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CA1313249C - Closed air system seismic wave generator - Google Patents

Closed air system seismic wave generator

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Publication number
CA1313249C
CA1313249C CA000569425A CA569425A CA1313249C CA 1313249 C CA1313249 C CA 1313249C CA 000569425 A CA000569425 A CA 000569425A CA 569425 A CA569425 A CA 569425A CA 1313249 C CA1313249 C CA 1313249C
Authority
CA
Canada
Prior art keywords
piston
bore
port
gas
chamber
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.)
Expired - Fee Related
Application number
CA000569425A
Other languages
French (fr)
Inventor
Andrew B. Woodrow
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Atlantic Richfield Co
Original Assignee
Atlantic Richfield Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Atlantic Richfield Co filed Critical Atlantic Richfield Co
Priority to CA000569425A priority Critical patent/CA1313249C/en
Application granted granted Critical
Publication of CA1313249C publication Critical patent/CA1313249C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

Abstract of the Disclosure Apparatus for generating seismic waves including an upstanding hollow cylindrical housing within which an impact piston latched in a cocked position is adapted to be propelled downwardly by high pressure expanding gas in the confined chamber above it within the housing so as to strike a target plate resting on the ground adjacent the lower end of the housing. After each blow against the target, the piston is retracted upwardly by means of hydraulic cylinders which recompress the gas in the chamber to its original pressure. Since there is no need for recharging the pressure chamber after each shot, economical rapid cycle operation is facilitated.

Description

RAPID CYCLE SEISMIC WAVE GENERATOR
Background of the Invention 1. Field of the Invention .
This invention relates generally to the field of seismic prospecting and more particularly to a method and apparatus for injecting a seismic wave into the earth.
2. Descrip~ion of the Prior Art U.S. Patent No. 4,284,165 issued August 18~ 1981 to Airhart and Barta teaches an apparatus for generating an _ acoustic pulse by propelling a mass downwardly by gas pres-sure against a rigid target in contact with the earth. The attained kinetic energy of the moving mass is transferred to the earth over a very short period of time. In this device, compressed gas is introduced within the hollow cy-lindrical housing which suppor~s the impact mas~ by means of continuou~ly repressurized high volume accumulators. The piston is provided with mean3 for guiding its travel along the bore of the hou~ing, but the piston has no seal rings.
Therefore, wi~h each opexation of this device, gas pressure escapes to atmosphere through the bottom of the hou~ing and must be replenished. The retrac~ion of the impact piston to its initial po~ition does not re~tore his lost pressure.
Another prior art d~vice for generating seismic waves through high energy impact of a moving piston against a rigid target i8 describedin U.S.Patent No. 4,284,164 issued August 18, 1981 ~o Airhart. As in the previously described patent, a piston is propelled downwardly within a cylindrical housing by a high pressure expanding gas delivered fxom ex-ternal high volume accumulators. Although in this dev.ice, the downwardly moving piston is provided with seal rings which preven~ escape of gas downwardly along ~he bore of the housing in which the piston moves, the expanding gas ~ 3132~9 which drives the piston downwardly is sLmultaneously dis-charged upwardly through constricted vent passages in the top of the housing.
Since devices of the character described do not employ completely enclosed pressure systems, they can only be operated successively with the use of high volume accumulators and powerful compressors to repressurize them. The time re-quired for this continual repres~urization limits the rate at which these devices may be recycled. The number and size of the compressors required also add significantly to the expense of installation and operation.
The general objec~ of this invention is, therefore, to provide an improved seismic wave generator of the impulse type utilizing gas pressure as the propulsion means.
It is a more particular objec~ of this invention to provide a device of the character described which facilitates rapi~ operation wi~h enhanced economy.
Other objects and advantages of this invention will become apparent from a consideration of the detailed descrip-tion to follow taken in conjunction with the drawings and the appended claims.
Summary of the Invention In accordance with ~he preferred embodiment of this invention, an impact piston is interfitted within the bore of an upstanding hollow cylindrical housing having a closed top and open bottom so as to create an enclosed gas pressure chamber above such piston o~ variable volume. In its upward cocked position, the piston is supported above a target resting on the earth. Upon release of this support means, the piston is propelled downwardly by gas pressure to strike the target, thereby suddenly transferring its attained kinetic energy to such target~ The resultant downward acceleration ~3~32~

