US20040031381A1 - Apparatus for launching an object in a fluid environment - Google Patents

Apparatus for launching an object in a fluid environment Download PDF

Info

Publication number
US20040031381A1
US20040031381A1 US10/224,229 US22422902A US2004031381A1 US 20040031381 A1 US20040031381 A1 US 20040031381A1 US 22422902 A US22422902 A US 22422902A US 2004031381 A1 US2004031381 A1 US 2004031381A1
Authority
US
United States
Prior art keywords
gas
expellable
tubular member
muzzle
flood
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.)
Granted
Application number
US10/224,229
Other versions
US6701819B1 (en
Inventor
Michael Williams
Paul Moody
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.)
US Government
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US10/224,229 priority Critical patent/US6701819B1/en
Assigned to THE UNITED STATES OF AMERICA reassignment THE UNITED STATES OF AMERICA ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MOODY, PAUL E., WILLIAMS, MICHAEL W.
Publication of US20040031381A1 publication Critical patent/US20040031381A1/en
Application granted granted Critical
Publication of US6701819B1 publication Critical patent/US6701819B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/07Underwater launching-apparatus

Definitions

  • the present invention generally relates to an apparatus for launching an object in a fluid environment.
  • the present invention is directed to an apparatus for launching an object into a fluid environment such as oceans, rivers, lakes, or any fluid or liquid contained within any man-made structure or made-made earthen works.
  • the apparatus comprises a tubular member having a forward muzzle end and an opposed rearward end.
  • the tubular member has a longitudinally extending axis, an interior region for receiving an object to be launched, an exterior wall confronting the fluid environment and an interior wall.
  • the apparatus further includes expellable members for closing the forward muzzle end and rearward end of the tubular member, at least one flood valve member located on a corresponding expellable member for enabling fluid confronting the exterior wall to flood the interior region so as to equalize forces on the interior and exterior walls of the tubular member, and an object contact member disposed within the interior region and movable along the longitudinally extending axis.
  • the object contact member contacts and moves the object when a propelling force is applied to the object contact member.
  • the apparatus further includes a propellant device for producing the propelling force.
  • the device contains a gas generator and is configured to generate gas in controlled amounts that are sufficient to propel the object contact member in the direction of the forward muzzle end.
  • the apparatus further includes a control device that controls the flood valve member, the expellable members and the propellant device in accordance with a predetermined timed sequence wherein the control device first controls the flood valve to allow fluid to flood the interior region. Thereafter, the control device causes the expellable members to be expelled from the forward muzzle end and rearward end. Thereafter, the control device controls the propellant device to release generated gas in successive bursts so as to produce a continuous propelling force that causes the object contact member to propel the object through the tubular member, out through the forward end muzzle and into the fluid surrounding the tubular member.
  • the successive bursts of generated gas are preferably uniform, continuous and stable thereby resulting in a fully stable ejection of the object at a relatively high exit velocity.
  • FIG. 1 is a combination side-elevational view, partially in cross-section, and schematic diagram of the apparatus of the present invention
  • FIG. 2 is a combination side-elevational view, partially in cross-section, and schematic diagram of one embodiment of the apparatus of the present invention.
  • FIG. 3 is a view taken along line 3 - 3 in FIG. 2.
  • FIGS. 1 - 3 of the drawings in which like numerals refer to like features of the invention.
  • Apparatus 10 generally comprises tubular member 12 which has forward muzzle end 14 and opposed rearward end 16 .
  • Tubular member 12 has longitudinally extending axis 18 and interior region 20 for receiving object 22 (e.g. vehicle, torpedo, weapon, buoy, hydroplane, etc.) that is to be launched into the fluid environment surrounding apparatus 10 .
  • object 22 e.g. vehicle, torpedo, weapon, buoy, hydroplane, etc.
  • Tubular member 12 can be made from any rigid material including metals, composites and plastics.
  • the term “fluid environment” includes oceans, rivers, lakes, or any body of fluid or liquid contained within any man-made structure or made-made earthen works.
  • tubular member 12 comprises a barrel. Such a barrel is described in U.S.
  • Apparatus 10 includes clamping device 23 that allows tubular member 12 to be attached to the hull of a vessel such as a ship, submarine or any other vessel or device that travels through such a fluid environment.
  • clamping device 23 is configured to allow tubular member 12 to be releasably attached to the vessel. Such a configuration enables tubular member 12 to be released from the vessel after object 22 is launched.
  • tubular member 12 has interior wall 24 and exterior wall 26 confronting the fluid environment.
  • Apparatus 10 includes a muzzle expellable member 28 and breech expellable member 30 for closing the forward muzzle end 14 and opposed rearward end 16 of tubular member 12 .
  • apparatus 10 further comprises flood valve members 32 for enabling fluid external to tubular member 12 to flood interior region 20 in a controlled manner so as to minimize water hammer effects, especially at relatively deep depths.
  • One flood valve member 32 is located on expellable member 28 .
  • the other flood valve member 32 is located on expellable member 30 .
  • Flood valve or valves 32 can be positioned on tubular member 12 in an alternate embodiment.
  • each flood valve 32 comprises an exploding valve that is exploded upon receipt of an electrical control signal. Once flood valve 32 explodes, fluid enters interior region 20 .
  • Apparatus 10 includes a plurality of exploding bolts 34 for attaching muzzle expellable member 28 to the forward muzzle end 14 and breech expellable member 30 to the opposed rearward end 16 .
