DE551830C - air force - Google Patents

air force

Info

Publication number
DE551830C
DE551830C DENDAT551830D DE551830DD DE551830C DE 551830 C DE551830 C DE 551830C DE NDAT551830 D DENDAT551830 D DE NDAT551830D DE 551830D D DE551830D D DE 551830DD DE 551830 C DE551830 C DE 551830C
Authority
DE
Germany
Prior art keywords
barrel
tabs
resilient tabs
air force
cylinder
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
Application number
DENDAT551830D
Other languages
German (de)
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.)
Dianawerk Mayer & Grammelspach
Original Assignee
Dianawerk Mayer & Grammelspach
Publication date
Application granted granted Critical
Publication of DE551830C publication Critical patent/DE551830C/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41BWEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
    • F41B11/00Compressed-gas guns, e.g. air guns; Steam guns
    • F41B11/60Compressed-gas guns, e.g. air guns; Steam guns characterised by the supply of compressed gas
    • F41B11/64Compressed-gas guns, e.g. air guns; Steam guns characterised by the supply of compressed gas having a piston effecting a compressor stroke during the firing of each shot
    • F41B11/642Compressed-gas guns, e.g. air guns; Steam guns characterised by the supply of compressed gas having a piston effecting a compressor stroke during the firing of each shot the piston being spring operated
    • F41B11/646Arrangements for putting the spring under tension
    • F41B11/647Arrangements for putting the spring under tension by a rocker lever
    • F41B11/648Arrangements for putting the spring under tension by a rocker lever in breakdown air guns

Landscapes

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

Description

Luftwaffe Es sind Vorderladerluftwaffen mit um ;einen Scharnierbolzen drehbaren Kipplauf bekannt, welcher in seiner gestreckten Lage dadurch festgehalten wird, daß sich zwei am Spannhebel angebrachte federnde Lappen an die Drehachse des Kipplaufes anlegen. Gemäß der Erfindung wird diese Drehachse durch zwei sich gegenüberstehende Schrauben mit abgerundeten oder keil- oder kegelförmigen Enden gebildet, hinter welchen nach Zurückbewegung des Laufes in die Schußstellung die federnden Lappen des Spannhebels einschnappen. Wird diese Anordnung bei Hinterladerluftwaffen angebracht, so kann mit ihrer Hilfe in einfacher Weise eine Dichtung der von der Laufanschlagfläche gebildeten Ladestelle erzielt werden, ohne daß hierfür wie bei vorbekannten, dem gleichen Zwecke dienenden Einrichtungen weitere von Hand zu betätigende Hilfsteile notwendig sind.Luftwaffe There are muzzle-loading air forces with around; a hinge pin rotatable tilt barrel known, which is thereby held in its extended position that two resilient tabs attached to the tensioning lever are attached to the axis of rotation of the Put on a breakaway. According to the invention, this axis of rotation is through two opposing Bolts formed with rounded or tapered or tapered ends, behind which after moving the barrel back into the firing position the resilient tabs of the clamping lever snap into place. If this arrangement is applied to breech-loading air weapons, with their help, a seal can be made from the barrel stop surface in a simple manner formed loading point can be achieved without this as with previously known, the facilities serving the same purpose other manually operated auxiliary parts are necessary.

Eine Ausführungsform des Erfindungsgegenstandes ist in Fig. t im Längsschnitt bei abgedrückter Waffe und geschlossenem Lauf, in Fig.2 bei gespannter Waffe und offenem Lauf je im Längsschnitt zur Darstellung gebracht.An embodiment of the subject matter of the invention is shown in Fig. T in longitudinal section with the gun pulled and the barrel closed, in Fig. 2 with the gun cocked and open barrel each shown in a longitudinal section.

Fig. 3 zeigt einen Querschnitt nach der Linie A. -B von Fig. r.Fig. 3 shows a cross section along the line A. -B of Fig. R.

