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WO2008014984A1 - Arrangement de réduction des gaz et canon ou arme équipé d'un Arrangement de réduction des gaz - Google Patents

Arrangement de réduction des gaz et canon ou arme équipé d'un Arrangement de réduction des gaz Download PDF

Info

Publication number
WO2008014984A1
WO2008014984A1 PCT/EP2007/006780 EP2007006780W WO2008014984A1 WO 2008014984 A1 WO2008014984 A1 WO 2008014984A1 EP 2007006780 W EP2007006780 W EP 2007006780W WO 2008014984 A1 WO2008014984 A1 WO 2008014984A1
Authority
WO
WIPO (PCT)
Prior art keywords
gas
insert
barrel
weapon
gas removal
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.)
Ceased
Application number
PCT/EP2007/006780
Other languages
German (de)
English (en)
Inventor
Norbert Fluhr
Wolfgang Bantle
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.)
Heckler und Koch GmbH
Original Assignee
Heckler und Koch GmbH
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 Heckler und Koch GmbH filed Critical Heckler und Koch GmbH
Priority to CA002659573A priority Critical patent/CA2659573A1/fr
Priority to EP07786474A priority patent/EP2047204A1/fr
Publication of WO2008014984A1 publication Critical patent/WO2008014984A1/fr
Priority to US12/364,320 priority patent/US20090229454A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A5/00Mechanisms or systems operated by propellant charge energy for automatically opening the lock
    • F41A5/18Mechanisms or systems operated by propellant charge energy for automatically opening the lock gas-operated
    • F41A5/26Arrangements or systems for bleeding the gas from the barrel
    • F41A5/28Adjustable systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A5/00Mechanisms or systems operated by propellant charge energy for automatically opening the lock
    • F41A5/18Mechanisms or systems operated by propellant charge energy for automatically opening the lock gas-operated
    • F41A5/26Arrangements or systems for bleeding the gas from the barrel