  • Exploding bolts 34 are exploded upon receipt of an electrical control signal. Explosion of bolts 32 propels expellable members 28 and 30 away from tubular member 12 .
  • apparatus 10 further comprises object contact member 36 disposed within interior region 20 and movable along longitudinally extending axis 18 .
  • Object contact member 36 contacts at contact surface 37 and moves object 22 when a propelling force is applied to the object contact member 36 .
  • object contact member 36 is generally cylindrical in shape and defines an interior space 38 .
  • object contact member 36 comprises a sabot.
  • tubular member 12 includes a rail (not shown) that longitudinally extends within interior region 20 .
  • object contact member 36 is movably mounted on the rail.
  • apparatus 10 further includes propellant device 40 for producing a propelling force.
  • Propellant device 40 is disposed within interior space 38 of object contact member 36 .
  • Device 40 produces a propelling force that propels object contact member 36 .
  • propellant device 40 is a plurality of chemical or hybrid gas generators and is configured to release generated gas via exit or exhaust opening 41 in controlled amounts that are sufficient to propel object contact member 36 .
  • Device 40 includes an electrical interface 42 that is configured to receive an electrical control signal that effects generation of the gas. The propelling force resulting from the release of the gas propels object contact member 36 and object 22 in the direction indicated by arrow 43 and toward forward muzzle end 14 .
  • object contact member 36 Prior to the generation of gas from device 40 , object contact member 36 is positioned so that device 40 is located near opposed rearward end 16 .
  • gas generator device 40 comprises a plurality of chemical gas generators 44 wherein each gas generator 44 can generate a predetermined amount of gas that is emitted from exit or exhaust opening 45 of each device 44 .
  • Gas generators 44 can be chemical gas generators or hybrid gas generators incorporating a chemical gas generator with compressed gas. Compressed gas, in standard packaging, does not have sufficient energy density to effect a launch.
  • Each generator 44 includes an electrical interface 46 for receiving an electrical control signal that effects generation of the gas in the corresponding gas generator device 44 .
  • exit 45 of each device 44 faces breech expellable member 30 .
  • the plurality of gas generators 44 are symmetrically arranged.
  • each gas generator 44 comprises a canister containing a gas generating compound or a gas generating compound and a compressed gas as is well known in the art of automobile airbag inflation devices.
  • wires 48 are not shown in FIG. 3.
  • apparatus 10 further comprises control device 47 .
  • Control device 47 is preferably located on board the vessel, ship or other device to which tubular member 12 is attached.
  • Control device 47 contains electrical circuitry and electronic components that generate electrical signals that are transferred by wires 48 to explosive bolts 34 , explosive flood valves 32 , and interface 42 of device 40 .
  • Control device 47 is configured so the electrical signals are generated in a predetermined order and are separated by a predetermined time duration. In such a configuration, control device 47 first produces electrical signals that cause explosive valves 32 to 1 s flood interior region 20 so as to equalize the pressures on interior wall 24 and exterior wall 26 of the tubular member 12 .
  • control device 47 After a predetermined amount of time has elapsed which is sufficient to allow interior region 20 to completely flood, control device 47 outputs electrical signals that cause explosion of explosive bolts 34 so as to expel expellable members 28 and 30 from forward muzzle end 14 and opposed rearward end 16 , respectively. After a predetermined amount of time has elapsed which is sufficient to allow expellable members 28 and 30 to fall away from tubular member 12 , control device 47 outputs electrical signals to interface 46 of device 40 to enable device 40 to generate gas in successive bursts so as to produce a continuous propelling force that is applied to object contact member 36 . As a result, object contact member 36 propels object 22 through tubular member 12 and out through forward muzzle end 14 .
  • control device 44 If device 40 is comprised of the plurality of gas generators 44 as shown in FIGS. 2 and 3, then wires 48 are connected to each electrical interface 46 of each gas generator 44 .
  • control device 44 generates electrical signals in a predetermined timed sequence so that each gas generator 44 generates gas in accordance with the predetermined timed sequence.
  • the predetermined timed sequence effects generation of gas from each gas generator 44 in a sequential order.
  • the gas generators 44 produce sufficient thrust to create a continuous, even, and stable ejection force during the entire launch of object 22 and causes object 22 to have a relatively high exit velocity as it exits tubular member 12 . Since expellable member 30 is expelled from tubular member 12 before the compressed gas is released, the full thrust produced by the released gas is utilized to accelerate object 22 during launch without any thrust being used to overcome sea pressure. Thus, the plurality of gas generators 44 located within interior space 38 of object contact member 36 in conjunction with the predetermined time sequence in which each generator 44 generates its gas results in a full-power stroke ejection of object 22 .
  • clamping means 23 is configured to include an electrical interface that is electrically connected to wires 48 .
  • apparatus 10 reduces the danger associated with explosive solid and liquid propellants. Furthermore, the design of apparatus 10 is relatively less complex than prior art systems and, therefore, can be implemented at relatively lower costs and with commercially available components. Additionally, apparatus 10 provides a consistent, continuous and even propelling force that is applied to the object during the entire launch process thereby resulting in a full-stroke ejection of the object. Apparatus 10 also provides for relatively high exit velocity of the object as it leaves tubular member 12 . Apparatus 10 eliminates any impact related to varying sea pressures (or ship depths).
  • apparatus 10 can be used in gaseous environment wherein object 22 is launched in the gaseous environment.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Abstract

