US2998769A - Rocket launched noisemaker - Google Patents
Rocket launched noisemaker Download PDFInfo
- Publication number
- US2998769A US2998769A US325497A US32549752A US2998769A US 2998769 A US2998769 A US 2998769A US 325497 A US325497 A US 325497A US 32549752 A US32549752 A US 32549752A US 2998769 A US2998769 A US 2998769A
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- United States
- Prior art keywords
- float
- shell
- rod
- rocket
- secured
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B22/00—Buoys
- B63B22/003—Buoys adapted for being launched from an aircraft or water vehicle;, e.g. with brakes deployed in the water
Definitions
- the present invention relates to a rocket launched noisernaker and more particularly to a flotation system used as an integral part of the apparatus.
- Prior art de vices of this character are not always reliable when submerged in water since the design of the flotation system is such that the device will not assume a buoyant position under all conditions of operation.
- a further problem is present when chemicals are employed for the generation of gas used in the flotation system, since such chemicals are usually subject to deterioration when exposed to the atmosphere prior to use. In the event of such exposure, the chemical substances will not effervesce and it is not possible to liberate the gas necessary for buoyant purposes.
- the apparatus containing chemicals is stored for long periods of time, the life of the chemicals is diminished to such an extent that proper operation of the device is also not possible.
- This invention is directed to an improved flotation system wherein all of the operating parts are strictly mechanical in nature and dependence of operation is not placed on chemically acting substances. All of such parts are positive acting, thereby precluding the possibility of the noisernaker becoming inoperative when launched from a vessel.
- a further feature of the invention in volves control of the time element with respect to the destruction of the device after it has been in operation for a predetermined period of time. The apparatus is therefore safer to handle, no storage or shipping precautions are necessary, one unit is adaptable for use when firing same at various ranges from the vessel, and it is less expensive to manufacture.
- An object of the present invention is to provide. an improved flotation system for buoyant bodies.
- Another object of the invention is to provide a single or plurality of buoyant elements for assuring positive flotation of the device.
- a further object is the provision of an adapter which accommodates rockets of various sizes for firing the device at various ranges from the launching vessel.
- a final object of the present invention is the provision of means for separating the elements within the body of the device in order to insure proper flotation of the apparatus in water.
- FIG. 1 is a plan view of the device with sections broken away showing the various elements and their location with respect to one another;
- FIG. 2 is a view taken on lines 22 of FIG. 1.
- FIG. 1 a tube weldment or shell which houses the various elements comprising the flotation system 11 and a sea battery 12 for supplying power to a motor-operated noisemaking device 14.
- the specific construction and details of the sea battery and noisemaking device are not pertinent to this invention and further description thereof will not be included herein.
- a type such as that disclosed by Vivian L. Chrisler et al. in copending application Serial No. 339,498, filed February 27, 1953, may be used with the instant invention.
- the flotation system enclosed by shell 10 comprises three main elements, namely, a head sub-assembly 16, a control float 18 and main float 20.
- Themain elements are assembled in tandem and are assembled within'a shell 10 for storage, handling, and launching.
- the units are releasably secured together by means of a central rod secured to the noisernaker and extending through the several units to a releasable engagement in the head subassembly 16 as hereinafter described.
- the head sub-assembly 16 consists of a cylindrical body 21 having steps thereon at 22 for receiving a rocket adapter 24.
- This rocket adapter has a protruding head which is both internally and externally threaded so that the noisernaker may be secured to various sizes of rockets used for launching the noisernaker from a vessel into the sea.
- the adapter is secured to the cylindrical body 21 by means of a thumb screw 26. Central and lateral bores 28 and 30 are drilled into the cylindrical body 21 for a purpose hereinafterdescribed.
- the cylindrical body has a protruding outer flange or base 31 which is adapted to fit within shell 10 and is held in water-tight engagement therewith by means of O-ring 32.
- the spring 34 is fitted within shell 10 and is biased against cylindrical body 21 at one end and against the upper surface of control float 18 at its other end. When the noisernaker is assembled, this spring is in a compressed condition thereby exerting-a force on each of these two members.
- the control float 18 is cylindrical in shape and is provided with a central opening extending longitudinally therethrough, thereby providing a passageway for rod 36 which extends throughthe opening and terminates near the upper end of the float;
- the control float 18 is preferably made in two sections which are fitted together to form a water-tight fit and has metering orifices 38 in the bottom and top portions so as to allow water to enter through the orifice at the bottom, the orifice at the top being utilized as a vent for venting air which is displaced by the water in the float.