Definitions

  • the invention relates to a gas take-off assembly for a barrel of a gas-pressure self-loading weapon (e.g., a machine gun) having a gas cylinder in communication with the barrel bore.
  • a gas take-off device is known for example from DE 196 15 181.
  • barrel denotes both a gun barrel with moves and fields as well as a smooth gun barrel.
  • Directional indications such as top, bottom, front, back, right and left are given for an attacking weapon from the point of view of the shooter.
  • a gas piston is arranged in a gas cylinder.
  • the gas cylinder is largely closed at one end, so that between the gas piston end face and the end wall of the gas cylinder, a pressure chamber is formed which communicates with the interior of the barrel.
  • a pressure chamber is formed which communicates with the interior of the barrel.
  • the resulting force acts on the power piston on a drive linkage, which is part of the loading mechanism in the weapon, and the cartridge supply and removal, the closure movement, and possibly the tensioning of the trigger mechanism causes.
  • this mechanism is driven, so long the trigger is held in the pulled position.
  • the detonation energy released during the firing is thus diverted partially for the weapon drive.
  • the flow cross-sections, the design of the gas piston and the pressure chamber are tuned to a particular weapon that a desired firing frequency, the so-called. Cadence is set, and a mechanical overload of the drive mechanism is prevented.
  • the pressure chamber at the front end with an axial gas outlet opening for pressure adjustment and - vote.
  • the gas entering the gas cylinder from the barrel partly exits the gas cylinder or the pressure chamber into the environment, so that a lower pressure acts in the pressure chamber compared to the barrel.
  • Such an embodiment is also known from DE 196 15 181.
  • Changes to the weapon or the ammunition also change the gas pressure conditions in the barrel bore or in the gas cylinder. If, for example, a normally equipped weapon - with a muzzle brake - alternatively provided with a muffler, so increases the gas pressure in the barrel bore and thus also in the gas cylinder or in the pressure chamber. As a result, the working piston is accelerated more. This results in that also the loading or repeating process is accelerated in an automatic weapon. The same effect occurs when a different type of ammunition is used (higher propellant charge, higher projectile mass). The so accelerated charging also increases the cadence. This is accompanied by an increased consumption of ammunition and the mechanical stress on the weapons components is increasing rapidly.
  • the object of the present invention is to provide an improved gas take-off device which at least partially eliminates the problems described above.
  • the invention is characterized in that the effective flow cross-section is tuned to a weapons configuration via a separate insert.
  • Weapon configuration in this context means a certain equipment of a weapon or the use of a specific ammunition with a weapon.
  • a suitable flow cross-section can be realized in a simple manner via a suitably designed insert.
  • different inserts with corresponding flow cross sections which were determined for certain weapon configurations can be exchanged without further adjustments of the weapon.
  • claim 2 is such
  • Insert piece adjustable or removable designed to be used in the gas take-off arrangement is advantageous in so far as here the corresponding additional design and processing for the use of such an insert constructive and manufacturing technology is easy to implement.
  • an insert may have a plurality of different through holes, which then define the desired flow cross section corresponding to a specific operating position of the insert. In this way, it is possible to "switch" back and forth between several operating modes.
  • the adjustment is carried out according to claim 4 by rotating or moving the insert in the gas removal arrangement.
  • the latchable design according to claim 5 facilitates the repeatable setting of corresponding operating positions.
  • Claim 6 relates to a development in which a specially trained indentation has effective surfaces which cooperate with a securing element, so that over the active surfaces of at least one of the features Stellanschlag, latching surface, built-in fuse is realized.
  • Stellanschlag means in this context that the adjustment of the insert is prevented beyond certain limits;
  • Detent surfaces define the corresponding operating positions in the gas take-off arrangement;
  • Installation safety means that an unwanted removal is prevented by a corresponding locking effect between the fuse element and the indentation.
  • the indentation itself can be produced by correspondingly suitable machining methods (for example, turning, milling, grinding, precision casting, injection molding, etc.).
  • an indicator element is provided on the insert over which the operating position the insert becomes visible or palpable.
  • Indicator function is particularly important in weapons, as the shooter can thus determine either "at a glance” or "with a handle” the appropriate operating position.
  • the development according to claim 8 facilitates the operation of the insert, wherein a hexagon socket profile with common tools or a slot with readily available tools (for example, coin) can be actuated.
  • Claims 9 and 10 relate to a barrel assembly with a gas take-off assembly according to the invention or a weapon with such a barrel assembly.
  • FIG. 1 shows a longitudinal section through the mouth region of a barrel with a gas removal device according to the invention
  • FIG. 2 is an enlarged view of the gas take-off region of FIG. 1,
  • FIG. 5 shows a cross section through the gas removal order according to the invention in the region of the gas channel
  • Fig. 6 shows a longitudinal section (sectional plane A-A in
  • FIG. 7 is a perspective view of an insert for a gas removal arrangement according to the invention.
  • Fig. 1 shows the mouth region of a weapon with the barrel 1, at the front end of a muzzle fire brake 2 is arranged. Behind the muzzle fire brake a gas pickup 3 is fixed to the barrel, which is coupled via an unillustrated linkage with the shutter mechanism, also not shown.
  • the ignited propellant catapults the projectile from the cartridge case through the barrel bore 4, which runs concentrically to the so-called core axis 6, forward out of the barrel mouth through the orifice fire brake 2 in the direction of the target.
  • a part of the propellant gas enters a tapping bore 8, which runs radially in the barrel 1 transversely to the bore 4, and is introduced via a coaxially adjoining gas channel 10 in the gas take-off 3 out of the gas cylinder 12 formed pressure chamber 14.
  • a gas piston 16 which bears with a corresponding fit on the cylindrical inner wall of the gas cylinder 12 slidably.
  • the fit between the outer surface of the gas piston 16 and the cylindrical inner wall of the gas cylinder 12 is selected so that the gas piston 16 is arranged displaceably in the gas cylinder 12, but largely gas-tight.
  • the surfaces sliding along each other are mechanically processed accordingly (turning, milling, grinding, honing) and treated surfaces (hardened, chrome-plated, coated, etc.) to increase the durability. It can also be provided piston rings.