An apparatus for launching an object in a fluid environment having a tubular member with a forward muzzle end, an opposed rearward end. The object is positioned in the tubular member. Ends of the tubular member are closed by expellable members. Flood valves are located on the expellable members and, on activation, allow flooding of the tubular member by external fluid. A propellant device and an object contact member are disposed within the tubular member. When the propellant device is activated, the object contact member moves the object. These actions are controlled by a control device which first causes the flood valves to enable fluid to flood the interior region. Next, the control device causes the expellable members to be expelled from the tubular member. The control device then causes the propellant device to generate gas in a predetermined manner launching the object from the tubular member.

Description

    STATEMENT OF GOVERNMENT INTEREST
  • [0001] 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.
  • CROSS REFERENCE TO OTHER PATENT APPLICATIONS
  • Not applicable. [0002]
  • BACKGROUND OF THE INVENTION
  • (1) Field Of The Invention [0003]
  • The present invention generally relates to an apparatus for launching an object in a fluid environment. [0004]
  • (2) Description of the Prior Art [0005]
  • Devices and systems for launching objects, weapons or vehicles into the ocean or other fluid or liquid environments are known in the art. For example, such devices are used to launch or eject buoys at relatively deep depths from a submerged submarine. Some of these devices and systems for launching objects are described in U.S. Pat. Nos. 3,476,048, 3,516,380, 4,185,345 and 5,918,307. One particular well known prior art system uses gas generators to launch objects underwater. One such system is described in U.S. Pat. No. 5,981,307 entitled “Underwater Projectile Launcher”. U.S. Pat. No. 5,981,307 discloses that the launcher described therein can use any of the well known types of chemical energy storage—solid, liquid or gaseous propellants—for generating the gas required to launch the projectile. [0006]
  • Typically, many launching systems currently in operation utilize solid propellants. In such systems, the solid propellant is ignited and gas is generated from the burning propellant. This gas is used to effect the device launch. One significant problem with such systems is that the solid propellant is highly flammable and explosive and must be handled with great care. This problem creates additional cost and expense associated with handling and storage of the solid propellant, and significantly increases the time it takes to initiate and effect a safe and successful launch of an object. [0007]
  • What is needed is an apparatus for launching an object into a fluid environment that eliminates the aforementioned deficiencies of the prior art systems which utilize gas generation to launch an object into a fluid environment. [0008]
  • SUMMARY OF THE INVENTION
  • The present invention is directed to an apparatus for launching an object into a fluid environment such as oceans, rivers, lakes, or any fluid or liquid contained within any man-made structure or made-made earthen works. In one embodiment, the apparatus comprises a tubular member having a forward muzzle end and an opposed rearward end. The tubular member has a longitudinally extending axis, an interior region for receiving an object to be launched, an exterior wall confronting the fluid environment and an interior wall. The apparatus further includes expellable members for closing the forward muzzle end and rearward end of the tubular member, at least one flood valve member located on a corresponding expellable member for enabling fluid confronting the exterior wall to flood the interior region so as to equalize forces on the interior and exterior walls of the tubular member, and an object contact member disposed within the interior region and movable along the longitudinally extending axis. The object contact member contacts and moves the object when a propelling force is applied to the object contact member. The apparatus further includes a propellant device for producing the propelling force. The device contains a gas generator and is configured to generate gas in controlled amounts that are sufficient to propel the object contact member in the direction of the forward muzzle end. The apparatus further includes a control device that controls the flood valve member, the expellable members and the propellant device in accordance with a predetermined timed sequence wherein the control device first controls the flood valve to allow fluid to flood the interior region. Thereafter, the control device causes the expellable members to be expelled from the forward muzzle end and rearward end. Thereafter, the control device controls the propellant device to release generated gas in successive bursts so as to produce a continuous propelling force that causes the object contact member to propel the object through the tubular member, out through the forward end muzzle and into the fluid surrounding the tubular member. The successive bursts of generated gas are preferably uniform, continuous and stable thereby resulting in a fully stable ejection of the object at a relatively high exit velocity.[0009]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The features of the invention are believed to be novel and the elements characteristic of the invention are set forth with particularity in the appended claims. The figures are for illustration purposes only and are not drawn to scale. The invention itself, however, both as to organization and method of operation, may best be understood by reference to the detailed description which follows taken in conjunction with the accompanying drawings in which: [0010]
