EP0040026A1 - Free piston machines - Google Patents
Free piston machines Download PDFInfo
- Publication number
- EP0040026A1 EP0040026A1 EP81301919A EP81301919A EP0040026A1 EP 0040026 A1 EP0040026 A1 EP 0040026A1 EP 81301919 A EP81301919 A EP 81301919A EP 81301919 A EP81301919 A EP 81301919A EP 0040026 A1 EP0040026 A1 EP 0040026A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- piston
- pressure
- recess
- exhaust
- supply line
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
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Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH DRILLING; MINING
- E21B—EARTH DRILLING, e.g. DEEP DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B4/00—Drives for drilling, used in the borehole
- E21B4/06—Down-hole impacting means, e.g. hammers
- E21B4/14—Fluid operated hammers
Abstract
A free piston machine of the valveless type using piston wall ports and cooperative flow passages in the cylinder wall for supplying live pressure fluid to the piston working chamber and for exhausting the power working chamber is characterised by an axial pressure fluid supply line (10) that enters and has open termination within a pressure recess (11, 11a) to cooperate therewith in accordance with the motion of the piston to control the flow of pressure fluid to the power working chamber of the machine. The supply line (10) may be fixed to the body of the machine and cooperate with a pressure recess (11) in the piston, or the supply line may be carried by the piston to move therewith and to cooperate with a pressure recess (11a) in the machine body.
Description
- THIS INVENTION concerns free piston machines and in particular pressure fluid-powered free piston machines in which a piston is caused to reciprocate by the admission of pressure fluid, e.g. compressed air, alternately to working chambers at opposite ends of a cylinder within which the piston is reciprocable. Many pneumatic drills, such as hammer drills, utilise this principle.
- The efficient conversion of the energy content of the pressure fluid into motion of the piston depends critically upon the manner in which the pressure fluid is directed to the working chambers and exhausted therefrom in relation to the motion of the piston. The arrangements adopted for controlling the pressure fluid flows fall, broadly, into two classes: the "valveless" arrangements in which the motion of the piston serves to cover and uncover various static ports and passages to accomplish the required control; and the "valved" arrangements in which a valve mechanism responds to the motion of the piston to switch the pressure fluid supply from one working chamber to the other at appropriate instants in the cycle of reciprocation of the piston. The present invention is concerned with the "valveless" class of machine and has as its objective the provision of improved arrangements for directing the pressure fluid to, and exhausting the spent fluid from, the working chambers of the machine.
- In general, in the prior art valveless machines, for instance the machines respectively disclosed in U.S. Patents 4084647 and 4146097, the porting arrangements and pressure fluid passages are relatively complex and lead both to difficulties in manufacture of the machine and to less than optimum utilisation of the energy of the pressure fluid. The latter disadvantage mainly arises from restrictions and directional changes in the flow path of the pressure fluid to the working chambers and/or to the effort of the pressure fluid being restricted to only a proportion of the available cross-sectional area of the piston.
- An object of the present invention is to provide a valveless pressure fluid-powered free piston machine that avoids these disadvantages of the prior art constructions.
- In its broadest aspect the present invention provides a valveless pressure fluid-powered free piston machine comprising a piston reciprocable in a cylinder providing power and return working chambers respectively at opposite ends thereof, axially spaced apart pressure and exhaust piston wall ports and associated pressure and exhaust passages in the piston, and cooperative flow passages formed at least partly in the cylinder wall for connecting said pressure and exhaust piston wall ports with the power and relurr. working chambers respectively, in accordance with the position of the piston in the cylinder, and a pressure fluid supply line extending axially within the power working chamber, characterised in that the supply line enters and has an open termination within a mating axial pressure recess, said supply line and said pressure recess being responsive to movement of the piston in the cylinder and cooperating to provide a flow path from the recess to the power working chamber during part of the cycle of reciprocation of the piston.