  • the propellant gas entering the pressure chamber 14 builds between the end face of the gas piston 16 and the end face of the gas cylinder 12 and the pressure chamber 14 to a working pressure, the gas piston 16 and thus the throttle linkage moves backwards, wherein the throttle linkage transmits the pressure pulse to the weapon drive which drives the shutter and loading mechanism (both not shown).
  • the gas take-off 3 and the gas cylinder 12 formed integrally thereon are connected to the barrel 1 via a collar 18.
  • the sleeve 18 can be shrunk with appropriate fit on a corresponding outer shell portion of the barrel 1.
  • the axial position on the barrel 1 is defined by a shoulder 20 against which the collar 18 rests with its rear end face 21.
  • the cuff 18 and thus the gas take-off 3 are additionally fixed axially and in the circumferential direction to the barrel 1.
  • the pinning 22 is realized for example via conical or dowel pins which pull the collar 18 in the region of the gas channel 10 down - transverse to the axis of the soul 6 - on the outside of the barrel 1, so that the outer mouth of the tapping channel 8 tightly into the mouth of the Gas channel 10 passes. This seal prevents gas losses between barrel 1 and cuff 18.
  • the gas piston 16 is provided at its front end with an auxiliary piston 16a, which partially immersed in the vent hole 24 in the illustrated in Fig. 2 starting position of the gas piston 16.
  • auxiliary piston 16a which partially immersed in the vent hole 24 in the illustrated in Fig. 2 starting position of the gas piston 16.
  • the vent hole 24 a part of the propellant gas passes forward through the outlet nozzle 26, when the gas piston 16 has moved under the action of the propellant gas a piece to the rear, so that the auxiliary piston 16 a, the vent hole 24 releases.
  • the pressure in the pressure chamber 14 is reduced and reduces the gas effect on the gas piston 16 and thus on the adjoining rear linkage.
  • a "softer" pressure curve on the gas piston 16 is realized. So are the forces on the subsequent linkage and the reload / shutter mechanism reduced.
  • an insert 30 is provided, which is inserted into a transverse to the gas channel 10 and the axis of the soul 6 extending through hole 32 (see also Fig. 5).
  • the insert 30 has in the illustrated embodiment, two at an angle of about 90 ° crossing and interpenetrating holes 10a and 10b, which have different diameters.
  • the bore 10a connects the running side end with the gas cylinder end of the gas channel 10.
  • the insert 30 By turning the insert 30 by 90 °, this can be adjusted so that the bore 10b connects the two ends of the gas channel 10 with each other.
  • the flow cross-section between the tapping bore 8 and the gas cylinder 12 and thus also the gas quantity flowing over it thus changes.
  • a fit is provided so that the non-active hole 10 a or 10 b, which is not aligned with the gas channel, is sealed by the inner wall or through hole 32.
  • This adjustment possibility to adjust the flow cross-section between the tap hole 8 and gas cylinder 12 and pressure chamber 14 in a fixed predefined manner allows to set the weapon to different modes to obtain the optimal cadence (protection frequency) in both modes.
  • the use of a muffler (not shown) instead of the muzzle fire brake 2 when firing the same ammunition increases the gas pressure in the bore 4.
  • This increased pressure would increase with unchanged gas channel cross section 10; 10a or 10b cause that would build up in the pressure chamber 14, a higher gas pressure, the in turn would lead to a higher acceleration of the gas piston 16.
  • This in turn would increase the weft cadence and thus cause a higher load or stress on the shutter and reload mechanism. In the worst case, it may even lead to the ejection mechanism is no longer reliable and the period for tracking a new cartridge from the magazine is too short, so that it can be reliably introduced from the closure assembly in the cartridge chamber.
  • the insert 30 can now be adjusted so that a bore 10a or 10b connects the tapping bore 8 with the pressure chamber 14 with a narrower cross-section.
  • the corresponding bore 10a or 10b thus throttles the overflowing gas so that the pressure builds up more slowly and thus the cadence remains constant.
  • a bore diameter of 1.7 mm bores 10a and 10b, respectively, is provided for use with a fire brake and a bore diameter of 1.2 mm for use with silencers.
  • the diameters may be generally between 0.5 and 2 mm.
  • the corresponding diameter must be adjusted and can also be in other areas.
  • Fig. 7 shows an enlarged perspective view of the insert 30.
  • the insert a Actuator 34, with a laterally projecting
  • Actuating and display wing 36 is provided.
  • An internal hexagonal profile 38 and an actuating slot 40 are introduced in the end face of the adjusting head 34 (FIG. 3). Both are for inserting corresponding tools or auxiliaries (e.g., a coin) to rotate the insert 30 in the through-bore 32 and thereby adjust the desired connection bore 10a or 10b.
  • corresponding tools or auxiliaries e.g., a coin
  • a recess 44 is provided, into which a securing element 46 can engage (FIG. 6).
  • the indentation 44 causes the following:
  • the front end 52 of the securing element 46 engages in the indentation 44 in a spring-loaded manner.
  • the corresponding spring force is biased via a compression spring 48, which is arranged together with the securing element 46 in a guide channel 49, via a locking pin 50.
  • Radial flanks 54 and 56 are connected to each other by fillets 58 and 60.
  • the indentation 44 and the bores 10a and 10b are matched in their arrangement to one another such that the fillets 58 and 60 each have a
  • the indentation 44 has two latching surfaces 62 and 64 which are connected to the end face 66 at the end 52 of Fuse element 46 cooperate.
  • Insert 30 moves the two locking surfaces 62 and 64 separating edge 63 on the end face 66 and thereby pushes the securing element 46 against the spring force. If a certain rotational position is exceeded, the end surface 66 pushes against the edge 63 under the action of the spring 48 and further rotates the insert 30 into its end position, in which the corresponding bore 10a or 10b is arranged in alignment with the gas channel 10.
  • the securing element 46 is provided with an actuating pin 68, which is accessible from outside via a groove 70 (FIG. 4). Over the actuating pin 68, the securing element 46 can be pushed out of engagement with the indentation 44, so that the insert 30 can be pushed out of the through hole 32. A shoulder 72 on the securing element 46 and a corresponding step 73 in the guide channel 49 prevent the securing element 46 from completely slipping into the through hole 32 when the actuating pin is released - with the insert piece 30 removed.
  • an insert 30 is provided with two through holes 10a, 10b. In other embodiments, however, a plurality of crosswise disposed through holes may be provided, so that more than two different bore settings can be made. There are also embodiments in which a corresponding insert 30 has only a single bore and the gas metering can be made via a corresponding replacement of such inserts.
  • the passage bores can also be arranged next to one another, ie in different axial positions on the shaft region 42. These holes can then by appropriate insertion or removal of the insert 30 with the gas channel 10 for Escapes are brought. The insert 30 is then as
  • Such a mechanism is to be provided with a corresponding locking device.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