  • FIG. 1 is a combination side-elevational view, partially in cross-section, and schematic diagram of the apparatus of the present invention; [0011]
  • FIG. 2 is a combination side-elevational view, partially in cross-section, and schematic diagram of one embodiment of the apparatus of the present invention; and [0012]
  • FIG. 3 is a view taken along line [0013] 3-3 in FIG. 2.
  • DESCRIPTION OF THE PREFERRED EMBODIMENT
  • In describing the preferred embodiments of the present invention, reference will be made herein to FIGS. [0014] 1-3 of the drawings in which like numerals refer to like features of the invention.
  • Referring to FIG. 1, there is shown [0015] apparatus 10 of the present invention. Apparatus 10 generally comprises tubular member 12 which has forward muzzle end 14 and opposed rearward end 16. Tubular member 12 has longitudinally extending axis 18 and interior region 20 for receiving object 22 (e.g. vehicle, torpedo, weapon, buoy, hydroplane, etc.) that is to be launched into the fluid environment surrounding apparatus 10. Tubular member 12 can be made from any rigid material including metals, composites and plastics. As used herein, the term “fluid environment” includes oceans, rivers, lakes, or any body of fluid or liquid contained within any man-made structure or made-made earthen works. In one embodiment, tubular member 12 comprises a barrel. Such a barrel is described in U.S. Pat. No. 5,918,307. Apparatus 10 includes clamping device 23 that allows tubular member 12 to be attached to the hull of a vessel such as a ship, submarine or any other vessel or device that travels through such a fluid environment. In one embodiment, clamping device 23 is configured to allow tubular member 12 to be releasably attached to the vessel. Such a configuration enables tubular member 12 to be released from the vessel after object 22 is launched.
  • Referring to FIG. 1, [0016] tubular member 12 has interior wall 24 and exterior wall 26 confronting the fluid environment. Apparatus 10 includes a muzzle expellable member 28 and breech expellable member 30 for closing the forward muzzle end 14 and opposed rearward end 16 of tubular member 12.
  • Referring to FIG. 1, [0017] apparatus 10 further comprises flood valve members 32 for enabling fluid external to tubular member 12 to flood interior region 20 in a controlled manner so as to minimize water hammer effects, especially at relatively deep depths. One flood valve member 32 is located on expellable member 28. The other flood valve member 32 is located on expellable member 30. Although the foregoing description is in terms of two flood valves 32, it is to be understood that apparatus 10 can utilize just one flood valve 32 or more than two flood valves 32. Flood valve or valves 32 can be positioned on tubular member 12 in an alternate embodiment. In a preferred embodiment, each flood valve 32 comprises an exploding valve that is exploded upon receipt of an electrical control signal. Once flood valve 32 explodes, fluid enters interior region 20.
  • [0018] Apparatus 10 includes a plurality of exploding bolts 34 for attaching muzzle expellable member 28 to the forward muzzle end 14 and breech expellable member 30 to the opposed rearward end 16. Exploding bolts 34 are exploded upon receipt of an electrical control signal. Explosion of bolts 32 propels expellable members 28 and 30 away from tubular member 12.
  • Referring to FIG. 1, [0019] apparatus 10 further comprises object contact member 36 disposed within interior region 20 and movable along longitudinally extending axis 18. Object contact member 36 contacts at contact surface 37 and moves object 22 when a propelling force is applied to the object contact member 36. In one embodiment, object contact member 36 is generally cylindrical in shape and defines an interior space 38. In a preferred embodiment, object contact member 36 comprises a sabot.
  • In an alternate embodiment of [0020] apparatus 10, tubular member 12 includes a rail (not shown) that longitudinally extends within interior region 20. In such an embodiment, object contact member 36 is movably mounted on the rail.
  • As shown in FIG. 1, [0021] apparatus 10 further includes propellant device 40 for producing a propelling force. Propellant device 40 is disposed within interior space 38 of object contact member 36. Device 40 produces a propelling force that propels object contact member 36. In accordance with the present invention, propellant device 40 is a plurality of chemical or hybrid gas generators and is configured to release generated gas via exit or exhaust opening 41 in controlled amounts that are sufficient to propel object contact member 36. Device 40 includes an electrical interface 42 that is configured to receive an electrical control signal that effects generation of the gas. The propelling force resulting from the release of the gas propels object contact member 36 and object 22 in the direction indicated by arrow 43 and toward forward muzzle end 14. Prior to the generation of gas from device 40, object contact member 36 is positioned so that device 40 is located near opposed rearward end 16.
