US2010178A - Flash eliminator for guns - Google Patents
Flash eliminator for guns Download PDFInfo
- Publication number
- US2010178A US2010178A US637267A US63726732A US2010178A US 2010178 A US2010178 A US 2010178A US 637267 A US637267 A US 637267A US 63726732 A US63726732 A US 63726732A US 2010178 A US2010178 A US 2010178A
- Authority
- US
- United States
- Prior art keywords
- gun
- gases
- liquid
- air
- muzzle
- 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
- 239000007789 gas Substances 0.000 description 26
- 239000007788 liquid Substances 0.000 description 20
- 239000003721 gunpowder Substances 0.000 description 14
- 238000002156 mixing Methods 0.000 description 9
- 239000000203 mixture Substances 0.000 description 6
- 239000007921 spray Substances 0.000 description 5
- 238000005507 spraying Methods 0.000 description 5
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000009740 moulding (composite fabrication) Methods 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- NIOPZPCMRQGZCE-WEVVVXLNSA-N 2,4-dinitro-6-(octan-2-yl)phenyl (E)-but-2-enoate Chemical compound CCCCCCC(C)C1=CC([N+]([O-])=O)=CC([N+]([O-])=O)=C1OC(=O)\C=C\C NIOPZPCMRQGZCE-WEVVVXLNSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 150000001768 cations Chemical class 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000000839 emulsion Substances 0.000 description 1
- 238000005187 foaming Methods 0.000 description 1
- 150000002484 inorganic compounds Chemical class 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- SYXUBXTYGFJFEH-UHFFFAOYSA-N oat triterpenoid saponin Chemical compound CNC1=CC=CC=C1C(=O)OC1C(C=O)(C)CC2C3(C(O3)CC3C4(CCC5C(C)(CO)C(OC6C(C(O)C(OC7C(C(O)C(O)C(CO)O7)O)CO6)OC6C(C(O)C(O)C(CO)O6)O)CCC53C)C)C4(C)CC(O)C2(C)C1 SYXUBXTYGFJFEH-UHFFFAOYSA-N 0.000 description 1
- 150000002894 organic compounds Chemical class 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000000344 soap Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/32—Muzzle attachments or glands
- F41A21/34—Flash dampers
Definitions
- a layer of liquid is created between the outflowing hot gases and the surrounding atmosphere.
- This layer prevents for a short time the gases from mixing with the air and accelerates the cooling down of the gases. Due to the strong expansion and subsequently to the mixing of the gases with the liquid, they are brought in such a condition that the gas mixture resulting from mixing with the air does no longer take fire.
- solutions of inorganic or organic compounds, organic liquids, emulsions or suspensions, etc. decreasing the inflammability of gas mixtures may be used, as
- a spraying device is mounted around or to the muzzle or further backwards on the stationary or recoiling parts of the gun, which device, according to the invention, is so constructed that just before discharging the gun it forms one or more somewhat diverging liquid layers in front of the muzzle, which temporarily envelop the outflowing gunpowder gases and. separate them from the surrounding air.
- the liquid layer need not necessarily be uninterrupted.
- a spray with closely spaced apertures or an atomizing spray instead of a slit also has a good effect.
- the latter is ejected with force, so that over some distance the spray remains almost parallel to its original direction, while thereafter the liquid atomizes more and more. It is also desirable to make the diameter of the spray circle larger than that of the barrel of the gun. The space between the sprayer and the barrel may generally remain open without any objection.
- Figure 1 is a side elevation view of a gun muzzle with one form of invention applied thereto.
- Figure 2 is an end View of the gun muzzle shown in Figure 1.
- the gun muzzle H has secured to it in a suitable manner as by brackets l2, 2.
- liquid conduit It which terminates in a ring l6 surrounding the gun bore at the muzzle and held in place by a suitable means such as bracket H3.
- the ring it has projecting from it in direction of the projectile travel a series of nozzles or orifices 2B.
- the nozzles or orifices are preferably divergent to compensate in a degree for the expansion of the gases issuing from the gun.
- valve means of any suitable construction For the sake of illustration I have shown conventionally a valve V.
- the spraying device may be mounted independently of the gun and if desired may operate for.
- Sprayers may be mounted for each gun, connected to a pipe through which the liquid is supplied under pressure.
- mobile mountings it is desirable to make use of the 'recoilin'g of the,
- a regulating mechanism connected with the discharging device, may be used.
