US3716010A - Snap acting ballast release device - Google Patents
Snap acting ballast release device Download PDFInfo
- Publication number
- US3716010A US3716010A US00082661A US3716010DA US3716010A US 3716010 A US3716010 A US 3716010A US 00082661 A US00082661 A US 00082661A US 3716010D A US3716010D A US 3716010DA US 3716010 A US3716010 A US 3716010A
- Authority
- US
- United States
- Prior art keywords
- band
- torpedo
- weights
- release device
- hull
- 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 - Lifetime
Links
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 4
- 239000002360 explosive Substances 0.000 description 7
- 230000014759 maintenance of location Effects 0.000 description 2
- 229910000639 Spring steel Inorganic materials 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
- F42B19/36—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means adapted to be used for exercise purposes, e.g. indicating position or course
- F42B19/38—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means adapted to be used for exercise purposes, e.g. indicating position or course with means for causing torpedoes to surface at end of run
- F42B19/42—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means adapted to be used for exercise purposes, e.g. indicating position or course with means for causing torpedoes to surface at end of run by releasing solid ballast
Definitions
- a snap acting ballast release device for a water vehicle such as a torpedo, including: the hull of the torpedo having an annular recess; a plurality of Weights disposed within the recess; a resilient band extending around the weights and secured thereto in a closed biased position; means releasably connecting the ends of the band in the closed biased position; the band being adapted, because of its resiliency, to assume a relaxed open position away from the torpedo hull, so that upon release of the ends of the band the band and its attached weights snap free of the torpedo.
- a torpedo is typically operated in two configurations, exercise and warshot.
- a special exercise section is substituted for the warhead section of the warshot configuration.
- the warshot torpedo is designed to be negatively buoyant so that it will sink to the ocean bottom at the end of a run. It is desirable, however, that the exercise torpedo be rendered buoyant at the end of its run so that it can be recovered and reused for subsequent exercises.
- US. Pat. No. 3,404,649 there is illustrated a ballast release device which renders an exercise torpedo buoyant after its run.
- the present invention is directed toward improving the ballast release device in this patent by providing quick and positive release of the ballast weights from the torpedo.
- the present invention is similar to the ballast release device in the aforementioned patent in the respect that the torpedo hull has an annular recess, and a plurality of weights are disposed within this recess.
- the present invention attains its improvements by providing a resilient band which extends around the weights and is secured thereto in a closed biased position. Means, such as explosive bolt, releasably connects the ends of the band in this closed position.
- the band because of its resiliency, is adapted to assume a relaxed open position away from the torpedo hull so that upon release of the ends of the band the band and its attached weights will snap free from the torpedo.
- An object of the present invention is to provide a snap acting ballast release device for a water vehicle.
- FIG. 1 is an ocean elevation view of a torpedo employing the ballast release device
- FIG. 2 is a longitudinal cross sectional view of the exercise section employing the ballast release device for an exercise torpedo;
- FIG. 3 is a transverse section of the exercise torpedo showing the top pair of weights, retention means, and bottom weight in cross-section;
- FIGS. 4 through 7 illustrate the ballast release device in operation.
- FIG. 1 a water vehicle, such as a torpedo, which has a ballast release device for releasing weights from the vehicle when it is desired to render it buoyant for retrieval purposes.
- a water vehicle such as a torpedo
- a ballast release device for releasing weights from the vehicle when it is desired to render it buoyant for retrieval purposes.
- an exercise torpedo there is a special exercise section 10 which is joined to forward and after portions of the torpedo by any conventional joiner, such as that disclosed in Patent 3,100,121 to Hillmer.
- the section 10 of the torpedo is a hull portion which is substantially cylindrical and which includes the present ballast release device 12.
- the exercise hull section 10 is provided with an annular recess 14 which circumscribes the torpedo and which may have opposed inwardly tapered walls 16.
- a plurality of weights 18, which may be constructed of lead, are disposed within the recess 14.
- the weights 18 may be a plurality of wedge shaped blocks which are adapted to fit and substantially fill the annular recess 14 in consecutive fashion, as illustrated in FIG. 3.
- a resilient band 20 which may be constructed from spring steel, may extend around the weights 18 and may be secured thereto in a closed biased position, as illustrated in FIG. 3.
- the band 20, because of its resiliency, is adapted to as sume a relaxed open position away from the cylindrical hull section 10. In the preferred embodiment the relaxed position is substantially flat, as illustrated in FIG. 3. With such an arrangement, a release of the ends of the band 20 will cause the band and its attached weights 18 to snap free of the torpedo and render the torpedo buoyant for recovery purposes.
- the band 20 in its closed connected position assume an outer shape which forms a substantially smooth continuation with the hull section 10.
- the continuation with the hull may be accomplished by providing the hull with annular depressions 2.4 of substantially the same thickness as the band 20 at the top opposing edges of the recess '14.