  • Referring to FIGS. 2 and 3, in one embodiment, [0022] gas generator device 40 comprises a plurality of chemical gas generators 44 wherein each gas generator 44 can generate a predetermined amount of gas that is emitted from exit or exhaust opening 45 of each device 44. Gas generators 44 can be chemical gas generators or hybrid gas generators incorporating a chemical gas generator with compressed gas. Compressed gas, in standard packaging, does not have sufficient energy density to effect a launch. Each generator 44 includes an electrical interface 46 for receiving an electrical control signal that effects generation of the gas in the corresponding gas generator device 44. As shown in FIG. 2, exit 45 of each device 44 faces breech expellable member 30. Referring to FIG. 3, in a preferred embodiment, the plurality of gas generators 44 are symmetrically arranged. In one embodiment, each gas generator 44 comprises a canister containing a gas generating compound or a gas generating compound and a compressed gas as is well known in the art of automobile airbag inflation devices. For the purpose of simplicity, wires 48 are not shown in FIG. 3.
  • Referring to FIG. 1, [0023] apparatus 10 further comprises control device 47. Control device 47 is preferably located on board the vessel, ship or other device to which tubular member 12 is attached. Control device 47 contains electrical circuitry and electronic components that generate electrical signals that are transferred by wires 48 to explosive bolts 34, explosive flood valves 32, and interface 42 of device 40. Control device 47 is configured so the electrical signals are generated in a predetermined order and are separated by a predetermined time duration. In such a configuration, control device 47 first produces electrical signals that cause explosive valves 32 to 1s flood interior region 20 so as to equalize the pressures on interior wall 24 and exterior wall 26 of the tubular member 12. After a predetermined amount of time has elapsed which is sufficient to allow interior region 20 to completely flood, control device 47 outputs electrical signals that cause explosion of explosive bolts 34 so as to expel expellable members 28 and 30 from forward muzzle end 14 and opposed rearward end 16, respectively. After a predetermined amount of time has elapsed which is sufficient to allow expellable members 28 and 30 to fall away from tubular member 12, control device 47 outputs electrical signals to interface 46 of device 40 to enable device 40 to generate gas in successive bursts so as to produce a continuous propelling force that is applied to object contact member 36. As a result, object contact member 36 propels object 22 through tubular member 12 and out through forward muzzle end 14. If device 40 is comprised of the plurality of gas generators 44 as shown in FIGS. 2 and 3, then wires 48 are connected to each electrical interface 46 of each gas generator 44. In such a configuration, control device 44 generates electrical signals in a predetermined timed sequence so that each gas generator 44 generates gas in accordance with the predetermined timed sequence. In one embodiment, the predetermined timed sequence effects generation of gas from each gas generator 44 in a sequential order.
  • The [0024] gas generators 44 produce sufficient thrust to create a continuous, even, and stable ejection force during the entire launch of object 22 and causes object 22 to have a relatively high exit velocity as it exits tubular member 12. Since expellable member 30 is expelled from tubular member 12 before the compressed gas is released, the full thrust produced by the released gas is utilized to accelerate object 22 during launch without any thrust being used to overcome sea pressure. Thus, the plurality of gas generators 44 located within interior space 38 of object contact member 36 in conjunction with the predetermined time sequence in which each generator 44 generates its gas results in a full-power stroke ejection of object 22.
  • If [0025] control device 47 is located on board the vessel or ship, then clamping means 23 is configured to include an electrical interface that is electrically connected to wires 48.
  • The present invention provides many other benefits and advantages. Specifically, [0026] apparatus 10 reduces the danger associated with explosive solid and liquid propellants. Furthermore, the design of apparatus 10 is relatively less complex than prior art systems and, therefore, can be implemented at relatively lower costs and with commercially available components. Additionally, apparatus 10 provides a consistent, continuous and even propelling force that is applied to the object during the entire launch process thereby resulting in a full-stroke ejection of the object. Apparatus 10 also provides for relatively high exit velocity of the object as it leaves tubular member 12. Apparatus 10 eliminates any impact related to varying sea pressures (or ship depths).
  • Although foregoing description is in terms of [0027] apparatus 10 being used in a fluid environment, it is to be understood that apparatus 10 can be used in gaseous environment wherein object 22 is launched in the gaseous environment.
  • While the present invention has been particularly described, in conjunction with a specific preferred embodiment, it is evident that many alternatives, modifications and variations will be apparent to those skilled in the art in light of the foregoing description. It is therefore contemplated that the appended claims will embrace any such alternatives, modifications and variations as falling within the true scope and spirit of the present invention. [0028]