- the main float 20 is made of a material such as balsa wood, cellulose, foam rubber, or expanded Royalite made by U.S. Rubber Company, which has a'- small specific gravity so as to have excellent buoyant characteristics. It is positioned below the control float 18. in shell 10 and is provided with a countersunk opening 40 in the bottom thereof for receiving a collar 42.
- a spider 44 is adapted to fit within shell 10 and is centrally bored. to provide access for rod 36. This spider has one side thereof held in engagement with sea battery 12 by means of the collar 42 which is held in position against the other side of the spider by means of a set screw 46 adapted to engage rod 36.
- the sea battery likewise has a central longitudinal opening for receiving the lower end of rod 36 which is threadably secured to plate 51 fitted in thebottom end of shell 10.
- a second spider 48 bears against the bottom side of sea battery 12 and is held thereagainst by means of spacer 50.
- the upper portion of the motor-operated noisernaker 14 is connected to the plate 51 which is in turn connected to the bottom end of shell 10, as shown at 53.
- the upper portion of the motor operated noisernaker 14 is made water-tight to the plate 51 by mean's'of O-ring 70.
- Appropriate conductors 72 extend from the sea battery to the motor for operation thereof.
- rod 36 terminates at a point adjacent the upper surface of control float 18.
- a coupling 52 is secured at one end to rod 36, the other end of the coupling being attached to a short section of stainless steel rod 54.
- the steel rod 54 has a portion of reduced diameter for receiving locking pin 56.
- This locking pin 56 rests in lateral bore 3t? and has a shoulder milled thereon for receiving a spring 58 which acts to move the locking pin out of engagement with rod 54.
- Threaded screw 60 holds the locking pin and spring in engagement with rod 54 under all conditions until the unit is prepared for use.
- a thin washer 62 is adapted to rest on the top of control float 18 and cord 64 is secured at one end to the washer and extends beneath float 18 where it is laid in the shell in a side to side manner, the other end of the cord being secured to rod 36 at the point where coupling 52 is secured to the rod.
- a rocket is attached to rocket adapter 24, nut 60 is backed off to provide movement of locking pin 56 and the noisemaker is subsequently fired from the ship.
- the force transmited from the rocket to the unit urges cylindrical body 21 in a forward direction, or to the right as shown in FIG. 1, thereby allowing spring 58 to move locking pin 56 out of engagement with the reduced section of rod 54.
- compressed spring 34 acts to eject the cylindrical body 21 and the appurtenances secured thereto into the sea.
- the shell will continue in a smooth path of travel and strike the water at varying distances from the ship, determined by the type of rocket used for launching the noisemaker.
- control float 18 will leave shell 10 and ascend to the surface, thus carrying with it, washer 62 and cord 64 which is securely attached thereto.
- the cord 64 will pay out as the control float 13 rises to the surface, and main float 20, because of its buoyant characteristics, will also rise to the surface and assume a position underneath control float 18, and it will remain in this position since cord 64 extends down through the center of float 29, thus making lateral displacement impossible. It is not necessary that main float 29 leave the shell 10 since it will buoy the unit in any event.
- control float 18 is void of water but immediately starts to fill through the orifice in the bottom, the air being vented through orifice 38 at the top.
- a flotation system for use with a submerged body, comprising a hollow cylindrical shell closed at one end and open at the other, a float having a central opening positioned in said shell, 2. rod secured at one end to the closed portion of said shell and arranged to extend through the central opening of said float, float releasing means secured in the open end of said shell, a longitudinal bore in said releasing means for receiving the other end of said rod, a portion of reduced diameter adjacent said other end of said rod, a lateral bore in said float releasing means, a locking pin in said lateral bore for engaging the reduced portion of said rod, and resilient means in said shell acting on said float releasing means for biasing said locking pin in. frictional engagement with said reduced portion of said rod, said locking pin being movable and provided with means adapting it for disengagement of the reduced portion upon compression of the resilient means, whereby the float releasing means will be ejected from said shell.
- spring means biases said locking pin in a direction away from rod engagement
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- General Engineering & Computer Science (AREA)
Description
Sept. 5, 1961 R. P. CRIST ROCKET LAUNCHED NOISEMAKER Filed Dec. 11, 1952 INVENTOR RALPH P. CRIST ATTORNEYS #N mu 2,998,769 Patented Sept. 5, 1961 2,998,769 ROCKET LAUNCIED NOISEMAIER Ralph P. Crist, 1925 N. Calvert t., Apt. 203, Arlington, Va. Filed Dec. 11, 1952, Ser. No. 325,497
3 Claims. (Cl. 1027) (Granted under Title 35, U.S. Code (1952), sec. 266) The invention herein described 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.