a ist der Zylinder mit dem durch. Feder bewegten Kolben b und der vorderen Anschlagfläche c. In den beiden Lappen a1 des Zylinders a sind Schraubend' gelagert, durch welche der Lauf e mit dem Zylinder a kippbar verbunden ist. Diese Schrauben sind: an ihrer Innenseite mit Rundköpfen d2 versehen, während sie auf der äußeren Seite je einen Kopf d3, tragen. f ist die Anschlagfläche des Laufes s und g der mit dem letzteren bei lt gelenkig verbundene, am Zylinder in bekannter Weise geführte Spannhebel. Dieser ist mit den beiden Lappen h versehen, welche mit den Rundköpfen d2 entsprechenden Vertiefungen h1 ausgestattet sind. Der Spannhebel g ist mit den federnden Lappen h aus einem Stück Blech in dem aus Fig.3 ersichtlichen U-förmigen Querschnitt gestanzt. Die beiden Lappen a1 des Zylinders sind durch einen Steg g miteinander verbunden.a is the cylinder with the through. Spring moving piston b and the front stop surface c. Screws' are mounted in the two tabs a1 of the cylinder a, by means of which the barrel e is tiltably connected to the cylinder a. These screws are: provided with round heads d2 on their inside, while they each have a head d3 on the outside. f is the stop surface of the barrel s and g is the clamping lever articulated to the latter at lt and guided in a known manner on the cylinder. This is provided with the two tabs h, which are equipped with recesses h1 corresponding to the round heads d2. The tensioning lever g is punched with the resilient tabs h from a piece of sheet metal in the U-shaped cross section shown in FIG. The two tabs a1 of the cylinder are connected to one another by a web g.

Beim Einschwenken des Laufes in die Schußstellung gleiten die beiden Lappen h zwischen den beiden Rundköpfen d2 der Schraubend' hindurch. Da der Abstand der Lappen voneinander größer ist als jener der Rundköpfe d2, so federn die Lappen beim Verbringen der Luftwaffe in Schußstellung so lange nach innen, bis ihre Vertiefungen hl die Rundköpfe erreicht haben, worauf die Lappen hinter denselben einschnappen und sich mittels ihrer Vertiefungen gegen die Rundköpfe legen. Dadurch wird der Lauf sicher in der S.cliußstellung gehalten.When swiveling the barrel into the firing position, the two slide Lobe h between the two round heads d2 of the screw through. Because the distance If the lobes of one another are larger than that of the round heads d2, the lobes spring when the Luftwaffe is in the firing position inwards until it is deepened hl have reached the round heads, whereupon the tabs snap into place behind them and lay down against the round heads by means of their indentations. This will make the Barrel held securely in the closed position.

Claims (1)

PATENTANSPRUCH: Luftwaffe mit um einen Scharnierbolzen drehbaren Kipplauf, welcher in seiner gestreckten Lage dadurch festgehalten wird, da.ß sich zwei am Spannhebel angle, -brachte federnde Lappen an die Drehachse des Kipplaufes anlegen, dadurch gekennzeichnet, daß diese durch zwei sich gegenüberstehende Schrauben (dl) mit abgerundeten oder keil- oder kegelförmigen Enden (d2) gebildet wird, hinter welchen nach Zurückbewegung des Laufes in Schußstellung die federnden Lappen (h) des Spannhebels einschnappen.PATENT CLAIM: Luftwaffe with a tilt barrel rotatable around a hinge pin, which is held in its stretched position by the fact that two on the Tension lever angle, - put resilient tabs on the axis of rotation of the tilt barrel, characterized in that it is secured by two opposing screws (dl) with rounded or wedge-shaped or conical ends (d2) is formed behind which, after the barrel has moved back into the firing position, the resilient tabs (h) of the clamping lever snap into place.
DENDAT551830D air force Expired DE551830C (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE551830T

Publications (1)

Publication Number Publication Date
DE551830C true DE551830C (en) 1932-06-06

Family

ID=6563182

Family Applications (1)

Application Number Title Priority Date Filing Date
DENDAT551830D Expired DE551830C (en) air force

Country Status (1)

Country Link
DE (1) DE551830C (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1030735B (en) * 1956-07-10 1958-05-22 J G Anschuetz G M B H Air rifle
DE1120934B (en) * 1959-05-19 1961-12-28 Birmingham Small Arms Co Ltd Air rifle cylinder
DE202018104651U1 (en) 2018-08-14 2019-11-15 German Sport Guns Gmbh Clamping system for a compressed air weapon
DE102018119676A1 (en) * 2018-08-14 2020-02-20 German Sport Guns Gmbh Clamping system for a compressed air weapon

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1030735B (en) * 1956-07-10 1958-05-22 J G Anschuetz G M B H Air rifle
DE1120934B (en) * 1959-05-19 1961-12-28 Birmingham Small Arms Co Ltd Air rifle cylinder
DE202018104651U1 (en) 2018-08-14 2019-11-15 German Sport Guns Gmbh Clamping system for a compressed air weapon
DE102018119676A1 (en) * 2018-08-14 2020-02-20 German Sport Guns Gmbh Clamping system for a compressed air weapon
WO2020035173A1 (en) 2018-08-14 2020-02-20 German Sport Guns Gmbh Charging system for an air gun

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