- the invention is applicable to all kinds of firearms.
- Apparatus for eliminating flashes from heavy or light ordnance comprising means for forming freely in air at the muzzle of a gun a liquid envelope for the outflowing gunpowder I gases by the projection of liquid in the direction of a projectiletraveLand means to cause the formation of said envelope just prior to the gun discharge, whereby the hot gases are permitted to expand and cool within said envelope while being kept from freely mixing with the air.
- Apparatus for eliminating flashes from heavy or light ordnance comprising spraying means positioned near the muzzle of the gun for creating freely in air an envelope for the outflowing gunpowder gases, and means to eject liquid from said spraying means in the direction of projectile travel just prior to the gun discharge, whereby the hot gases are permittedto expand and cool within said envelope while being kept from freely mixing with the air.
- Apparatus for eliminating flashes from heavy or light ordnance comprising a spraying device positioned at the muzzle of a gun for form ing freely in air at least one diverging liquid envelope enclosing the gunpowder gases, and supply means for'delivering liquid under pressure to said device just prior to the gun discharge, whereby .the hot gases arepermitted to expand and cool within said envelope while being'kept from freely mixing withthev air.
- heavy or light ordnance comprising projecting liquid freely in air at the muzzle of the gun in the direction of projectile traveljust prior to gun discharge to form an envelope enclosing the gunpowder gases at the moment of discharge, where'- by the hot gases are permitted to expand and; being keptfrom' cool within said envelope while freely mixing with air.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Nozzles (AREA)
Description
1935- G. DE BRUIN I 2,010,178
FLASH ELIMINATOR FOR GUNS Filed Oct. 11, 1932 INVENTOR GERRIT DE BRUIN BY l-us ATTORNEYS Patented Aug. 6, 1935 half to Naamlooze Venno'otschap Nederlandsche Springstofienfabrieken, Amsterdam, Netherlands Ap l cation October 11,
1932, Serial No. 637,267
In the Netherlands October 13, 1931 5 Claims.
Accordingto current theories the muzzle flash of firearms is caused by a secondary combustion process. When burning gunpowder in a firearm a quantity of inflammable gases is formed,
for the greater part carbon monoxide (CO) and hydrogen (H2). During the combustion in the barrel the carbon and hydrogen contained in the gunpowder cannot fully burn down to CO2 and 1-120, asthe quantity of oxygen present in the gunpowder is not suflicient thereto. When these gases leave the muzzle and mix with the oxygen of the air themixture will take fire, if a suitable proportion of mixture is attained and if the temperature of the gas mixture is still above the ignition temperature.
This flash is a highly undesirable phenomenon,
as it discloses the position of the gun or the place oi" the gunner and blinds the gun-detachment.
Much trouble has been taken to overcome this disadvantage, but always the solution of this problem has been sought in the manufacture of a gunpowder showing but little or no flash, a so called flashless gunpowder. This solution, however, has the disadvantage that the flashlessness of gunpowder can only be obtained by sacrificing part of the ballistic property; e. g. with flashless gunpowder and under equal circumstances one must always be content with a smaller initial velocity of the projectile than would be attainable if the requirement of flashlessness was not to be answered. The same disadvantage is experienced if the flashlessness is obtained by adding foreign substances to the charge or by trying to cool the gases in the barrel behind the projectile by injecting a liquid in the barrel.
' 'This invention seeks the solution of the problem in another direction and starts from the principle, that, using any kind of flash giving gunpowder, the powder is allowed to have its full effect on the projectile in the barrel, measures only being taken at the moment that the gases together with the projectile leave the muzzle of the firearm.
In order to prevent the gases from igniting at the said moment on account of their mixing with the oxygen of this air, according to the invention a layer of liquid is created between the outflowing hot gases and the surrounding atmosphere. This layer (or layers) prevents for a short time the gases from mixing with the air and accelerates the cooling down of the gases. Due to the strong expansion and subsequently to the mixing of the gases with the liquid, they are brought in such a condition that the gas mixture resulting from mixing with the air does no longer take fire.