of the target deforms the earth elastically to generate a seismic wave. Means are provided or initially filling the space above the piston with gas from an external source at a first lower pressure in the bottom-most piston position~
By means of a plurality of hydraulic cylinders aligned with the housing, the impact piston is lifted from such bottom-most position to its cocked position thereby increasin~ the pressure in the confined chamber space above it to a second higher value. Since the piston is provided with airtight 1~ seals, the chamber is therefore repressurized to substantially the same pressure after each shot. Thu~ the device can be operated repetitively at a rapid rate without requiring ex-ternal gas supply means.
Brief Descri tion of the Drawings P
FIGUR~ a sectional view oX a seismic wave generator in accordance with the preferred embodiment of this invention.
FIGURE 2 is a partial sectional view of a seismic wave generator in accordance with an alternate embodiment of this invention.
FIGURE 3 is a partial sectional view of a seismic wave generator in accordance with a fur~her alternate em-bodiment of this invention.
Brief Description of the Preferred Em~odiments With reference now to FIGURE 1, a seismic wave generator 10 is seen to consist generally of an upstanding hollcw cylindrical housing 12 supported by means o frame 14 from any desired transport vehicle (not shown~ in spaced relation abo~e the earth. An impact piston 16 is adapted to move slidably within the bore of housing 12 from an upper cocXed position as shown in FIGURE 1 to a lower operated position (shown in dotted outline) in which piston 16 makes - ~3132~

contac~ with ~he ground contacting target plate 20. The space between the top surface 22 of piston 16 and the closed top 24 of housing 12 constitutes a gas pressure chamber 26 of variable volume. Piston 16 terminates at i~s lower end external to the open bottom 28 of housing 12 in an enlarged diameter impact mass 32 having a convex impacting surface 34 adapted in operation to strike the mating concave surPace 35 of upstanding pillar 36 of target plate 20.
Piston 16 is provided with a plurality of seal rings 38 adjacent its top surface 22 and a plurality of spaced apart longi~udinally extending guide strips 40 affixed to th~
outer surface thereof. Vuring the downward motion of piston 16, guide strips 40 maintain proper axial alignment with the bore of housing 12, their upper ends heing beveled to insure proper matin~ with said bore upon return of piston 16 to its upper cocked position.
Piston 16 may be returned to its upper cocked posi-tion by means such as hydraulic lift cylinders 44 extending coaxially with the bore of housing 12 on either side thereof and provided respectively with lift rods 46 extending through apertures 50 in piston flange 52 extending radially outward of impact mass 32. The lower ends of lift rods 46 are pro-vided with lift rings 54. Preparatory to the operation of generator 10, lift rods 46 are lowered to assume the dotted position as shcwn. Upon completion of a firing operation, lift rings 54 engage and bear upwardly against flange 52 so as to return piston 16 to its initial coc~ed position.
Piston 16 may be supported in the cocked position by any convenient means such as electrically operated latches 60.
As shown, a pair o latches 60 move radially of housing 12 to supportively engage the under surface of flange 52. In opera-tion, latches 60 are wi~hdrawn, whereupon impact piston 16 is ~3~'~2~9 downwardly propelled by gas pressure in chamber 26 in addition to its own weight. Piston 16 is then accelerated rapidly so that convex impacting surface 34 strikes concave surface 35 to generate the desired seismic pulse.
Typically, chamber 26 is filled through conduit 27 to 2 first lower pressure in the downward most position of piston 16 from some suitable external source (not shown).
Thereafter, piston 16 is retracted upwardly to its cocked position by means of hydraulic cylinders 44 so as to increase the pressure in chamber 26 in inverse proportion to the decrease in the volume thereo. Cylinders 44 may be operated from relatively low pressure compressor sources.
~ lhat has ~een described is essentially a closed pressure system wherein ~ubstantially no gas escapes from chamber 26 as the device is operated. Therefore, at the conclusion of each "sho~" or operation, chamber ~6 is re-pressurized to substantially the same pressure as before.
In this manner, generator 10 may be cycled rapidly without the need for constantly replenished high volume arcumulators as taught by the prior art. The initial pressuriæing of chamber 26 may be accomplished at a relatively low pressure thus reducing the size of compressors required. Over time, some leakage from chamber 26 will necessarily occur, but by precision machining of parts and use of high-grade seal this leakage can be controlled sufficiently to permit a reasonable number of repetitive generator "shots" without significant energy degradation.
The fact that generator 10 constitu~es a closed self-contained system maXes it particularly well adapted for use in a man-portable, relatively light weight system, as well as in hi~h energy devices employing heavy impact masses for deep earth penetration.