- The pressure and exhaust passages in the piston are preferably rectilinear and inclined with respect to the axis of the piston so as to be formable by a simple drilling or like operation followed by surface finishing so as to minimise regions of stress concentration and to enable the available strength of the piston material to be fully realised, while providing flow paths of suitable cross-sectional area for efficient transmission of pressure fluid to the return working chamber, and for the efficient exhaust of spent fluid from the power working chamber. These passages are also preferably disposed within the same portion of the length of the piston to provide a strong and compact piston configuration.
- As in the usual case of a free piston machine, such as a hammer drill, movement of the piston in one direction constitutes the "power stroke" while movement of the piston in the opposite direction constitutes a "return stroke". In a machine in accordance with the invention, the said pressure fluid supply line is arranged within the power working chamber, i.e. the chamber to which pressure fluid is admitted to effect the power stroke of the piston, and admission of pressure fluid to this power working chamber is controlled. by the position of the piston as it affects the position of the pressure recess relative to the said supply line. This arrangement enables the full cross-sectional area of the piston to be exposed to the pressure fluid at the commencement of the power stroke so that the maximum thrust is developed to displace the piston in the power stroke.
- In some embodiments of the invention, the pressure recess is formed in the piston and the pressure fluid supply line is fixed to the cylinder or to a component associated therewith, the pressure recess in this case being connected to the said pressure passage in the piston.
- In other embodiments, however, the pressure recess is formed in the cylinder, e.g. in a headpiece thereof, or in a component associated therewith, and the pressure fluid supply line is fixed to the piston to move therewith, being connected to the said pressure passage in the piston.
- The piston may have an axial exhaust recess connected to the exhaust passage or passages in the piston. This exhaust recess may be arranged to cooperate with an axial exhaust line, such as a foot valve tube, to control the flow of spent pressure fluid from the return working chamber, or this recess may serve solely for passing spent pressure fluid from the power working chamber to an exhaust outlet, the movement of the piston providing, by other means, control of the flow of spent pressure fluid from the return working chamber.
- The length and location of the pressure fluid flow path-defining component constituted by the supply line, relative to the piston stroke, will determine the proportion of the power stroke over which pressure fluid may continue to flow from the supply line to the power working chamber. This flow path-defining component may comprise one or more grooves extending along the exterior of the supply line to provide one or more discrete flow paths between the pressure recess in the piston and the power working chamber when the piston is appropriately positioned in the cylinder, but in preferred embodiments the flow path-defining component comprises a suitable length of circumferential relieving of the supply line to provide greatest freedom for symmetrical pressure fluid flow from the pressure recess to the power working chamber.
- The said cooperative flow passages in the piston and cylinder wall may take various configurations. For instance flats or longitudinal grooves in the piston may cooperate with circumferential relieving of the cylinder wall in appropriate locations therein, or circumferential relieving of discrete areas of the piston may cooperate with suitably positioned longitudinal recesses or grooves formed in the cylinder wall. Other arrangements will be apparent to those skilled in the art.
- Exemplary embodiments of the invention, as applied to a down-the- hole hammer drill, are illustrated in the accompanying drawings in which:
- FIGURES 1 and IA together constitute a longitudinal section of part of a hammer drill constituting one embodiment of the invention;
- FIGURE 2 is a section on line II-II of Figure 1;
- FIGURE 3 is a section on line III-III of Figure 1;
- FIGURE 4 is a section on line IV-IV of Figure lA;
- FIGURES 5 and 5A correspond with Figures 1 and lA but show a second embodiment of the invention;
- FIGURE 6 is a cross-section on the line VI-VI of Figure 5;
- FIGURE 7 is a cross-section on the line VII-VII of Figure 5A;
- FIGURE 8 is a cross section on the line VIII-VIII of Figure 5B; and
- FIGURE 9 is a longitudinal section of another embodiment.