Claims (15)

What is claimed is:
1. An apparatus for launching an object in a fluid environment, comprising:
a tubular member having a forward muzzle end and an opposed rearward end, the tubular member having a longitudinally extending axis, an exterior wall confronting the fluid environment and an interior wall defining an interior region for receiving an object to be launched;
a muzzle expellable member closing the forward muzzle end of the tubular member;
a breech expellable member closing the rearward end of the tubular member;
at least one flood valve member enabling environmental fluid to flood the interior region so as to equalize pressure between the interior and exterior walls of the tubular member;
an object contact member slidably disposed within the tubular member interior region and movable along the longitudinally extending axis, the object contact member contacting and moving the object;
a propellant device disposed in said tubular member between the breech expellable member and the object contact member, the propellant device being configured to produce gas in successive bursts that are sufficient to propel the object contact member in the direction of the forward muzzle end; and
a control device joined to the flood valve member, the expellable members and the propellant device.
2. The apparatus according to claim 1 wherein:
the control device first causes the flood valve member to allow fluid to flood the tubular member interior region, the control device next causing the muzzle expellable member and breech expellable member to be expelled from the tubular member, and the control device causing the propellant device to produce the gas in a preprogrammed manner; and
the propellant device is configured to produce the gas in accordance with the preprogrammed manner.
3. The apparatus according to claim 1 wherein the propellant device comprises a plurality of gas generators, each gas generator producing a predetermined amount of gas.
4. The apparatus according to claim 3 wherein the plurality of gas generators are symmetrically arranged.
5. The apparatus according to claim 3 wherein each gas generator comprises a selected one of a chemical generating a gas and a combination of a chemical generating a gas with a compressed gas.
6. The apparatus according to claim 2 wherein:
the propellant device comprises a plurality of gas generators, each gas generator producing a predetermined amount of gas; and
the control device is configured to control the plurality of gas generators in a manner such that each gas generator produces gas therein in accordance with the preprogrammed manner.
7. The apparatus according to claim 6 wherein the predetermined timed sequence effects production of the gas of each gas generator in a sequential manner.
8. The apparatus according to claim 1 wherein the object contact member is generally cylindrical in shape and defines an interior space.
9. The apparatus according to claim 8 wherein the propellant device is disposed within the interior space of the object contact member.
10. The apparatus according claim 1 wherein the object contact member slides out of the tubular member after the object is launched.
11. The apparatus according to claim 1 wherein the muzzle expellable member is attached to the forward muzzle end and the breech expellable member is attached to the rearward end, the apparatus further comprising a plurality of exploding bolts for attaching the muzzle expellable member to the forward muzzle end and the breech expellable member to the rearward end.
12. The apparatus according to claim 1 wherein the at least one valve member comprises a pair of valve members, one valve member being located on the muzzle expellable member, the other valve member being located on the breech expellable member.
13. The apparatus according to claim 1 wherein the at least one valve member comprises an exploding valve.
14. The apparatus according to claim 1 further comprising means for attaching the tubular member to a vessel.
15. The apparatus according to claim 14 wherein the attaching means comprises means for releasing the tubular member from the vessel.
US10/224,229 2002-08-19 2002-08-19 Apparatus for launching an object in a fluid environment Expired - Fee Related US6701819B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US10/224,229 US6701819B1 (en) 2002-08-19 2002-08-19 Apparatus for launching an object in a fluid environment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/224,229 US6701819B1 (en) 2002-08-19 2002-08-19 Apparatus for launching an object in a fluid environment