La présente invention concerne un arrangement (3) de réduction des gaz pour un canon (1). Selon l'invention, l'arrangement (3) de réduction des gaz comprend un cylindre (12) à gaz qui est en liaison communicante avec l'orifice (4) du canon par le biais d'un conduit (8, 10, 10a ; 10b) de liaison. Il est ici prévu une pièce (30) d'entrée qui détermine la section (10a ; 10b) transversale d'écoulement efficace et ainsi la pression de travail dans le cylindre (12) à gaz en fonction d'une configuration d'arme à feu donnée. L'invention concerne également un sous-ensemble canon ou une arme équipé d'un tel arrangement (3) de réduction des gaz.
PCT/EP2007/006780 2006-08-03 2007-07-31 Arrangement de réduction des gaz et canon ou arme équipé d'un Arrangement de réduction des gaz Ceased WO2008014984A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CA002659573A CA2659573A1 (fr) 2006-08-03 2007-07-31 Arrangement de reduction des gaz et canon ou arme equipe d'un arrangement de reduction des gaz
EP07786474A EP2047204A1 (fr) 2006-08-03 2007-07-31 Arrangement de réduction des gaz et canon ou arme équipé d'un arrangement de réduction des gaz
US12/364,320 US20090229454A1 (en) 2006-08-03 2009-02-02 Field adjustable gas bleed assemblies for use with firearms

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE102006036309 2006-08-03
DE102006036309.4 2006-08-03
DE102006056130A DE102006056130A1 (de) 2006-08-03 2006-11-28 Gasabnahmeanordnung und Lauf bzw. Waffe mit einer Gasabnahmeanordnung
DE102006056130.9 2006-11-28