- Referring first to Figures 1 to 4, the hammer drill partly illustrated therein comprises a body defining a cylinder 1 within which a
piston 2 is recipr'ocable. The upper end of the body has a tubular spigot 3 adapted for attachment to a drill tube (not shown) by means of which the body may be rotated during a drilling operation and through which compressed air as pressure fluid is supplied to the drill. The pressure fluid flows into the drill by way of apassage 4 in the spigot 3, past a spring-loadednon-return valve 5 to a passage 6 communicating viaports 7 with thebore 8 of acylinder headpiece 9 carrying an axial pressurefluid supply line 10 that extends into apressure recess 11 in the adjacent end of thepiston 2. The region within the cylinder 1 between thepiston 2 and theheadpiece 9 constitutes a workingchamber 12 to which pressure fluid is admitted to effect the downward or "power" stroke of thepiston 2 and for this reason is termed the "power" working chamber herein. - The lower end of the
piston 2 is formed with anexhaust recess 13 that in the illustrated stroke-end position shown in Figure IA receives afoot valve tube 14 that defines an exhaust line for the outflow of spent pressure fluid and that is secured in the upper end of theshank 15 of a drill bit the head of which is not shown in the drawing. Thedrill bit shank 15 is secured in achuck 16 so as to have limited freedom for axial movement relatively to the drill body. Thus thebit shank 15 and thechuck 16 have cooperatingsplines 17 for the transmission of torque from the drill body to the bit, the splines being relieved as at 18 over a length of the bit shank to provideshoulders ring 21 to limit the axial movement of the bit. - In Figure lA the bit is shown in a position near the uppermost extent of its free motion and the
piston 2 is shown at the end of a power stroke, with its bottom end in engagement with an anvil surface at the upper end of thebit shank 15. - The pressure recess 11 in the upper end of the
piston 2 is connected bypressure passages 22 topressure ports 23 in the wall of the piston near to the lower end thereof. As shown in Figure 2, there are threepassages 22 and these are preferably rectilinear so as to be readily formable by drilling and reaming techniques and to be given a high degree of surface finish to minimise stress-raising changes of section and/or direction. Thepassages 22 may have other configurations if desired. - The exhaust recess 13 at the lower end of the piston is connected to
exhaust passages 24 that extend obliquely upwardly toexhaust ports 25 in the wall of the piston near to its upper end. As shown in Figure 2 there are threepassages 24, equiangularly spaced apart around the axis of the piston and disposed in the intervals between thepassages 22. Thepassages 24 are larger in cross-section than thepassages 22 because they are required to pass air that has expanded to a lower pressure than the live compressed air to be passed by thepassages 22. - As shown in Figure 3, the upper end of the
piston 2 is formed withexternal flats 26 that in the position of the piston shown cooperate with acircumferential recess 27 formed in the wall of the cylinder and that in turn communicates with theexhaust ports 25 in thepiston 2. Thus in the Illustrated position of the piston (and in the final part of the power stroke thereof and in the corresponding initial part of the return stroke) an exhaust flow path extends from thepower working chamber 12 past theflats 26 to therecess 27 and thence viaexhaust ports 25 andpassages 24 to theexhaust recess 13, and thefoot valve tube 14, to anexhaust passage 28 leading to openings (not shown) in the head of the bit. - As best seen in Figure 4, the lower end portion of the
piston 2 is formed withexternal flats 29 that in the illustrated position of the piston overlie acircumferential recess 30 in the wall of the cylinder. Thepressure ports 23 in the cylinder are positioned to overlie therecess 30 in this position of the piston so as to provide a flow path for compressed air from thepressure recess 11 via thepassages 22 andpressure ports 23 to thereturn working chamber 31 defined in the lower end of the cylinder 1 between the bottom of the piston and the anvil surface of thebit shank 15. - The
piston 2 is also formed, below theexhaust ports 25 but above thepressure ports 23, with a by-pass groove 32 the upper end of which breaks into one of theexhaust ports 25 and that is so positioned on the piston that if thebit shank 15 moves to its lowermost permitted position (as can happen under certain drilling conditions), the by-pass groove 32 mates with therecess 30 to provide a flow path between thereturn working chamber 31 and the exhaust recess 13 so as to prevent live compressed air entering thechamber 31 from being effective to cause a return stroke of the piston. - The
piston 2 is further formed with a small boreaxial passage 33 connecting therecesses - The