In general a mere cooling action will suffice and the layer of liquid will then be water; however, in
cases in which the desired effect can but difiicultly be attained with water only, solutions of inorganic or organic compounds, organic liquids, emulsions or suspensions, etc. decreasing the inflammability of gas mixtures, may be used, as
well as solutions of soap, saponine or other foaming means, which guarantee a better coating for the gas mass and consequently thus accelerate the cooling of the gases by expansion, before the mixture with air takes place. 7
In order toapply the'liquid layer or layersin the right place a spraying device is mounted around or to the muzzle or further backwards on the stationary or recoiling parts of the gun, which device, according to the invention, is so constructed that just before discharging the gun it forms one or more somewhat diverging liquid layers in front of the muzzle, which temporarily envelop the outflowing gunpowder gases and. separate them from the surrounding air. The liquid layer need not necessarily be uninterrupted. A spray with closely spaced apertures or an atomizing spray instead of a slit also has a good effect. In order to prevent the velocity of the projectile from being influenced by colliding of the projectile with the liquid, it is desirable that the latter is ejected with force, so that over some distance the spray remains almost parallel to its original direction, while thereafter the liquid atomizes more and more. It is also desirable to make the diameter of the spray circle larger than that of the barrel of the gun. The space between the sprayer and the barrel may generally remain open without any objection.
Referring to the drawing;-- 1
Figure 1 is a side elevation view of a gun muzzle with one form of invention applied thereto.
Figure 2 is an end View of the gun muzzle shown in Figure 1.
In the drawing the gun muzzle H] has secured to it in a suitable manner as by brackets l2, 2. liquid conduit It which terminates in a ring l6 surrounding the gun bore at the muzzle and held in place by a suitable means such as bracket H3. The ring it has projecting from it in direction of the projectile travel a series of nozzles or orifices 2B. The nozzles or orifices are preferably divergent to compensate in a degree for the expansion of the gases issuing from the gun.
For controlling the flow of liquid, there may be inserted in the conduit [4 between the spray nozzles 2B and a reservoir 22, valve means of any suitable construction. For the sake of illustration I have shown conventionally a valve V.
In stationary mountings (ships, fortresses, etc.)
the spraying device may be mounted independently of the gun and if desired may operate for.
several guns simultaneously, in which case one or more Sprayers may be mounted for each gun, connected to a pipe through which the liquid is supplied under pressure. With mobile mountings it is desirable to make use of the 'recoilin'g of the,
fire-arm for bringing theliquid under pressure.
For the synchronization a regulating mechanism, connected with the discharging device, may be used.
The invention is applicable to all kinds of firearms.
I claim:
1. Apparatus for eliminating flashes from heavy or light ordnance, comprising means for forming freely in air at the muzzle of a gun a liquid envelope for the outflowing gunpowder I gases by the projection of liquid in the direction of a projectiletraveLand means to cause the formation of said envelope just prior to the gun discharge, whereby the hot gases are permitted to expand and cool within said envelope while being kept from freely mixing with the air. 2. Apparatus for eliminating flashes from heavy or light ordnance, comprising spraying means positioned near the muzzle of the gun for creating freely in air an envelope for the outflowing gunpowder gases, and means to eject liquid from said spraying means in the direction of projectile travel just prior to the gun discharge, whereby the hot gases are permittedto expand and cool within said envelope while being kept from freely mixing with the air.
,3. Apparatus for eliminating flashes from heavy or light ordnance, comprising a spraying device positioned at the muzzle of a gun for form ing freely in air at least one diverging liquid envelope enclosing the gunpowder gases, and supply means for'delivering liquid under pressure to said device just prior to the gun discharge, whereby .the hot gases arepermitted to expand and cool within said envelope while being'kept from freely mixing withthev air.
4. The method of eliminating flashes from heavy or light ordnance; comprising forming freely in air a liquid envelope at the muzzle of the gun, to enclose the gunpowder gases at the momentof gun discharge, whereby the hot gases are permitted to expand and cool within said'en velope while being kept from freely mixing with the air.