Publications (2)

Publication Number Publication Date
US20040031381A1 true US20040031381A1 (en) 2004-02-19
US6701819B1 US6701819B1 (en) 2004-03-09

Family

ID=31715226

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/224,229 Expired - Fee Related US6701819B1 (en) 2002-08-19 2002-08-19 Apparatus for launching an object in a fluid environment

Country Status (1)

Country Link
US (1) US6701819B1 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7237353B1 (en) * 2004-07-30 2007-07-03 The United States Of America Represented By The Secretary Of The Navy Muzzle break with gas relief membrane for an underwater gun
EP2107331A1 (en) * 2008-04-03 2009-10-07 Whitehead Alenia Sistemi Subacquei S.p.A. Torpedo lauch device
US20150008280A1 (en) * 2013-06-03 2015-01-08 Lockheed Martin Corporation Launched air vehicle system
EP1950521B1 (en) 2007-01-27 2015-10-21 ThyssenKrupp Marine Systems GmbH Method for storing and deploying submersibles in a submarine
US10502515B2 (en) * 2017-01-17 2019-12-10 Raytheon Company Launch piston brake
CN113834381A (en) * 2021-06-16 2021-12-24 北京机械设备研究所 Underwater balance launching device and launching method thereof

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6871610B1 (en) * 2003-06-06 2005-03-29 The United States Of America As Represented By The Secretary Of The Navy Assembly for launching bodies from an underwater platform
US7032530B1 (en) * 2003-09-29 2006-04-25 The United States Of America As Represented By The Secretary Of The Navy Submarine air bag launch assembly
US7159501B1 (en) * 2004-11-08 2007-01-09 The United States Of America As Represented By The Secretary Of The Navy Stackable in-line surface missile launch system for a modular payload bay
US7232353B1 (en) * 2005-04-18 2007-06-19 The United States Of America As Represented By The Secretary Of The Navy Retrievable pneumatic buoy system for submarine use
US8166904B2 (en) * 2007-12-12 2012-05-01 Irobot Corporation Delivery systems for pressure protecting and delivering a submerged payload and methods for using the same
US7942107B2 (en) 2007-12-12 2011-05-17 Irobot Corporation Delivery systems for pressure protecting and delivering a submerged payload and methods for using the same
US7681352B2 (en) * 2008-06-30 2010-03-23 Lockheed Martin Corporation Underwater gun comprising a valve-type barrel-seal
US7874091B2 (en) * 2008-06-30 2011-01-25 Lockheed Martin Corporation Underwater gun comprising a plate-type barrel seal
US8042295B2 (en) * 2008-06-30 2011-10-25 Lockheed Martin Corporation Underwater gun comprising a barrel adapter including a barrel seal
US8046947B2 (en) * 2008-06-30 2011-11-01 Lockheed Martin Corporation Underwater gun comprising a passive fluidic barrel seal
US7832134B2 (en) * 2008-06-30 2010-11-16 Lockheed Martin Corporation Underwater gun comprising a turbine-based barrel seal
US8161899B1 (en) * 2008-09-11 2012-04-24 The United States Of America As Represented By The Secretary Of The Navy Multiple torpedo mine
US7730838B1 (en) * 2009-01-30 2010-06-08 Raytheon Company Buoyancy dissipater and method to deter an errant vessel
US8371204B2 (en) 2010-04-30 2013-02-12 Raytheon Company Bubble weapon system and methods for inhibiting movement and disrupting operations of vessels
US8402895B2 (en) 2010-04-30 2013-03-26 Raytheon Company Vortice amplified diffuser for buoyancy dissipater and method for selectable diffusion
US9453705B2 (en) * 2014-02-21 2016-09-27 Lockheed Martin Corporation Payload launcher and autonomous underwater vehicle
US10112686B2 (en) * 2015-01-30 2018-10-30 Woods Hole Oceanographic Institution System for the deployment of marine payloads
US10464693B2 (en) 2015-09-04 2019-11-05 Lockheed Martin Corporation Launch canister with air bag ram
US11072406B2 (en) * 2016-01-29 2021-07-27 Woods Hole Oceanographic Institution System for the deployment of marine payloads
KR101793541B1 (en) 2017-05-30 2017-11-06 국방과학연구소 Detachable cover device
KR101877186B1 (en) * 2017-12-07 2018-07-10 국방과학연구소 Sliding cover device