- the heads of mounting bolts 26 may be attached to the interior surface of the band by any suitable means, such as welding.
- a pair of the bolts 26 extend radially inwardly through each weight 18 and are secured to the weights by nuts threaded on their opposite ends.
- Each weight 18 is provided with a pair of notches 28 which provide clearances for the nuts so that they do not interfere with the bottom of the recess 14.
- the releasable means 22 for the band 20 may include a retainer block 30 which is split into two portions.
- the end weights 18 on the band 20 may be provided with opposing recesses for receiving this retainer block.
- One block portion may be attached to the inner surface of the band 20 adjacent one end thereof and the other block portion may be attached to the inner surface of the band adjacent the other end thereof.
- Specially configured brackets 32 may be provided for making these attachments. The end portions of each bracket 32 may be welded to the interior surface of the band 20 and the block portions may be mounted thereto by bolts 34.
- an explosive bolt 36 may be provided which extends through both block portions and is threaded into at least one of the block portions for retention purposes.
- the bolt 36 contains an internal explosive which separates the bolt, and this explosive is detonated by an electrical lead 38.
- the lead 38 extends into a center portion of the torpedo through a fitting 40 and is actuated by instrumentation (not shown) which is set for a predetermined release time.
- instrumentation not shown
- the block may be provided with an internal substantially cylindrical cavity 42, and within this cavity there may be provided a ring collar 44 which bridges the joint of the retainer block portions.
- the ballast release device 12 is mounted to the torpedo prior to the exercise run. After the run is completed instrumentation within the torpedo sends a signal to the explosive bolt 36 which causes the bolt to separate Within the retainer block 30. Upon this occurrence the retainer block portions are separated and the resiliency of the band 20 causes the band and the attached weights 18 to quickly snap away from the torpedo. This renders the torpedo buoyant so that it can be recovered at the surface by a surface ship.
- a snap-acting ballast release device comprising; 7
- said hull having an annular recess
- said band being adapted, because of its resiliency, to
- said band having in its closed connected position an outer shape which forms a smooth continuation of the hull shape
- weights being wedge shaped and secured directly to the inner service of the resilient band in a substantially continuous fashion thereal'ong when the band is in a closed biased position;
- weights being secured to the resilient band by bolts which are welded to the inner surface of the band, whereby upon release of the ends of the'band, the band and its attached weights snap free of the vehicle.
- a combination as claimed in claim 1 including;
- the relaxed open position of the band being substantially flat.
- a combination as claimed in claim 2 including:
- the recess having annular opposed inwardly tapered walls;
- each weight being configured to substantially fit and fill an annular segment of said recess.
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- Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Physical Education & Sports Medicine (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
Abstract
A SNAP ACTING BALLAST RELEASE DEVICE FOR A WATER VEHICLE, SUCH AS A TORPEDO, INCLUDING: THE HULL OF THE TORPEDO HAVING AN ANNULAR RECESS, A PLURALITY OF WEIGHTS DISPOSED WITHIN THE RECESS, A RESILIENT BAND EXTENDING AROUND THE WEIGHTS AND SECURED THERETO IN A CLOSED BIASED POSITION, MEANS RELEASABLY CONNECTING THE ENDS OF THE BAND IN THE CLOSED BIASED POSITION, THE BAND BEING ADAPTED, BECAUSE OF ITS RESILIENCY, TO ASSUME A RELAXED OPEN POSITION AWAY FROM THE TORPEDO HULL, SO THAT UPON RELEASE OF THE ENDS OF THE BAND THE BAND AND ITS ATTACHED WEIGHTS SNAP FREE OF THE TORPEDO.
Description
Feb. 13, 1973 w. G- WILSON ETAL 3,716,010
SNAP ACTING BALLAST RELEASE DEVICE Filed Oct. 21, 1970 2 Sheets-Sheet l 12 mil/ M f 6E W2 0;
8/19/1455 11. WZZJHM D. WW5,
Feb. 13, 1973 w. G. WILSON ETAL 3,716,010
SNAP ACTING BALLAST RELEASE DEVICE Filed Oct. 21. 1970 2 Sheets-Sheet 2 32 HQ 12 m mum-M I f/wa/raes mZL/HM 6: 71 7280;
/WES J1 GEE-5A6 WZLIHM 0. W175,
4 FQV/n 65 0 /57 firraens g United States Patent SNAP ACTING BALLAST RELEASE DEVICE William G. Wilson, Livermore, James H. Green, Sierra Madre, and William D. White, Pasadena, Calif., as-
signors to the United States of America as represented by the Secretary of the Navy Filed Oct. 21, 1970, Ser. No. 82,661 Int. Cl. F42b 15/10, 19/00 US. Cl. 11422 3 Claims ABSTRACT OF THE DISCLOSURE A snap acting ballast release device for a water vehicle, such as a torpedo, including: the hull of the torpedo having an annular recess; a plurality of Weights disposed within the recess; a resilient band extending around the weights and secured thereto in a closed biased position; means releasably connecting the ends of the band in the closed biased position; the band being adapted, because of its resiliency, to assume a relaxed open position away from the torpedo hull, so that upon release of the ends of the band the band and its attached weights snap free of the torpedo.
