Air cannon and associated launch canister for a line-fouling system
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F41H-013/00
A63B-069/20
A63B-071/00
F41H-011/05
F41F-001/08
F41B-011/62
A61K-038/16
B63C-009/26
G06F-011/34
B63B-021/22
B63B-021/48
A63B-071/02
출원번호
US-0906128
(2014-06-04)
등록번호
US-10030943
(2018-07-24)
우선권정보
GB-1313226.1 (2013-07-24)
국제출원번호
PCT/GB2014/051729
(2014-06-04)
국제공개번호
WO2015/011437
(2015-01-29)
발명자
/ 주소
Searle, Matthew
Hocking, William Mark
Howell, Andrew Rhys
Taylor, Derek William
출원인 / 주소
BCB INTERNATIONAL LIMITED
대리인 / 주소
Maschoff Brennan
인용정보
피인용 횟수 :
0인용 특허 :
11
초록▼
FIG. 7 shows an air cannon system loaded with a launch canister containing a prop-fouler. A pressure vessel (28) contains an inlet including a poppet valve (100) that, upon command, can be selectively placed in either a one-way flow position to permit charging of the pressure vessel or otherwise ope
FIG. 7 shows an air cannon system loaded with a launch canister containing a prop-fouler. A pressure vessel (28) contains an inlet including a poppet valve (100) that, upon command, can be selectively placed in either a one-way flow position to permit charging of the pressure vessel or otherwise opened to trigger rapid discharge through pressure equalization with the ambient environment. The air cannon may include multiple splayed barrels or a single barrel (158). A launch canister (202), realized in the form of a tube, has a driving plate (350) that closes an end of the launch tube. The driving plate is the first point loaded into the barrel. Within the launch canister (202) a first portion of a floating prop-fouling line is stored. The prop-fouling line, such as made from Dyneema®, has at its ends two drogues that, upon entry into the water, fill with water to produce drag resistance to movement of the prop-fouling line. To avoid undue stress on canopy panels of each drogue and to avoid twisting of shroud lines (312) to the canopy, a rotating shackle (310a, 310b) acts as a coupling point between the shroud lines (312) and the prop-fouling line. Only one drogue (306), its associated coupling and a selected length prop-fouling line are loaded into the launch canister, with the other drogue and its rotating shackle (310b) loaded into a cradle (166). Upon firing, gas expansion causes the rapid acceleration and ejection of the launch tube (202) and generally straight line deployment of the prop-fouling line (302).
대표청구항▼
1. An air cannon system comprising: A) an air cannon comprising (i) a barrel with a muzzle end and a manifold end, (ii) a pressure vessel, (iii) a manifold coupled, via a valve, between the pressure vessel and the manifold end of the barrel such that the pressure vessel is selectively in fluid commu
1. An air cannon system comprising: A) an air cannon comprising (i) a barrel with a muzzle end and a manifold end, (ii) a pressure vessel, (iii) a manifold coupled, via a valve, between the pressure vessel and the manifold end of the barrel such that the pressure vessel is selectively in fluid communication with the barrel through controlled operation of the valve, and (iv) a firing mechanism;B) a launch canister delivery system having a sleeve configured to be slideably loadable within the barrel of the air cannon, the sleeve having a closed end and an open end, the closed end including a driving disk having an external rear surface; andC) a floating boat fouling line comprising a major part and a minor part, wherein the major part is packed within the sleeve of the launch canister delivery system and the minor part is kept external to the sleeve, the floating boat fouling line including: i) high-strength lightweight cord having first and second ends and a central section therebetween, the central section comprising a first length of the cord and a second length of the cord that end-to-end make up the cord between the first and second ends and where the first length of the cord is more than half of the central section and the second length of the cord is less than half of the central section;ii) a first rotating shackle and a second rotating shackle, the first rotating shackle coupled to the first end of said cord and the second rotating shackle coupled to the second end of said cord; andiii) a front drogue and a tail drogue, each of said front drogue and said tail drogue including a canopy and each of said front drogue and said tail drogue having multiple shroud lines extending from the canopy thereof; wherein the shroud lines from the front drogue are attached to the first rotating shackle and the shroud lines from the tail drogue are attached to the second