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US12/364,320 Continuation US20090229454A1 (en) 2006-08-03 2009-02-02 Field adjustable gas bleed assemblies for use with firearms

Publications (1)

Publication Number Publication Date
WO2008014984A1 true WO2008014984A1 (fr) 2008-02-07

Family

ID=38670523

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2007/006780 Ceased WO2008014984A1 (fr) 2006-08-03 2007-07-31 Arrangement de réduction des gaz et canon ou arme équipé d'un Arrangement de réduction des gaz

Country Status (6)

Country Link
US (1) US20090229454A1 (fr)
EP (1) EP2047204A1 (fr)
KR (1) KR20090043503A (fr)
CA (1) CA2659573A1 (fr)
DE (1) DE102006056130A1 (fr)
WO (1) WO2008014984A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010123604A3 (fr) * 2009-01-27 2011-01-06 Windauer Bernard T Bloc gaz à régulation de pression
US20120003390A1 (en) * 2008-12-19 2012-01-05 Advanced Interconnect Materials, Llc Copper interconnection structure and method for forming copper interconnections
US8528458B2 (en) 2011-07-27 2013-09-10 Bernard T. Windauer Pressure-regulating gas block
US9719739B2 (en) 2014-02-06 2017-08-01 Bernard (Bernie) T. Windauer Gas block balancing piston for auto-loading firearm
US20230122319A1 (en) * 2021-10-15 2023-04-20 Heckler & Koch Gmbh Gas block for automatic firearms

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US7891284B1 (en) * 2007-06-06 2011-02-22 Christopher Gene Barrett Firearm with gas system accessory latch
US9261314B1 (en) 2010-07-19 2016-02-16 Jason Stewart Jackson Sleeve piston for actuating a firearm bolt carrier
US8671818B1 (en) 2010-11-30 2014-03-18 O.S.S. Holdings, LLC Firearm discharge gas flow control
US8813632B2 (en) * 2011-07-19 2014-08-26 Jason Mark Adams Adjustable firearm gas block
US8701543B2 (en) * 2011-09-06 2014-04-22 Armalite, Inc. Adjustable gas system for firearms
US8869674B2 (en) 2012-02-14 2014-10-28 Michael Alan Ruck Gas piston control system for a firearm
US8893608B2 (en) * 2012-07-03 2014-11-25 Lawrence S. Kramer Gas piston system for M16/AR15 rifle or M4 carbine systems
US9383149B2 (en) 2012-12-05 2016-07-05 Ra Brands, L.L.C. Gas-operated firearm with pressure compensating gas piston
US9097475B2 (en) 2012-12-05 2015-08-04 Ra Brands, L.L.C. Gas-operated firearm with pressure compensating gas piston
US9212856B2 (en) 2012-12-26 2015-12-15 Ra Brands, L.L.C. Gas cut-off system for firearms
US8950313B2 (en) 2013-01-04 2015-02-10 Ra Brands, L.L.C. Self regulating gas system for suppressed weapons
US8887616B2 (en) 2013-01-11 2014-11-18 Ra Brands, L.L.C. Auto regulating gas system for supressed weapons
US9766026B2 (en) 2013-10-21 2017-09-19 Sig Sauer, Inc. Gas operating system for an automatic pistol-caliber firearm
US9500423B2 (en) 2014-01-24 2016-11-22 Ra Brands, L.L.C. Method and mechanism for automatic regulation of gas flow when mounting a suppressor to a firearm
US9903675B2 (en) * 2014-12-22 2018-02-27 Charles B. Cassels Multi-block gas regulator
US9335106B1 (en) * 2014-12-23 2016-05-10 Smith & Wesson Corp. Adjustable gas block
US9273916B1 (en) * 2015-01-05 2016-03-01 Carmelo Russo Firearm impingement system having adjustable gas block
US9816769B1 (en) 2016-10-25 2017-11-14 Ambimjb, Llc Gas piston firearm system and method
DE102016121070B4 (de) 2016-11-04 2018-05-17 C. G. Haenel GmbH Verstellbare Gasabnahmeanordnung für eine Gasdrucklader-Schusswaffe
DE102017002165B4 (de) 2017-03-07 2018-12-27 Heckler & Koch Gmbh Gasabnahme und damit ausgestattetes Waffenrohr sowie Selbstladefeuerwaffe mit einer solchen Gasabnahme
US10466000B2 (en) * 2017-08-07 2019-11-05 Todd Conrad Gardner Gas flow volume control apparatus for firearms
US10690425B2 (en) 2017-12-22 2020-06-23 Charles B. Cassels Firearm with locked breech rotating bolt pistol
US10935335B2 (en) 2018-02-06 2021-03-02 Adams Arms, Llc Gas regulation system
EP3800426B1 (fr) 2019-10-04 2022-05-18 Glock Technology GmbH Arme à feu à réarmement par emprunt de gaz
US11280567B1 (en) 2019-11-25 2022-03-22 Heckler & Koch Inc. Adjustable gas piston action firearm
US11680762B2 (en) * 2020-12-21 2023-06-20 Caracal International, Llc Firearm with adjustable gas block regulator
US11506460B1 (en) * 2021-05-24 2022-11-22 Fuller Phoenix, Llc Multi-modal gas blocks for gas piston-operated firearms
US20230349651A1 (en) * 2022-04-27 2023-11-02 Surefire, Llc Adjustable gas regulator valve for direct gas operated firearms
US20240377150A1 (en) * 2023-05-12 2024-11-14 Polaris Capital Corporation Adjustable gas regulating systems and apparatuses
US20250290715A1 (en) * 2023-05-12 2025-09-18 Zero Line, Inc. Recoilless Gas Block System