supply line 10 is externally relieved over that part of its length from theheadpiece 9 to approximately the position of the upper end face of thepiston 2 when the latter is in its normal power stroke-end position within the cylinder, that is, approximately the position illustrated. It will be noted that the pressure recess 11, except for its entrance region, is of larger diameter than the end portion of thesupply line 10 and accordingly the external relieving of the supply line and the enlargement of therecess 11 together provide a flow path from therecess 11 to thepower working chamber 12 when thepiston 2 is at or near the upper end of its permitted travel. - The operation of the embodiment just described in relation to Figures 1 to 4 is as follows. Assuming that the parts are in the position shown and that a supply of compressed air is available to flow past the
non-return valve 5 and via thesupply line 10 to thepressure recess 11, this live compressed air will flow from therecess 11 via thepassage 22,pressure ports 23 and recess 30, to thereturn working chamber 31 and thus cause upwards movement of thepiston 2. - During the course of this upwards movement or "return stroke" of the piston, the
pressure ports 23 will move out of register with therecess 30 and thus cut off the supply of compressed air to the working chamber 3L The compressed air that has been admitted to this chamber, however, will expand to continue exerting upwards thrust upon thepiston 2. - When the
piston 2 has travelled by a distance sufficient to withdraw thefoot valve tube 14 from therecess 13, thistube 14 will be placed into communication with the workingchamber 31. The spent (expanded) air in that chamber will thus be able to escape via thefoot valve tube 14 toexhaust passage 28, thereby to terminate the upthrust on thepiston 2. - During the return stroke of the
piston 2, theexhaust ports 25 will move out of register with therecess 27 and thus isolate thepower working chamber 12 from theexhaust passages 24 leading to therecess 13. Air thus trapped within the workingchamber 12 will therefore commence to be compressed by the continuing upward motion of thepiston 2. Moreover, as thepiston 2 approaches the end of its return stroke, the full section terminal portion of thesupply line 10 will enter the enlarged region of therecess 11 and so establish a flow path between the latter and thepower working chamber 12 for the admission of live compressed air to theworking chamber 12. This admission of compressed air to thepower working chamber 12 will thus arrest the upward motion of the piston and commence to drive it downwardly on its power stroke. Compressed air will continue to be admitted to the workingchamber 12 until such time as the flow path from the recess II to thechamber 12 is interrupted by the entry of the full section portion of thesupply line 10 into the matching sized entrance to therecess 11 in the piston. Thereafter the air in thechamber 12 will expand to give up energy to thepiston 2 until such time as theflats 26 overlap therecess 27 to provide a path to exhaust for the spent air in thechamber 12. - At the termination of its power stroke, the
piston 2 delivers a blow on the anvil surface at the upper end of thebit shank 15 and the above- described cycle then repeats. - It will be observed that during the power stroke and until such time as the
pressure ports 23 come to register with therecess 30, the full pressure of the compressed air entering therecess 11 acts effectively on the cross-section of the piston corresponding with the cross-section of the recess II. At the same time the compressed air that is entering or has entered thepower working chamber 12 from the recess II is exerting thrust on the annular area of the piston surrounding the supply line 1C so that, in effect, the live compressed air is active upon the total cross section of the piston to exert the maximum available thrust thereon. - The
axial passage 33 in the piston provides for a constant bleed of live compressed air from therecess 11 to therecess 13 and thus to the exhaust system. In operation of the hammer drill, the pulsating flow of exhausted, spent, air from the exhaust system serves for cooling the bit and for flushing cuttings away from the bit face. The bleed of live air viapassage 33 supplements this exhaust flow to enhance the action thereof, while maintaining an adequate flushing function at times when the piston is not reciprocating, as a result of movement of the bit to a position bringing the by-pass groove into register with therecess 30. - The embodiment of the invention illustrated in Figures 5 to 8 of the drawings differs significantly from that shown in Figures 1 to 4 only in regard to the manner in which the cooperative flow passages are formed in the piston and in the cylinder wall for connecting the pressure ports with the return working chamber, and the exhaust ports with the power working chamber, during the cycle of reciprocation of the piston.
- Thus components of the embodiment of Figures 5 to 8 that correspond with components of the embodiment of Figures 1 to 4 have been given the same reference numerals as in those Figures and will not be further described.