heavy or light ordnance, comprising projecting liquid freely in air at the muzzle of the gun in the direction of projectile traveljust prior to gun discharge to form an envelope enclosing the gunpowder gases at the moment of discharge, where'- by the hot gases are permitted to expand and; being keptfrom' cool within said envelope while freely mixing with air. 7 I
- Y GERRIT DE:BRUIN.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NL164237X | 1931-10-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2010178A true US2010178A (en) | 1935-08-06 |
Family
ID=19776625
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US637267A Expired - Lifetime US2010178A (en) | 1931-10-13 | 1932-10-11 | Flash eliminator for guns |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US2010178A (en) |
| BE (1) | BE391291A (en) |
| CH (1) | CH164237A (en) |
| DE (1) | DE611432C (en) |
| FR (1) | FR743542A (en) |
| GB (1) | GB390425A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2514883A1 (en) * | 1981-10-21 | 1983-04-22 | Foerenade Fabriksverken | PRESSURE DAMPER FOR ARMS WITHOUT BACK |
| FR2721100A1 (en) * | 1994-06-14 | 1995-12-15 | Lacroix E Tous Artifices | Gun barrel muzzle mask |
| WO2004076956A1 (en) * | 2003-02-28 | 2004-09-10 | Opus Akustik Ab | A method and a device for noise reduction |
| US10145636B2 (en) * | 2017-01-16 | 2018-12-04 | David B. Stark | Reduction of first shot noise in firearm sound suppressors |
| US10337819B1 (en) * | 2017-01-16 | 2019-07-02 | David B. Stark | Reduction of first shot noise in firearm sound suppressors |
-
0
- BE BE391291D patent/BE391291A/xx unknown
- FR FR743542D patent/FR743542A/fr not_active Expired
-
1932
- 1932-09-27 GB GB26857/32A patent/GB390425A/en not_active Expired
- 1932-09-27 CH CH164237D patent/CH164237A/en unknown
- 1932-10-09 DE DEN34271D patent/DE611432C/en not_active Expired
- 1932-10-11 US US637267A patent/US2010178A/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2514883A1 (en) * | 1981-10-21 | 1983-04-22 | Foerenade Fabriksverken | PRESSURE DAMPER FOR ARMS WITHOUT BACK |
| US4554860A (en) * | 1981-10-21 | 1985-11-26 | Forenade Fabriksverken | Pressure damper for recoilless weapons |
| FR2721100A1 (en) * | 1994-06-14 | 1995-12-15 | Lacroix E Tous Artifices | Gun barrel muzzle mask |
| WO2004076956A1 (en) * | 2003-02-28 | 2004-09-10 | Opus Akustik Ab | A method and a device for noise reduction |
| US10145636B2 (en) * | 2017-01-16 | 2018-12-04 | David B. Stark | Reduction of first shot noise in firearm sound suppressors |
| US10337819B1 (en) * | 2017-01-16 | 2019-07-02 | David B. Stark | Reduction of first shot noise in firearm sound suppressors |
Also Published As
| Publication number | Publication date |
|---|---|
| GB390425A (en) | 1933-04-06 |
| DE611432C (en) | 1935-04-24 |
| CH164237A (en) | 1933-09-30 |
| BE391291A (en) | |
| FR743542A (en) | 1933-04-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2679137A (en) | Apparatus for burning fuel in a fast moving gas stream | |
| US1860276A (en) | Firearm | |
| US2419866A (en) | Aerial torpedo | |
| US1375601A (en) | Propelling device for use on vehicles, marine vessels, or aircraft | |
| US1376316A (en) | Projectile | |
| US4607849A (en) | Jet exhaust simulator | |
| CN113983458A (en) | An air/alcohol torch igniter based on a bubble atomizing nozzle | |
| US1897092A (en) | Aircraft with rotative wings | |
| US20100314139A1 (en) | Target-Specific Fire Fighting Device For Launching A Liquid Charge At A Fire | |
| US2648196A (en) | Ram jet burner with aqueous injection to promote smooth burning | |
| US2094854A (en) | Gun | |
| US2010178A (en) | Flash eliminator for guns | |
| US2476171A (en) | Smoke screen generator | |
| US1817470A (en) | Fuel burning apparatus and method | |
| FI57922C (en) | FOERFARANDE OCH ANORDNING FOER FRAMSTAELLNING AV SVAVELDIOXID | |
| US2701444A (en) | Burner for jet engines | |
| US2480147A (en) | Firing device for combustion apparatus | |
| US1267760A (en) | Liquid-fuel combustion. | |
| US2981059A (en) | Dual thrust chamber rocket | |
| US1342901A (en) | Confined-combustion method | |
| US3017367A (en) | Valveless pulsejet smoke generator | |
| US2659199A (en) | Apparatus for avoiding hot starts in turbojet engine operation and for igniting fuel in the afterburner | |
| CN107653429B (en) | Accumulative pressure high frequency detonation-gun | |
| US2658340A (en) | Apparatus for igniting fuel in fast-moving hot gas streams | |
| US3016086A (en) | Recoilless flamethrower |