STATEMENT OF GOVERNMENT INTEREST The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
BACKGROUND OF THE INVENTION A torpedo is typically operated in two configurations, exercise and warshot. In the exercise version, a special exercise section is substituted for the warhead section of the warshot configuration. To assure equivalent performance, it is important that the exercise section duplicate the same overall trim and weight characteristics of the warhead section. Since special instrumentation in the exercise section accounts for only a portion of the warhead explosive weight, it is typical to use ballast weights to make up the difference.
The warshot torpedo is designed to be negatively buoyant so that it will sink to the ocean bottom at the end of a run. It is desirable, however, that the exercise torpedo be rendered buoyant at the end of its run so that it can be recovered and reused for subsequent exercises. In US. Pat. No. 3,404,649 there is illustrated a ballast release device which renders an exercise torpedo buoyant after its run. The present invention is directed toward improving the ballast release device in this patent by providing quick and positive release of the ballast weights from the torpedo.
SUMMARY OF THE INVENTION The present invention is similar to the ballast release device in the aforementioned patent in the respect that the torpedo hull has an annular recess, and a plurality of weights are disposed within this recess. The present invention attains its improvements by providing a resilient band which extends around the weights and is secured thereto in a closed biased position. Means, such as explosive bolt, releasably connects the ends of the band in this closed position. The band, because of its resiliency, is adapted to assume a relaxed open position away from the torpedo hull so that upon release of the ends of the band the band and its attached weights will snap free from the torpedo.
STATEMENT OF THE OBJECTS OF THE INVENTION An object of the present invention is to provide a snap acting ballast release device for a water vehicle.
Patented Feb. 13, 1973 BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is an ocean elevation view of a torpedo employing the ballast release device;
FIG. 2 is a longitudinal cross sectional view of the exercise section employing the ballast release device for an exercise torpedo;
FIG. 3 is a transverse section of the exercise torpedo showing the top pair of weights, retention means, and bottom weight in cross-section; and
FIGS. 4 through 7 illustrate the ballast release device in operation.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawings wherein like reference numerals designate like or similar parts throughout the several views there is shown in FIG. 1 a water vehicle, such as a torpedo, which has a ballast release device for releasing weights from the vehicle when it is desired to render it buoyant for retrieval purposes. In an exercise torpedo, there is a special exercise section 10 which is joined to forward and after portions of the torpedo by any conventional joiner, such as that disclosed in Patent 3,100,121 to Hillmer. The section 10 of the torpedo is a hull portion which is substantially cylindrical and which includes the present ballast release device 12.
As best illustrated in FIG. 2, the exercise hull section 10 is provided with an annular recess 14 which circumscribes the torpedo and which may have opposed inwardly tapered walls 16. A plurality of weights 18, which may be constructed of lead, are disposed within the recess 14. The weights 18 may be a plurality of wedge shaped blocks which are adapted to fit and substantially fill the annular recess 14 in consecutive fashion, as illustrated in FIG. 3.
In order to provide a snap away release of the weights 18 from the torpedo a resilient band 20, which may be constructed from spring steel, may extend around the weights 18 and may be secured thereto in a closed biased position, as illustrated in FIG. 3. A means 22, which will be described in more detail hereinafter, releasably connects the ends of the bands in this closed biased position. The band 20, because of its resiliency, is adapted to as sume a relaxed open position away from the cylindrical hull section 10. In the preferred embodiment the relaxed position is substantially flat, as illustrated in FIG. 3. With such an arrangement, a release of the ends of the band 20 will cause the band and its attached weights 18 to snap free of the torpedo and render the torpedo buoyant for recovery purposes.
It is desirable that the band 20 in its closed connected position assume an outer shape which forms a substantially smooth continuation with the hull section 10. As illustrated in FIG. 2, the continuation with the hull may be accomplished by providing the hull with annular depressions 2.4 of substantially the same thickness as the band 20 at the top opposing edges of the recess '14. In order that the attachment of the weights 18 to the band 20 not interrupt the smooth configuration of the exterior surface of the band, the heads of mounting bolts 26 may be attached to the interior surface of the band by any suitable means, such as welding. A pair of the bolts 26 extend radially inwardly through each weight 18 and are secured to the weights by nuts threaded on their opposite ends. Each weight 18 is provided with a pair of notches 28 which provide clearances for the nuts so that they do not interfere with the bottom of the recess 14.