- As is apparent from Figures 7 and 8 in particular, the
piston 2 in this embodiment has no terminal relieving corresponding with theflats longitudinal grooves 41, preferably equiangularly spaced about the axis of the cylinder so as to provide symmetry of flow and disposed to provide communication between the workingchamber 12 and theexhaust ports 25 during the relevant part of the piston reciprocation cycle, while minimising asymmetry in the stresses in the drill body. In the arrangement shown there are four meniscus-section grooves 41 but it should be understood that there may be a different number of grooves and that these may have different sectional shapes to meet particular air flow and cylinder strength requirements. - A second set of
longitudinal grooves 42 is provided lower in the cylinder 1 than thegrooves 41 to provide the function of theflats 29 at the lower end of the piston in the embodiment of Figures 1 to 4. As shown in Figure 8, thesegrooves 42 are similar in configuration and arrangement to thegrooves 41 but other configurations and arrangements are possible to meet particular requirements as to air flow and cylinder strength. - To provide for uninterrupted communication between the
grooves 41 and theexhaust ports 25 during the relevant portion of the operating cycle and regardless of the rotational orientation of the piston within the cylinder, the piston is formed with a circumferential relieving 43 with which theexhaust ports 25 communicate. Likewise the piston is formed with a circumferential relieving 44 with which thepressure ports 23 communicate so as to provide for uninterrupted communication between those pressure ports and thegrooves 42 during the relevant portion of the operating cycle. - It will be noted that the circumferential relieving 43 communicates with a
groove 32 to provide the same function as the similar groove in the embodiment of Figures 1 to 4. - The embodiment illustrated in Figure 9 differs from the previously described embodiments of Figures 1 to 8 in two respects: the pressure
fluid supply line 10 is fixed to the piston to reciprocate therewith and to cooperate with a pressure recess lla that is formed in thecylinder headpiece 9; and secondly in that the lower end of thepiston 2 is stemmed and extends through aseal ring 50 in the cylinder and from which it is withdrawn at and near the upper stroke-end position to provide for venting of the return workingexhaust chamber 31 to an annular exhaust space 51 that communicates with lateral exhaust ports (not shown). - Thus in this embodiment the
exhaust recess 13 in the piston serves solely for venting thepower working chamber 12 to the exhaust port of the machine. - It will be apparent that this second modification is unrelated to the first: that is to say, the rearrangement of the
supply line 10 and pressure recess can be applied to the machines with foot valves and axial exhaust lines and likewise the stemmed piston and seal ring arrangement may be applied to control return working chamber venting in a machine in which the supply line and pressure recess arrangement is as in the embodiments of Figures 1 to 8. - It has been pointed out that in machines in accordance with the invention; the full cross-sectional area of the piston is available for exposure to the pressure fluid to generate the thrust to propel the piston on its power stroke so that conversion of pressure fluid energy into usable piston energy is maximised. It is accordingly possible to design the machine to operate with short strokes and higher than usual operating frequencies to achieve higher overall power outputs than, or conversely to utilise a heavier piston operating at lower impact velocities than usual to obtain the same power output as, conventional machines of corresponding dimensions and subject to the same pressure fluid supply. It has also been mentioned that the passages formed in the piston are susceptible to simple formation techniques that enable an optimum compromise to be obtained between passage cross-section and freedom of flow path, on the one hand, and piston strength on the other hand. As noted, the passages in the piston are preferably arranged within the same portion of the length of the piston to provide a compact configuration. This also enables the passages to be located in a piston region of full cross section not weakened by the presence of recesses such as the
recesses - Further advantages of the machine of the invention are that the cylinder is not complicated by the need to provide therein ports and blind passages as in many prior art constructions, the only required cylinder passages in the machine of the invention being open to the bore of the cylinder throughout their length and thus being capable of being manufactured by simple machining or other forming techniques and with minimisation of the cylinder strength reduction as the result of the provision of such passages. Complicated cylinder liner systems are not required.