~3~2~9 In an alternate embodiment of this invention as shown in the partial view of FIGVRE 2, a generator 60 func-tioning in substantially the same manner and having components substantially similar to those of generator 10 includes a hollow upstanding cylindrical housing 62 (only the upper end o which is illustrated) which is supported by frame 64 from a transport vehicIe (not shown~. In the cocked position of impact piston 68, the upper end 70 thereof is received within and sealingly enqaged by downwardly opening cap 72 supported in any suitable fashion within enclosed pressure chamber 74 communicating between housing top 76 and impact piston 68.
Beneath cap 72, piston 68 engages the bore of housing 62 through hermetic seal rings 77. Retraction of piston 68 to its cocked position may be effected in the manner previously described in the embodiment of FIGURE 1 by means of hydraulic cylinders 78. The distinguishing feature of this embodiment is that in the cocked position of piston 68, the gas pressure within chamber 74 is isolated from the upper surface 79 of piston 68 by mean~ of seal ring 80. Thus, piston 68 in its 2Q cocked position is urged downwardly only by its own weight.
Any gas trapped between upper surface 79 of piston 68 and the corresponding inner surface 81 of cap 72 may be vented to atmosphere through line ~2 by operation of valve 84.
In operation, release of piston 68 through opera-tion of latch means (not shown~ permi~ piston 68 to fall under its own weight. ~en seal ring 80 disengages surface 81, pressure from chamber 74 infiltrates cap 72 through spaces 86 and pushes downwardly on the top surface 79 of piston 68 to powerfully accelerate it towards a target in the manner previously described.
As in the embodiment of FIGURE 1, the pressure chamber 74 may be ini~ially filled through line 90 rom some ~3~ 32~

external source (not shown~ to a first lower pressure, the pressure therein being increased to a second higher pressure with the upper movement of piston 68 in response to the operation of hydraulic lift cylinders 78. This embodiment of the invention, however, possesses the additional feature that the latch means (not shown) fox piston 68 need only support the weight oP piston 68 in the cocked position. There-fore, such latch mean-~ may be correspondingly less substantial because subjected to lower mechanical stresses than in the embodiment of FIGURE 1.
A further alternate embodiment o~ this invention is shown in FIGURE 3 wherein a seismic wave generator 100 is shown in part including an upstanding hollow cylindrical housing 102 within which an impact piston 104 is slidably supported by suitable latching means ~not shown). Housing 102 may be attached to a stabilizing transport vehicle through frame 105. In this embodiment, the upper end of impact pi~ton 104 is provided with an upwardly tapered wall 106 terminating in upper face 108 which is adapted in the cocked position of piston 104 to be received within downwaxdly opening cap 110 supported in any euitable fashion within pressure chamber 112. Isolation bPtween upper face 108 and the pressure in chamber 112 is secured by means of upper tapered seal ring 116 which contacts the mating tapered inner surface 118 of cap 110 in the cocked position of piston 104. LeaXage of pressure in chamber 112 in a downward direction is initially prevented by means of a second lower tapered seal ring 120 which is adapted to contact the mating tapered bore surface 122 of housing 102 beneath the bottom of cap 110. Additional seal rings 126 of constant diameter circling piston 104 provide added protection agains~ leakage as will be seen.
In this embodiment, it will be observed that in the cocked - 1 3~32~

position of pisto~ 104, a portion of tapered surface 106 is in constant communication with the pressure in chamber 112.
~herefore, a component of force due to the compressed gas in chamber 112 is constantly exerted downwardly against piston 104. The taper of surace 106 may be, for example, at an angl e of about 5 to the axial direction, which is sufficient to provide an initial breakaway force on piston 104 in the event seals 116 and 120 ~end to wedge against surfaces 118 and 122. The taper is not so great, however, that the down-ward pressure on the supporting latches (not shown) becomes excessive so as to risk leakage around seals 116 and 120.
As in the embodiment of FIGURE 2, except for the slight dcwnward pressure against tapered surface 106 in the latched or cocked position, piston 104 is urgçd downwardly only by its own weight~ In operation, when pressure from chamber 112 infiltrates cap 110, piston 104 disengages cap 110 and seals 116 and 120 no longer make contact with housing 102.
Seal rings 126 thereafter prevent pressure from escaping from the confines of chamber 112 and the space above piston 104. In the manner previously described, chamber 11~ may be initially pre~surized through line 130 by operating valve 132 to admit gas from an external source ~not shown). Hydraulic lift cylinders 140 lift piston 104 frGm its "fired" downward posi~ion to i~s cocked position and repressuri ze chamber 112 to operational pressure.
It should bP understood that in any of the em~odi ments of this invention described, various gases may be used, such as, for example, nitrogen. If desired, dewatered air may be subs~ituted. It is also evident that helical springs may be substituted for hydraulic cylinders to lift the gen-Prator piston to its cocXed position.
In opera~ion of this generator, it may be oriented -- 13~32~9 either vertically or at any desired angle to the vertical so as to generate both shear and compressional wave components.
The absPnce of heavy accumulators and compressor~ increases the manueverability of the device in varying such angle of orientation as well as making transportation less burdensome.
What has been described is illustrative only and many modifications of the features of thi~ de~ice will occur to those skilled in the art without departing from the qcope of the invention as more particularly se~ forth in the claims appended hereto.

