Optionally, after the pile assembly 20a or 20b is driven to a point at which the drive member 32 is at or near a surface of the ground 24, an extension pile member (not shown) may be connected to the pile assembly 20a or 20b to allow further driving of the pile assembly 20a or 20b. An extension pile member is similar to the pile assembly 20a or 20b except that the outer surface thereof at the driven end is externally threaded to engage with the threaded surface portion 58. With the external threaded surface of the extension pile member engaged with the threaded surface portion 58, rotation of the extension pile member causes the threaded portions to engage to join the extension pile member to the pile assembly 20a or 20b. Continued rotation of the extension pile member causes rotation of the pile assembly 20a or 20b and further drives the pile assembly 20a or 20b into the ground 24 such that the drive member 32 is below the surface of the ground 24. Additional extension pile members may be used to form a pile string extending a desired target depth.

Claims
  • 1. A pile assembly to be driven into the ground comprising: a cylindrical hollow elongate member defining a driven end portion and a pile axis, where the pile axis is aligned with a longitudinal axis of the elongate member,the driven end portion defines a driven end surface, andthe driven end surface defines a plurality of first portions angled relative to the pile axis, a plurality of second portions angled relative to the pile axis, and a point defined at an intersection of each of the first and second portions such that a plurality of one tooth portions is integrally formed by the elongate member;a drive member supported by the elongate member to facilitate axial rotation of the elongate member; anda plurality of flight members each defining a lead surface and a trailing surface, where the lead surfaces are angled with respect to the pile axis; wherebythe plurality of flight members are substantially helical and are supported by the driven end portion of the elongate member such that each of the plurality of flight members extends from the driven end portion of the elongate member through a different angular portion, where the different angular portions extend substantially the same distance around the circumference of the elongate member and the different angular portions total approximately 360 degrees,the plurality of flight members are symmetrically supported on the elongate member such that the lead surface of each flight member is at substantially the same angular location as the trailing surface adjacent thereto and the trailing surface of each flight member is at substantially the same angular location as the lead surface adjacent thereto,each of the plurality of flight members is spaced from the driven end surface of the elongate member, andeach of the plurality of flight members is spaced from at least one other flight member such that at least one of the plurality of flight members is offset from at least one of the flight members along the pile axis;axial rotation of the elongate member causes the at least one tooth portion defined by the driven end surface to engage the ground,after the driven end surface engages the ground, the lead surface closest to the tooth portions cuts into the ground,after the lead surface closest to the tooth portions cuts into the ground, another lead surface cuts into the ground, andthe plurality of flight members engage the ground to auger the elongate member into the ground; andthe flight members engage the ground to balance loads on the elongate member as the elongate member is rotated to auger the elongate member into the ground.
  • 2. A pile assembly as recited in claim 1, in which the plurality of flight members comprises first and second flight members; the first flight member extends around the driven end portion of the elongate member through an angle of approximately 180 degrees; and the second flight member extends around the driven end portion of the elongate member through an angle of approximately 180 degrees.
  • 3. A pile assembly as recited in claim 1, in which: the first portions of the driven end surface are substantially parallel to the pile axis; andthe second portion of the driven end surface are angled relative to the pile axis.
  • 4. A pile assembly to be driven into the ground comprising: a hollow, cylindrical elongate member defining a pile axis, a drive end portion, a driven end portion, and a shaft portion extending between the drive end portion and the driven end portion, where the pile axis is aligned with a longitudinal axis of the elongate member, andthe driven end portion defines a driven end surface that is substantially cylindrical and defines a plurality of first portions angled relative to the pile axis, at bast a plurality of second portions angled relative to the pile axis, and a point defined at an intersection of the first and second portions such that a plurality of tooth portions is integrally formed by the elongate member;a drive member arranged on the drive end portion of the elongate member to facilitate axial rotation of the elongate member; anda plurality of flight members each defining a lead surface and a trailing surface, where the lead surfaces are angled with respect to the pile axis; wherebythe plurality of flight members are substantially helical and are supported by the driven end portion of the elongate member such that each of the plurality of flight members extends around the driven end portion of the elongate member through a different angular portion, where the different angular portions extend substantially the same distance around the circumference of the elongate member and the different angular portions total approximately 360 degrees,the plurality of flight members are symmetrically supported on the elongate member such that the lead surface of each flight member is at substantially the same angular location as the trailing surface adjacent thereto and the trailing surface of each flight member is at substantially the same angular location as the lead surface adjacent thereto, andeach of the plurality of flight members is spaced from at least one other flight member such that at least one of the plurality of flight members is offset from at least one of the flight members along the pile axis;axial rotation of the elongate member causes the at least one tooth portion defined by the driven end surface to engage the ground, andafter the driven end surface penetrates the ground, the lead surface closest to the tooth portions cuts into the ground,after the lead surface closest to the tooth portions cuts into the ground, another lead surface cuts into the ground, andthe plurality of flight members engage the ground to auger the elongate member into the ground; andthe plurality of flight members engage the ground to balance the loads on the elongate member as the elongate member is rotated to auger the elongate member into the ground.