- Moreover, because of their internal simplicity, machines in accordance with the invention may be constructed with integral or
non-detachable headpieces 9 such as illustrated in Figure 9, and/or with non-detachable chucks. - The pressure fluid supply line that extends axially in the power working chamber is of simple configuration capable of being manufactured by straightforward machining or equivalent techniques that preserve the strength and avoid the formation of stress raisers in this component, such as are unavoidable in certain prior art constructions with complicated porting of a pressure fluid supply line.
- The machine of the invention is mechanically simple, comprising a single moving part (the piston) and only few major functional items, viz, the cylinder, the pressure fluid supply line and the exhaust line (foot valve) or other arrangement for venting the return working chamber.
Claims (6)
1. A valveless pressure fluid-powered free piston machine comprising a piston reciprocable in a cylinder providing power and return working chambers (12, 31) respectively at opposite ends thereof; axially spaced-apart pressure and exhaust piston wall ports (23, 25) and associated pressure and exhaust passages (22, 24) in the piston, and cooperative flow passages formed at least partly in the cylinder wall for connecting said pressure and exhaust piston wall ports with the power and return working chambers respectively, in accordance with the position of the piston in the cylinder, and a pressure fluid supply line (10) extending axially within the power working chamber (12), characterised in that the supply line (10) enters and has an open termination within a mating axial pressure recess (II, lla), said supply line and said pressure recess being responsive to movement of the piston in the cylinder and cooperating to provide a flow path from the recess (ll, lla) to the power working chamber (12) during part of the cycle of reciprocation of the piston.
2. A machine according to claim 1, further characterised in that the pressure and exhaust passages (22, 24) in the piston are rectilinear, inclined with respect to the axis of the piston, and disposed within the same portion of the length of the piston.
3. A machine according to claim 1 or 2, further characterised in that the pressure recess is formed in the piston and is connected to the pressure passage or passages therein.
4. A machine according to claim 1, 2 or 3, further characterised in that the piston has an axial exhaust recess (13) facing the return working chamber (31) and connected to the exhaust passage or passages (24) in the piston.
5. A machine according to claim 4, further characterised in that said exhaust recess is arranged to cooperate with an axial exhaust line (14) to control the flow of spent pressure fluid from the return working chamber.
6. A machine according to any preceding claim, further characterised in that the pressure fluid flow path-defining component of the said supply line (10) comprises circumferential relieving of the supply line.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8015389 | 1980-05-09 | ||
GB8015389 | 1980-05-09 | ||
GB8040286 | 1980-12-16 | ||
GB8040286 | 1980-12-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0040026A1 true EP0040026A1 (en) | 1981-11-18 |
Family
ID=26275454
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP81301919A Withdrawn EP0040026A1 (en) | 1980-05-09 | 1981-04-30 | Free piston machines |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0040026A1 (en) |
AU (1) | AU7025881A (en) |
CA (1) | CA1151027A (en) |
ES (1) | ES502022A0 (en) |
PT (1) | PT73003B (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0081897A1 (en) * | 1981-12-10 | 1983-06-22 | WEAVER & HURT LIMITED | Percussive drills |
EP0099594A2 (en) * | 1982-07-23 | 1984-02-01 | WEAVER & HURT LIMITED | Rock drills |