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1526256A (en) * 1924-04-05 1925-02-10 Fried Krupp Germaniawerft Ag Underwater-torpedo tube
US3279319A (en) * 1964-06-19 1966-10-18 Joseph W Semonian Floatable rocket launcher
CH503967A (en) * 1969-02-20 1971-02-28 Oerlikon Buehrle Ag bullet
DE3333614A1 (en) * 1983-09-17 1985-04-18 Gemmecke, Kurt, Ing.(grad.), 2400 Lübeck Hydraulically operated underwater ejector device
DE3711059C1 (en) * 1987-04-02 1988-10-13 Krupp Mak Maschb Gmbh Training of drainpipes, discharge pipes or containers in submarines
DE3737090A1 (en) * 1987-11-02 1989-05-11 Krupp Atlas Elektronik Gmbh Torpedo tube for firing torpedoes underwater
DE3940583A1 (en) * 1989-12-08 1991-06-13 Tech Mathematische Studiengese Tube for underwater launching of missile - is initially filled with gas at pressure corresponding to depth of water
US5495819A (en) * 1994-03-09 1996-03-05 Marion; Frank A. Endothermic gas generator for use in a device propulsion

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7237353B1 (en) * 2004-07-30 2007-07-03 The United States Of America Represented By The Secretary Of The Navy Muzzle break with gas relief membrane for an underwater gun
EP1950521B1 (en) 2007-01-27 2015-10-21 ThyssenKrupp Marine Systems GmbH Method for storing and deploying submersibles in a submarine
EP2107331A1 (en) * 2008-04-03 2009-10-07 Whitehead Alenia Sistemi Subacquei S.p.A. Torpedo lauch device
US20150008280A1 (en) * 2013-06-03 2015-01-08 Lockheed Martin Corporation Launched air vehicle system
US9938021B2 (en) * 2013-06-03 2018-04-10 Lockheed Martin Corporation Launched air vehicle system
US10421558B2 (en) 2013-06-03 2019-09-24 Lockheed Martin Corporation Launched air vehicle system
US10502515B2 (en) * 2017-01-17 2019-12-10 Raytheon Company Launch piston brake
CN113834381A (en) * 2021-06-16 2021-12-24 北京机械设备研究所 Underwater balance launching device and launching method thereof

Also Published As

Publication number Publication date
US6701819B1 (en) 2004-03-09

Similar Documents

Publication Publication Date Title
US6701819B1 (en) Apparatus for launching an object in a fluid environment
US6164179A (en) Submarine deployable vertical launch spar buoy
US5341718A (en) Launched torpedo decoy
US4455917A (en) Shock wave end cap removal device
US8161899B1 (en) Multiple torpedo mine
US6502528B1 (en) Pressure-balanced gas turbine underwater launcher
JPS61205800A (en) Antisubmarine weapon
US6427574B1 (en) Submarine horizontal launch tactom capsule
US6376762B1 (en) Small vehicle launch platform
KR20150052714A (en) Weapon firing apparatus using compressed air of high-pressure
US5117731A (en) Tactical acoustic decoy
US5495819A (en) Endothermic gas generator for use in a device propulsion
US6672239B1 (en) Elastomeric launch assembly and method of launch
EP1902938A2 (en) Float for a device air-launched into the sea, in particular for a countermeasure
CN115289919B (en) Target damage warhead in water based on high-pressure and normal-pressure bubble combined pulsation principle
Williams PATENT COUNSEL NAVAL UNDERSEA WARFARE CENTER 1176 HOWELL ST. CODE OOOC, BLDG. 112T NEWPORT, RI 02841
US5895882A (en) Air-delivered remotely-activated infrared anti-ship missile decoy and deployment method
US3084627A (en) Underwater launched surface mine
JP6086831B2 (en) Underwater projectile launcher
AU737923B2 (en) A pyroacoustic generator for protecting submarines and surface vessels
US3506086A (en) Submarine target simulator
US3465639A (en) Hypervelocity jet and projectile velocity augmenter
US3083667A (en) Variable buoyancy underwater missile
US3120709A (en) Surface launch test vehicle
US3468217A (en) Hypervelocity jet system

Legal Events

Date Code Title Description
AS Assignment

Owner name: THE UNITED STATES OF AMERICA, RHODE ISLAND

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:WILLIAMS, MICHAEL W.;MOODY, PAUL E.;REEL/FRAME:013455/0621

Effective date: 20020808

REMI Maintenance fee reminder mailed
LAPS Lapse for failure to pay maintenance fees
STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362

FP Lapsed due to failure to pay maintenance fee

Effective date: 20080309