rotating shackle, the rotating shackles arranged both (a) to act as a sink weight to cause, when deployed in water, submersion of each respective canopy, and (b) to isolate twisting of said central section of said cord from twisting of said shroud lines;wherein the major part of the floating boat fouling line that is packed within the sleeve includes the front drogue, the first rotating shackle and the first length of the central section of the cord, whereas the minor part of the floating boat fouling line outside of the sleeve includes the tail drogue, the second rotating shackle and the second length of the central section of the cord, and wherein the closed end of the sleeve is loaded into the barrel so that the driving disk is seated adjacent to the manifold end;whereinthe pressure vessel of the air cannon is arranged to store, when the air cannon is primed, at least one charge of pressurized gas to permit firing of the air cannon; andthe firing mechanism includes a trigger and the valve, the valve arranged to be controllably opened, in response to actuation of the trigger, to cause, after both charging of the pressure vessel with said at least one charge of pressurized gas and actuation of the trigger to fire the air cannon, rapid expansion of pressurized gas from the pressure vessel into the manifold, thereby to cause, in use, high-velocity gas forcibly to act on the external rear surface of the driving disk of the sleeve to accelerate the launch canister delivery system out of the barrel through the muzzle end. 2. The air cannon system of claim 1, further comprising a cradle coupled to the barrel, wherein the minor part of the floating boat fouling line is loaded into the cradle. 3. The air cannon system of claim 2, wherein the cradle is a secondary barrel located beneath the barrel, the secondary barrel having an open end and a closed end and wherein the secondary barrel is packed with the minor part of the floating boat fouling line such that the tail drogue is loaded closest to the closed end of the secondary barrel. 4. The air cannon system of claim 3, wherein the floating boat fouling line further includes a rear float and wherein the secondary barrel is packed with the rear float, wherein the rear float is coupled to said cord, the rear float positioned adjacent to the second rotating shackle and wherein the rear float is inboard of the second rotating shackle relative to the tail drogue. 5. The air cannon system of claim 1, wherein the floating boat fouling line further includes a front float and wherein the sleeve of the launch canister delivery system is packed with the front float, and wherein the front float is coupled to said cord and positioned adjacent to the first rotating shackle and inboard of the first rotating shackle relative to the front drogue. 6. The air cannon system of claim 1, wherein the canopies of the front drogue and the tail drogue each have a volume between about 5000 cm3 and about 20000 cm3. 7. The air cannon system of claim 1, wherein the high-strength lightweight cord is made from one of: a UHMWPE material; anda natural fiber. 8. The air cannon system of claim 1, wherein the sleeve includes at least one ventilation hole juxtaposed with the driving disk. 9. The air cannon system of claim 1, wherein the front drogue is loaded closest to the driving disk and the first length of the central section of the cord is loaded between the first rotating shackle and the open end of the sleeve. 10. The air cannon system of claim 1, wherein the sleeve includes a plurality of ventilation holes juxtaposed with the driving disk. 11. The air cannon system of claim 10, wherein the plurality of ventilation holes are circumferentially-spaced. 12. The air cannon system of claim 10, wherein the cord has a run-out length of the cord from the sleeve, and wherein the run-out length is between about fifty meters and about three hundred meters. 13. The air cannon system of claim 1, wherein the cord has a length and the length is between about twenty meters and about three hundred meters. 14. The air cannon system of claim 1, wherein the valve in the firing mechanism is a poppet valve.
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이 특허에 인용된 특허 (11)
Metherell, Mark B.; Metherell, Alexander F., Apparatus and method for protecting ships and harbors from attack by vessels.
Nicolaevich Isakov S. (Severny pr. ; d.83 ; kv. 154 St. Petersburg SUX 195249) Nicolaevich Isakov I. (pos. Levasheva ; d.35 St. Petersburg SUX 194901) Vasilievich Yurkin S. (Prosveshenia pr. ; d. 35 , Pneumatic launcher.
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