GB2219817A (en) * | 1988-06-15 | 1989-12-20 | Abraham Gien | Down the hole hammer equipment |
EP0564427A1 (en) * | 1992-03-31 | 1993-10-06 | Uniroc Aktiebolag | Down-the-hole drilling machine |
WO1999057411A1 (en) | 1998-05-04 | 1999-11-11 | Permon S.R.O. | Pneumatic submersible boring tool |
US6386301B1 (en) * | 1997-10-01 | 2002-05-14 | Ian Graeme Rear | Down-hole hammer |
US7272579B1 (en) * | 2000-02-17 | 2007-09-18 | Fedbid, Inc. | Auction based procurement system |
EP1943407A1 (en) * | 2005-11-03 | 2008-07-16 | Rockmore International, Inc. | Backhead and drill assembly with backhead |
US8046269B2 (en) | 2000-02-17 | 2011-10-25 | Fedbid, Inc. | Auction based procurement system |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB749328A (en) * | 1953-05-01 | 1956-05-23 | Hughes Tool Co | Fluid actuated reciprocatory prime mover |
US3964551A (en) * | 1974-09-20 | 1976-06-22 | Reed Tool Company | Pneumatic impact drilling tool |
US3970153A (en) * | 1975-01-13 | 1976-07-20 | Abraham Gien | Pneumatic percussion machines |
US4030554A (en) * | 1975-07-07 | 1977-06-21 | Bakerdrill, Inc. | Bore hole airhammer and anvil bit |
US4084647A (en) * | 1976-07-01 | 1978-04-18 | William Lister | Pneumatic percussion hammer |
US4146097A (en) * | 1972-04-24 | 1979-03-27 | Bakerdrill, Inc. | Bore hole air hammer |
-
1981
- 1981-04-30 EP EP81301919A patent/EP0040026A1/en not_active Withdrawn
- 1981-05-08 AU AU70258/81A patent/AU7025881A/en not_active Abandoned
- 1981-05-08 ES ES502022A patent/ES502022A0/en active Granted
- 1981-05-08 CA CA000377180A patent/CA1151027A/en not_active Expired
- 1981-05-08 PT PT7300381A patent/PT73003B/en unknown
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB749328A (en) * | 1953-05-01 | 1956-05-23 | Hughes Tool Co | Fluid actuated reciprocatory prime mover |
US4146097A (en) * | 1972-04-24 | 1979-03-27 | Bakerdrill, Inc. | Bore hole air hammer |
US3964551A (en) * | 1974-09-20 | 1976-06-22 | Reed Tool Company | Pneumatic impact drilling tool |
US3970153A (en) * | 1975-01-13 | 1976-07-20 | Abraham Gien | Pneumatic percussion machines |
US4030554A (en) * | 1975-07-07 | 1977-06-21 | Bakerdrill, Inc. | Bore hole airhammer and anvil bit |
US4084647A (en) * | 1976-07-01 | 1978-04-18 | William Lister | Pneumatic percussion hammer |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0081897A1 (en) * | 1981-12-10 | 1983-06-22 | WEAVER & HURT LIMITED | Percussive drills |
EP0099594A2 (en) * | 1982-07-23 | 1984-02-01 | WEAVER & HURT LIMITED | Rock drills |
EP0099594A3 (en) * | 1982-07-23 | 1984-04-25 | Weaver & Hurt Limited | Rock drills |
GB2219817A (en) * | 1988-06-15 | 1989-12-20 | Abraham Gien | Down the hole hammer equipment |
GB2219817B (en) * | 1988-06-15 | 1992-04-01 | Abraham Gien | Down the hole hammer equipment |
EP0564427A1 (en) * | 1992-03-31 | 1993-10-06 | Uniroc Aktiebolag | Down-the-hole drilling machine |
US6386301B1 (en) * | 1997-10-01 | 2002-05-14 | Ian Graeme Rear | Down-hole hammer |
WO1999057411A1 (en) | 1998-05-04 | 1999-11-11 | Permon S.R.O. | Pneumatic submersible boring tool |
US7272579B1 (en) * | 2000-02-17 | 2007-09-18 | Fedbid, Inc. | Auction based procurement system |
US8046269B2 (en) | 2000-02-17 | 2011-10-25 | Fedbid, Inc. | Auction based procurement system |
EP1943407A1 (en) * | 2005-11-03 | 2008-07-16 | Rockmore International, Inc. | Backhead and drill assembly with backhead |
EP1943407A4 (en) * | 2005-11-03 | 2012-01-04 | Rockmore International Inc | Backhead and drill assembly with backhead |
Also Published As
Publication number | Publication date |
---|---|
AU7025881A (en) | 1981-11-12 |
CA1151027A (en) | 1983-08-02 |
ES8302186A1 (en) | 1982-12-16 |
ES502022A0 (en) | 1982-12-16 |
PT73003B (en) | 1982-04-30 |
PT73003A (en) | 1981-06-01 |
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