As illustrated in FIG. 3, the releasable means 22 for the band 20 may include a retainer block 30 which is split into two portions. The end weights 18 on the band 20 may be provided with opposing recesses for receiving this retainer block. One block portion may be attached to the inner surface of the band 20 adjacent one end thereof and the other block portion may be attached to the inner surface of the band adjacent the other end thereof. Specially configured brackets 32 may be provided for making these attachments. The end portions of each bracket 32 may be welded to the interior surface of the band 20 and the block portions may be mounted thereto by bolts 34.
In order to join and subsequently separate the block portions 30 an explosive bolt 36 may be provided which extends through both block portions and is threaded into at least one of the block portions for retention purposes. The bolt 36 contains an internal explosive which separates the bolt, and this explosive is detonated by an electrical lead 38. The lead 38 extends into a center portion of the torpedo through a fitting 40 and is actuated by instrumentation (not shown) which is set for a predetermined release time. In order to prevent explosive bolt fragmentation of the block 30 the block may be provided with an internal substantially cylindrical cavity 42, and within this cavity there may be provided a ring collar 44 which bridges the joint of the retainer block portions.
OPERATION OF THE INVENTION In the operation of the present invention the ballast release device 12 is mounted to the torpedo prior to the exercise run. After the run is completed instrumentation within the torpedo sends a signal to the explosive bolt 36 which causes the bolt to separate Within the retainer block 30. Upon this occurrence the retainer block portions are separated and the resiliency of the band 20 causes the band and the attached weights 18 to quickly snap away from the torpedo. This renders the torpedo buoyant so that it can be recovered at the surface by a surface ship.
Obviously many modifications and variations of the the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
We claim: 1. In a vehicle having a cylindrical hull, a snap-acting ballast release device comprising; 7
said hull having an annular recess;
a plurality of weights disposed within said recess;
a resilient band extending around the weights and secured thereto in a closed biased position;
means releasably connecting the ends of said band in the closed biased position;
said band being adapted, because of its resiliency, to
assume a relaxed open position away from the cylindrical hull;
said band having in its closed connected position an outer shape which forms a smooth continuation of the hull shape;
said weights being wedge shaped and secured directly to the inner service of the resilient band in a substantially continuous fashion thereal'ong when the band is in a closed biased position;
and said weights being secured to the resilient band by bolts which are welded to the inner surface of the band, whereby upon release of the ends of the'band, the band and its attached weights snap free of the vehicle.
2. A combination as claimed in claim 1 including;
the relaxed open position of the band being substantially flat.
3. A combination as claimed in claim 2 including:
the recess having annular opposed inwardly tapered walls; and
each weight being configured to substantially fit and fill an annular segment of said recess.
References Cited UNITED STATES PATENTS 3,404,649 10/1968 Valihora 114-20 R 3,115,836 12/1963 Brashears 102-49.5 2,890,670 6/ 1959 Le Francois 114-22 3,513,512 5/1970 Phillips 24-279 3,109,216 11/1963 Brown 24-279 2,712,326 7/ 1955 Yurdin 24-279 X BENJAMIN A. BORCHELT, Primary vExaminer J. M. HANLEY, Assistant Examiner US. Cl. X.R. 102-495
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US8266170A | 1970-10-21 | 1970-10-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3716010A true US3716010A (en) | 1973-02-13 |
Family
ID=22172585
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00082661A Expired - Lifetime US3716010A (en) | 1970-10-21 | 1970-10-21 | Snap acting ballast release device |
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US (1) | US3716010A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4280407A (en) * | 1979-05-21 | 1981-07-28 | C-I-L Inc. | Explosive package assembly |
US4530269A (en) * | 1983-05-12 | 1985-07-23 | Burroughs Corp. | Remotely initiated separation latch assembly |
DE3617429A1 (en) * | 1986-05-23 | 1995-03-09 | Diehl Gmbh & Co | Method for attacking submarines, and a missile for carrying out the method |
US6403873B1 (en) * | 2000-08-22 | 2002-06-11 | The United States Of America As Represented By The Secretary Of The Navy | Torpedo joint band with in-water separation capability utilizing frangible link EEDs |
-
1970
- 1970-10-21 US US00082661A patent/US3716010A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4280407A (en) * | 1979-05-21 | 1981-07-28 | C-I-L Inc. | Explosive package assembly |
US4530269A (en) * | 1983-05-12 | 1985-07-23 | Burroughs Corp. | Remotely initiated separation latch assembly |
DE3617429A1 (en) * | 1986-05-23 | 1995-03-09 | Diehl Gmbh & Co | Method for attacking submarines, and a missile for carrying out the method |
US6403873B1 (en) * | 2000-08-22 | 2002-06-11 | The United States Of America As Represented By The Secretary Of The Navy | Torpedo joint band with in-water separation capability utilizing frangible link EEDs |
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