Claims (4)

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:
1. A seismic wave generator for impacting an earth-contacting target comprising:
(a) a hollow cylinder housing defining a bore having a closed and an open end and having a side wall penetrated by at least one port intermediate such closed and open ends;
(b) means for supporting the housing in an upstanding position such that the closed end of the bore is uppermost and the target faces the open end;
(c) an elongated piston extending movably within the bore through the open end thereof for reciprocating movement therein such that a clearance is formed within the bore between the closed end thereof and the piston;
(d) a chamber filled with gas compressed to a selected value in a fluid communication with the bore through the port;
(e) means for releasably supporting the piston in a cocked position wherein the piston projects above the port;
(f) first annular seal means positioned intermediate the piston and the side wall of the bore for establishing slidable hermetic engagement therebetween above the port when the piston is in the cocked position such as to fluidly isolate the chamber from the clearance;
(g) second annular seal means positioned intermediate the piston and the side wall of the bore for establishing slidable hermetic engagement therebetween below the port such as to prevent escape of gas through the open end of the bore irrespective of the position of such piston;
(h) means for disabling the means for supporting the piston so as to permit the piston to fall from the cocked position, thereby effecting interruption of such slidable engagement thereof with the side wall of the bore above the port and enabling the gas to expand through the port into such clearance and to thereby drive the piston into the target; and (i) means for returning the piston to the cocked position, thereby repressurizing the gas in such chamber to substantially the selected value as a result of the flow of such gas from the bore into such chamber through the port.
2. Apparatus claimed in claim 1 further including valve means communicating with the clearance for venting gas pressure above the piston in excess of atmospheric upon return of the piston to the cocked position.
3. Apparatus as claimed in claim 1 wherein the piston is provided with an upwardly tapered side wall adjacent the upper end of the piston and the side wall of the bore has a correspondingly tapered portion adjacent its closed end, the port being disposed so as to penetrate the tapered side wall portion of the bore and expose the tapered wall of the piston to the pressure of the gas in the chamber when the piston is in the cocked position.
4. A seismic wave generator for impacting an earth-contacting target comprising:
(a) a hollow cylindrical housing defining a bore having a closed and an open end and having a side wall penetrated by at least one port intermediate such closed and open end;
(b) means for supporting the housing in an upstanding position such that the closed end of the bore is uppermost and the target faces the open end;
(c) an elongated piston extending movably within the housing through the open end of the bore for reciprocating movement therein such that a clearance of variable volume is formed within the bore between the closed end and the piston;
(d) a chamber filled with gas compressed to a selected value in communication with the bore through the port;
(e) means for releasably supporting the piston in a cocked position wherein the piston projects above the port;
(f) a first and a second annular seal ring carried on the piston in longitudinally spaced relation such that in the cocked position of the piston the first seal ring engages the side wall of the bore above the port in hermetic slidable relation so as to fluidly isolate the clearance from the chamber and such that in all positions of such piston the second seal ring engages the side wall of the bore below the port, thereby preventing escape of such gas through the open end of the bore;
(g) means for disabling the means for supporting the piston thereby permitting the piston to fall until the first seal ring reaches the level of the port, thus effecting fluid communication between the chamber and the clearance through the port and enabling the gas to drive the piston downwardly to strike the target to generate a seismic wave, thereby reducing the pressure of the gas in such chamber in proportion to the increase in the volume of such clearance;
and (h) means for returning the piston to such cocked position, thereby reducing the volume of the clearance and simultaneously repressurizing the gas in such chamber to substantially the selected value by the flow of such gas from the bore through the port.
CA000569425A 1988-06-14 1988-06-14 Closed air system seismic wave generator Expired - Fee Related CA1313249C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA000569425A CA1313249C (en) 1988-06-14 1988-06-14 Closed air system seismic wave generator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA000569425A CA1313249C (en) 1988-06-14 1988-06-14 Closed air system seismic wave generator

Publications (1)

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CA1313249C true CA1313249C (en) 1993-01-26

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112731516A (en) * 2020-12-18 2021-04-30 四川京航天程科技发展有限公司 Pneumatic artificial seismic source device without open fire

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112731516A (en) * 2020-12-18 2021-04-30 四川京航天程科技发展有限公司 Pneumatic artificial seismic source device without open fire

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Effective date: 19950726