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GB191000482A (fr) *
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DE648391C (de) 1932-02-22 1937-07-30 Fridtjof N Brondby Gasdrucklader
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CH631542A5 (en) * 1978-08-10 1982-08-13 Oerlikon Buehrle Ag Device for adjusting the firing rate of an automatic firearm
EP0380041A1 (fr) * 1989-01-27 1990-08-01 Mauser-Werke Oberndorf GmbH Régulateur pour la pression des gaz
DE19615181A1 (de) 1996-04-17 1997-10-23 Heckler & Koch Gmbh Gasdruckladendes Selbstladegewehr

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GB191000482A (fr) *
BE332360A (fr) * 1925-02-20 1926-03-31 Vickers Ltd Perfectionnements aux mitrailleuses et aux armes à feu automatiques
DE648391C (de) 1932-02-22 1937-07-30 Fridtjof N Brondby Gasdrucklader
US2748662A (en) * 1952-11-07 1956-06-05 Clarence E Simpson Gas regulating device for a firearm
CH631542A5 (en) * 1978-08-10 1982-08-13 Oerlikon Buehrle Ag Device for adjusting the firing rate of an automatic firearm
EP0380041A1 (fr) * 1989-01-27 1990-08-01 Mauser-Werke Oberndorf GmbH Régulateur pour la pression des gaz
DE19615181A1 (de) 1996-04-17 1997-10-23 Heckler & Koch Gmbh Gasdruckladendes Selbstladegewehr

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120003390A1 (en) * 2008-12-19 2012-01-05 Advanced Interconnect Materials, Llc Copper interconnection structure and method for forming copper interconnections
WO2010123604A3 (fr) * 2009-01-27 2011-01-06 Windauer Bernard T Bloc gaz à régulation de pression
US8528458B2 (en) 2011-07-27 2013-09-10 Bernard T. Windauer Pressure-regulating gas block
US9719739B2 (en) 2014-02-06 2017-08-01 Bernard (Bernie) T. Windauer Gas block balancing piston for auto-loading firearm
US20230122319A1 (en) * 2021-10-15 2023-04-20 Heckler & Koch Gmbh Gas block for automatic firearms
US12188738B2 (en) * 2021-10-15 2025-01-07 Heckler &Koch Gmbh Gas block for automatic firearms

Also Published As

Publication number Publication date
DE102006056130A1 (de) 2008-02-07
US20090229454A1 (en) 2009-09-17
KR20090043503A (ko) 2009-05-06
EP2047204A1 (fr) 2009-04-15
CA2659573A1 (fr) 2008-02-07

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