  • 5. A pile assembly as recited in claim 4, in which: the plurality of flight members comprises first and second flight members;the first flight member extends around the drive end portion of the elongate member through an angle of approximately 180 degrees; andthe second flight member extends around the driven end portion of the elongate member through an angle of approximately 180 degrees.
  • 6. A pile assembly as recited in claim 4, in which: the first portions of the driven end surface are substantially parallel to the pile axis; andthe second portions of the driven end surface are angled relative to the pile axis.
  • 7. A method of driving a pile assembly into the ground comprising the steps of: providing a cylindrical hollow elongate member defining a driven end portion and a pile axis, where the pile axis is aligned with a longitudinal axis of the elongate member,the driven end portion defines a driven end surface, andthe driven end surface defines a plurality of first portions angled relative to the pile axis, portions angled extending at a second angle relative to the pile axis, and a point defined at an intersection of each of the first and second portions such that a plurality of tooth portions is integrally formed by the elongate member;supporting a drive member on the elongate member;providing a plurality of substantially helical flight members each defining a lead surface and a trailing surface, where the lead surfaces are angled with respect to the pile axis;supporting the plurality of flight members on the driven end portion of the elongate member such that each of the plurality of flight members extends around the driven end portion of the elongate member a different angular portion, where the different angular portions extend substantially the same distance around the circumference of the elongate member and the different angular portions total approximately 360 degrees,the plurality of flight members are symmetrically supported on the elongate member such that the lead surface of each flight member is at substantially the same angular location as the trailing surface adjacent thereto and the trailing surface of each flight member is at substantially the same angular location as the lead surface adjacent thereto,each of the plurality of flight members is spaced from the driven end surface of the elongate member, andeach of the plurality of flight members is spaced from at least one other flight member such that at least one of the plurality of flight members is offset from at least one of the flight members along the pile axis; andengaging the drive member to axially rotate the elongate member such that the at least one tooth portion defined by the driven end surface to engage the ground, andafter the driven end surface engages the ground, the lead surface closest to the tooth portions cuts into the ground,after the lead surface closest to the tooth portions cuts into the ground, another lead surface cuts into the ground, andthe plurality of flight members engage the ground to auger the elongate member into the ground; whereinthe plurality of flight members engage the ground to balance loads on the elongate member as the elongate member is rotated to auger the elongate member into the ground.
  • 8. A method as recited in claim 7, in which: the step of providing a plurality of substantially helical flight members comprises the step of providing first and second flight members such thatthe first flight member extends around the driven end portion of the elongate member through an angle of approximately 180 degrees; and
  • 9. A method as recited in claim 7, in which the step of providing the cylindrical hollow elongate member comprises the steps of: forming the first portions of the driven end surface such that the first portions are substantially parallel to the pile axis; andforming the second portions of the driven end surface such that the second portions are angled relative to the pile axis.
RELATED APPLICATIONS

This application, U.S. patent application Ser. No. 15/285,326 filed Oct. 4, 2016 claims benefit of U.S. Provisional Application Ser. No. 62/239,692 filed Oct. 9, 2015, the contents of which are incorporated herein by reference.