The present invention relates to a rocket launched noisernaker and more particularly to a flotation system used as an integral part of the apparatus. Prior art de vices of this character are not always reliable when submerged in water since the design of the flotation system is such that the device will not assume a buoyant position under all conditions of operation. A further problem is present when chemicals are employed for the generation of gas used in the flotation system, since such chemicals are usually subject to deterioration when exposed to the atmosphere prior to use. In the event of such exposure, the chemical substances will not effervesce and it is not possible to liberate the gas necessary for buoyant purposes. In addition to this, if the apparatus containing chemicals is stored for long periods of time, the life of the chemicals is diminished to such an extent that proper operation of the device is also not possible.
This invention is directed to an improved flotation system wherein all of the operating parts are strictly mechanical in nature and dependence of operation is not placed on chemically acting substances. All of such parts are positive acting, thereby precluding the possibility of the noisernaker becoming inoperative when launched from a vessel. A further feature of the invention in volves control of the time element with respect to the destruction of the device after it has been in operation for a predetermined period of time. The apparatus is therefore safer to handle, no storage or shipping precautions are necessary, one unit is adaptable for use when firing same at various ranges from the vessel, and it is less expensive to manufacture.
An object of the present invention is to provide. an improved flotation system for buoyant bodies.
Another object of the invention is to provide a single or plurality of buoyant elements for assuring positive flotation of the device.
A further object is the provision of an adapter which accommodates rockets of various sizes for firing the device at various ranges from the launching vessel.
A final object of the present invention is the provision of means for separating the elements within the body of the device in order to insure proper flotation of the apparatus in water.
With these and other objects in view as will herein-' after more fully appear, and which will be more particularly pointed out in the appended claims, reference is now made to the following description taken in connection with the accompanying drawings in which:
FIG. 1 is a plan view of the device with sections broken away showing the various elements and their location with respect to one another; and
FIG. 2 is a view taken on lines 22 of FIG. 1.
Referring now to the drawings wherein like reference characters designate like or corresponding parts throughout the several views, there is shown in FIG. 1 a tube weldment or shell which houses the various elements comprising the flotation system 11 and a sea battery 12 for supplying power to a motor-operated noisemaking device 14. The specific construction and details of the sea battery and noisemaking device are not pertinent to this invention and further description thereof will not be included herein. However, a type such as that disclosed by Vivian L. Chrisler et al. in copending application Serial No. 339,498, filed February 27, 1953, may be used with the instant invention.
The flotation system enclosed by shell 10, comprises three main elements, namely, a head sub-assembly 16, a control float 18 and main float 20. Themain elements are assembled in tandem and are assembled within'a shell 10 for storage, handling, and launching. The units are releasably secured together by means of a central rod secured to the noisernaker and extending through the several units to a releasable engagement in the head subassembly 16 as hereinafter described.
The head sub-assembly 16 consists of a cylindrical body 21 having steps thereon at 22 for receiving a rocket adapter 24. This rocket adapter has a protruding head which is both internally and externally threaded so that the noisernaker may be secured to various sizes of rockets used for launching the noisernaker from a vessel into the sea. The adapter is secured to the cylindrical body 21 by means of a thumb screw 26. Central and lateral bores 28 and 30 are drilled into the cylindrical body 21 for a purpose hereinafterdescribed. The cylindrical body has a protruding outer flange or base 31 which is adapted to fit within shell 10 and is held in water-tight engagement therewith by means of O-ring 32. The spring 34 is fitted within shell 10 and is biased against cylindrical body 21 at one end and against the upper surface of control float 18 at its other end. When the noisernaker is assembled, this spring is in a compressed condition thereby exerting-a force on each of these two members.
The control float 18 is cylindrical in shape and is provided with a central opening extending longitudinally therethrough, thereby providinga passageway for rod 36 which extends throughthe opening and terminates near the upper end of the float; The control float 18 is preferably made in two sections which are fitted together to form a water-tight fit and has metering orifices 38 in the bottom and top portions so as to allow water to enter through the orifice at the bottom, the orifice at the top being utilized as a vent for venting air which is displaced by the water in the float.
The main float 20 is made of a material such as balsa wood, cellulose, foam rubber, or expanded Royalite made by U.S. Rubber Company, which has a'- small specific gravity so as to have excellent buoyant characteristics. It is positioned below the control float 18. in shell 10 and is provided with a countersunk opening 40 in the bottom thereof for receiving a collar 42. A spider 44 is adapted to fit within shell 10 and is centrally bored. to provide access for rod 36. This spider has one side thereof held in engagement with sea battery 12 by means of the collar 42 which is held in position against the other side of the spider by means of a set screw 46 adapted to engage rod 36. The sea battery likewise has a central longitudinal opening for receiving the lower end of rod 36 which is threadably secured to plate 51 fitted in thebottom end of shell 10. A second spider 48 bears against the bottom side of sea battery 12 and is held thereagainst by means of spacer 50. The upper portion of the motor-operated noisernaker 14 is connected to the plate 51 which is in turn connected to the bottom end of shell 10, as shown at 53. The upper portion of the motor operated noisernaker 14 is made water-tight to the plate 51 by mean's'of O-ring 70. Appropriate conductors 72 extend from the sea battery to the motor for operation thereof.
As afore-mentioned, rod 36 terminates at a point adjacent the upper surface of control float 18. A coupling 52 is secured at one end to rod 36, the other end of the coupling being attached to a short section of stainless steel rod 54. The steel rod 54 has a portion of reduced diameter for receiving locking pin 56. This locking pin 56 rests in lateral bore 3t? and has a shoulder milled thereon for receiving a spring 58 which acts to move the locking pin out of engagement with rod 54. Threaded screw 60 holds the locking pin and spring in engagement with rod 54 under all conditions until the unit is prepared for use. A thin washer 62 is adapted to rest on the top of control float 18 and cord 64 is secured at one end to the washer and extends beneath float 18 where it is laid in the shell in a side to side manner, the other end of the cord being secured to rod 36 at the point where coupling 52 is secured to the rod.
The operation of the device is as follows:
A rocket is attached to rocket adapter 24, nut 60 is backed off to provide movement of locking pin 56 and the noisemaker is subsequently fired from the ship. The force transmited from the rocket to the unit urges cylindrical body 21 in a forward direction, or to the right as shown in FIG. 1, thereby allowing spring 58 to move locking pin 56 out of engagement with the reduced section of rod 54. When this occurs, compressed spring 34 acts to eject the cylindrical body 21 and the appurtenances secured thereto into the sea. The shell will continue in a smooth path of travel and strike the water at varying distances from the ship, determined by the type of rocket used for launching the noisemaker. As the noisemaker strikes the water and becomes immersed therein, control float 18 will leave shell 10 and ascend to the surface, thus carrying with it, washer 62 and cord 64 which is securely attached thereto. The cord 64 will pay out as the control float 13 rises to the surface, and main float 20, because of its buoyant characteristics, will also rise to the surface and assume a position underneath control float 18, and it will remain in this position since cord 64 extends down through the center of float 29, thus making lateral displacement impossible. It is not necessary that main float 29 leave the shell 10 since it will buoy the unit in any event. At the time operation of the device commences, control float 18 is void of water but immediately starts to fill through the orifice in the bottom, the air being vented through orifice 38 at the top. These orifices are of such size that the rate of flooding of water will take a predetermined time to fill the float due to the size of such orifices. When the float completely fills with water the complete unit then assumes negative buoyancy and sinks to the bottom of the ocean.
It will be readily apparent to those skilled in the art that only a preferred modification has been described herein, and that many changes therein are possible without departing from the spirit of the present invention. It should be understood, of course, that it is intended to cover all changes and modifications of the example of the invention herein chosen for the purposes of the disclosure, which do not constitute departures from the spirit and scope as set forth in the appended claims.
What is claimed is:
1. A flotation system for use with a submerged body, comprising a hollow cylindrical shell closed at one end and open at the other, a float having a central opening positioned in said shell, 2. rod secured at one end to the closed portion of said shell and arranged to extend through the central opening of said float, float releasing means secured in the open end of said shell, a longitudinal bore in said releasing means for receiving the other end of said rod, a portion of reduced diameter adjacent said other end of said rod, a lateral bore in said float releasing means, a locking pin in said lateral bore for engaging the reduced portion of said rod, and resilient means in said shell acting on said float releasing means for biasing said locking pin in. frictional engagement with said reduced portion of said rod, said locking pin being movable and provided with means adapting it for disengagement of the reduced portion upon compression of the resilient means, whereby the float releasing means will be ejected from said shell.
2. The combination according to claim 1 wherein spring means biases said locking pin in a direction away from rod engagement;
3. The combination according to claim 1 wherein an adapter is secured to the outer end of said float releasing means, and rocket attaching means atfixed to said adapter for accommodating various sizes of rockets.