US Referenced Citations (81)
Number Name Date Kind
500780 Simon Jul 1893 A
910421 Schlueter Jan 1909 A
999334 Pearson Aug 1911 A
1684816 Arden Sep 1928 A
2101285 Stevens Dec 1937 A
2128428 Murray, Jr. Aug 1938 A
2232845 Fieroh Feb 1941 A
3059436 Hermann, Jr. Oct 1962 A
3175630 Hein et al. Mar 1965 A
3411305 Cella Nov 1968 A
3999392 Fukushima et al. Dec 1976 A
4297056 Nottingham Oct 1981 A
4351624 Barber Sep 1982 A
4519729 Clarke et al. May 1985 A
4632602 Hovnanian Dec 1986 A
4650372 Gorrell Mar 1987 A
4768900 Burland Sep 1988 A
5088565 Evarts Feb 1992 A
5106233 Breaux Apr 1992 A
5117925 White Jun 1992 A
5240348 Breaux Aug 1993 A
5244316 Wright et al. Sep 1993 A
5263544 White Nov 1993 A
5355964 White Oct 1994 A
5388931 Carlson Feb 1995 A
5515655 Hoffmann May 1996 A
5529132 Evarts Jun 1996 A
5544979 White Aug 1996 A
5609380 White Mar 1997 A
5653556 White Aug 1997 A
5794716 White Aug 1998 A
6039508 White Mar 2000 A
6394704 Saeki May 2002 B1
6427402 White Aug 2002 B1
6431795 White Aug 2002 B2
6442906 Hwang Sep 2002 B1
6447036 White Sep 2002 B1
6543966 White Apr 2003 B2
6557647 White May 2003 B2
6641323 Ronsheim Nov 2003 B2
6648556 White Nov 2003 B1
6672805 White Jan 2004 B1
6732483 White May 2004 B1
6736218 White May 2004 B1
6896448 White May 2005 B1
6908262 White Jun 2005 B1
6988564 White Jan 2006 B2
7168890 Evarts Jan 2007 B1
7392855 White Jul 2008 B1
7694747 White Apr 2010 B1
7708499 Evarts et al. May 2010 B1
7824132 White Nov 2010 B1
7854571 Evarts Dec 2010 B1
7914236 Neville Mar 2011 B2
7950877 Evarts May 2011 B2
8070391 White Dec 2011 B2
8181713 White May 2012 B2
8186452 White et al. May 2012 B1
8434969 White May 2013 B2
8496072 White Jul 2013 B2
8763719 White Jul 2014 B2
8769893 Gill et al. Jul 2014 B1
9249551 White Feb 2016 B1
9255375 Yingling et al. Feb 2016 B2
9556581 Hale et al. Jan 2017 B2
9556621 Pelc et al. Jan 2017 B2
9631335 Reusing et al. Apr 2017 B2
9957684 Suver et al. May 2018 B2
20050039952 Hill et al. Feb 2005 A1
20060198706 Neville Sep 2006 A1
20100266344 Plotkin et al. Oct 2010 A1
20100303552 Yingling et al. Dec 2010 A1
20110162859 White Jul 2011 A1
20120292062 White Nov 2012 A1
20130149040 Evarts Jun 2013 A1
20140056652 Suver Feb 2014 A1
20140356075 Hale Dec 2014 A1
20140377011 Yingling et al. Dec 2014 A1
20150016893 Suver et al. Jan 2015 A1
20160356294 Fenwick et al. Dec 2016 A1
20170167102 Suver et al. Jun 2017 A1
Foreign Referenced Citations (15)
Number Date Country
2394894 Feb 2002 CA
2942801 Oct 2015 CA
102296608 Jul 2015 CN
59228529 Dec 1984 JP
497015 Mar 1992 JP
2005256500 Sep 2005 JP
2005315050 Nov 2005 JP
2006089933 Apr 2006 JP
2006177125 Jul 2006 JP
2006312825 Nov 2006 JP
2009138487 Jun 2009 JP
46428 Apr 1929 NO
2109881 Apr 1998 RU
WO 9600326 Jan 1996 WO
2012031108 Mar 2012 WO
Non-Patent Literature Citations (2)
Entry
USPTO, “Non-Final Office Action, U.S. Appl. No. 15/372,196,” dated Oct. 4, 2017, 23 pages.
USPTO, “Non-Final Office Action, U.S. Appl. No. 15/174,724,” dated Dec. 11, 2018, 18 pages.
Related Publications (1)
Number Date Country
20170101759 A1 Apr 2017 US
Provisional Applications (1)
Number Date Country
62239692 Oct 2015 US