References Cited in the file of this patent UNITED STATES PATENTS 910,942 McCombie Ian. 26, 1909 927,772 Brust July 13, 1909 1,295,213 Saladiner Feb. 25, 1919 1,312,114 Harvey Aug. 5, 1919 1,442,345 Kee Ian. 16, 1923 1,449,168 Elia Mar. 20, 1923 2,375,893 Caulkins May 15, 1945 2,395,252 Carpenter Feb. 19, 1946 2,521,516 Heidman et a1. Sept. 5, 1950 2,586,828 Keeran Feb. 26, 1952 2,637,862 Freas May 12, 1953
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US325497A US2998769A (en) | 1952-12-11 | 1952-12-11 | Rocket launched noisemaker |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US325497A US2998769A (en) | 1952-12-11 | 1952-12-11 | Rocket launched noisemaker |
Publications (1)
Publication Number | Publication Date |
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US2998769A true US2998769A (en) | 1961-09-05 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US325497A Expired - Lifetime US2998769A (en) | 1952-12-11 | 1952-12-11 | Rocket launched noisemaker |
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US (1) | US2998769A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5117731A (en) * | 1991-11-04 | 1992-06-02 | The United States Of America As Represented By The Secretary Of The Navy | Tactical acoustic decoy |
US7392733B1 (en) * | 2004-09-20 | 2008-07-01 | The United States Of America As Represented By The Secretary Of The Navy | High resolution projectile based targeting system |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US910942A (en) * | 1905-12-18 | 1909-01-26 | John Bedell Stanford Macilwaine | Explosive mine or projectile. |
US927772A (en) * | 1908-05-13 | 1909-07-13 | Frank P Brust | Combined wreck-locator and life-saver. |
US1295213A (en) * | 1917-10-01 | 1919-02-25 | Joseph M Saladiner | Multiple submarine-destroyer. |
US1312114A (en) * | 1919-08-05 | District of coltocbia | ||
US1442345A (en) * | 1917-07-23 | 1923-01-16 | Charles L Kee | Aircraft-launched temporary drifting mine |
US1449168A (en) * | 1920-09-13 | 1923-03-20 | Vickers Ltd | Submarine mine |
US2375893A (en) * | 1941-04-24 | 1945-05-15 | Cecil P Caulkins | Projectile |
US2395252A (en) * | 1944-06-27 | 1946-02-19 | Nasa | Impact operated release mechanism |
US2521516A (en) * | 1945-07-13 | 1950-09-05 | William A Heidman | Automatic load releasing clutch for parachutes and the like |
US2586828A (en) * | 1950-01-19 | 1952-02-26 | Royal V Keeran | Radio buoy |
US2637862A (en) * | 1948-06-18 | 1953-05-12 | Raymond L Freas | Buoyant chamber scuttling device |
-
1952
- 1952-12-11 US US325497A patent/US2998769A/en not_active Expired - Lifetime
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1312114A (en) * | 1919-08-05 | District of coltocbia | ||
US910942A (en) * | 1905-12-18 | 1909-01-26 | John Bedell Stanford Macilwaine | Explosive mine or projectile. |
US927772A (en) * | 1908-05-13 | 1909-07-13 | Frank P Brust | Combined wreck-locator and life-saver. |
US1442345A (en) * | 1917-07-23 | 1923-01-16 | Charles L Kee | Aircraft-launched temporary drifting mine |
US1295213A (en) * | 1917-10-01 | 1919-02-25 | Joseph M Saladiner | Multiple submarine-destroyer. |
US1449168A (en) * | 1920-09-13 | 1923-03-20 | Vickers Ltd | Submarine mine |
US2375893A (en) * | 1941-04-24 | 1945-05-15 | Cecil P Caulkins | Projectile |
US2395252A (en) * | 1944-06-27 | 1946-02-19 | Nasa | Impact operated release mechanism |
US2521516A (en) * | 1945-07-13 | 1950-09-05 | William A Heidman | Automatic load releasing clutch for parachutes and the like |
US2637862A (en) * | 1948-06-18 | 1953-05-12 | Raymond L Freas | Buoyant chamber scuttling device |
US2586828A (en) * | 1950-01-19 | 1952-02-26 | Royal V Keeran | Radio buoy |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5117731A (en) * | 1991-11-04 | 1992-06-02 | The United States Of America As Represented By The Secretary Of The Navy | Tactical acoustic decoy |
US7392733B1 (en) * | 2004-09-20 | 2008-07-01 | The United States Of America As Represented By The Secretary Of The Navy | High resolution projectile based targeting system |
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