DE1578006C - Tube for flight stabilized missiles - Google Patents
Tube for flight stabilized missilesInfo
- Publication number
- DE1578006C DE1578006C DE19671578006 DE1578006A DE1578006C DE 1578006 C DE1578006 C DE 1578006C DE 19671578006 DE19671578006 DE 19671578006 DE 1578006 A DE1578006 A DE 1578006A DE 1578006 C DE1578006 C DE 1578006C
- Authority
- DE
- Germany
- Prior art keywords
- pipe
- parts
- tube
- barrel
- connection
- 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
Links
- 230000000630 rising Effects 0.000 claims description 2
- 230000023298 conjugation with cellular fusion Effects 0.000 claims 2
- 230000013011 mating Effects 0.000 claims 2
- 239000004570 mortar (masonry) Substances 0.000 claims 2
- 230000021037 unidirectional conjugation Effects 0.000 claims 2
- 210000002105 Tongue Anatomy 0.000 claims 1
- 238000004140 cleaning Methods 0.000 claims 1
- 238000011109 contamination Methods 0.000 claims 1
- 230000001808 coupling Effects 0.000 claims 1
- 238000010168 coupling process Methods 0.000 claims 1
- 238000005859 coupling reaction Methods 0.000 claims 1
- 239000000789 fastener Substances 0.000 claims 1
- 239000002245 particle Substances 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 238000004642 transportation engineering Methods 0.000 claims 1
- 239000007789 gas Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 1
Description
Rohrteile 2 und 3 hinsichtlich der Länge 4 so aufeinander abgestimmt, daß die Führungsfläche 8 b nicht ganz von der Muffe 4 bedeckt wird, so daß die Nuten 10 in öffnungen 11 nach außen treten können. Ein an den Verbindungsflächen befindlicher Schmutz wird beim Zusammenschrauben der Rohrteile in die Nuten 10 geschoben, aus welchen sich der Schmutz ausblasen läßt. Die Nut 10 läuft bei 10 α zweckmäßig sanft ansteigend aus. Die Nuten dienen noch dem Zweck zu erkennen, ob die Stirnflächen 9 α und 9 b nicht fest gegeneinander verschraubt sind. Bei den durchlaufenden Längsnuten werden die Gase frei abgeleitet und es wird die Fehlerquelle erkannt. Bei Fehlen der Längsnuten 10 können die austretenden Pulvergase Verschweißungen an den Führungsflächen bzw. dem Gewinde verursachen. Die auf dem Umfang verteilt angeordneten Sacklöcher 14 und 15 dienen zum Eingriff von hakenförmigen Schlüsseln.Pipe parts 2 and 3 matched to one another in terms of length 4 so that the guide surface 8 b is not completely covered by the sleeve 4, so that the grooves 10 can emerge in openings 11 to the outside. Any dirt on the connecting surfaces is pushed into the grooves 10 when the pipe parts are screwed together, from which the dirt can be blown out. The groove 10 expediently ends in a gently rising manner at 10 α. The grooves also serve the purpose of recognizing whether the end faces 9 α and 9 b are not screwed tightly against one another. With the continuous longitudinal grooves, the gases are discharged freely and the source of the error is recognized. In the absence of the longitudinal grooves 10, the powder gases escaping can cause welds on the guide surfaces or the thread. The blind holes 14 and 15, which are arranged distributed around the circumference, are used for the engagement of hook-shaped keys.
Hierzu 1 Blatt Zeichnungen1 sheet of drawings
Claims (2)
den des Granatwerfers von der Mitte;des Laufs aus Fig.2 veranschaulicht eine Draufsicht auf das,around one in the area of the closed. Rohrbdens .'F i g. 1 shows the tube for the wing-stabilized lying transverse axis can be swiveled out so that a shaft according to the invention in a longitudinal section,
that of the grenade launcher from the middle; the barrel of Fig. 2 illustrates a top view of the,
den Lauf teile erfolgt einerseits durch eine äußere Füh- . In Fig. 3 ist ein Querschnitt nach der Linie IH-III rung und andererseits durch einen lösbaren, gasdich-. der F i g. 1 dargestellt.To be made; The connection of the two 45, tube of Fig. 1. ;: -.-- ■ - + ■■ ^ '-, - r
the running parts are carried out on the one hand by an external guide. In Fig. 3 is a cross section along the line IH-III tion and on the other hand through a detachable, gas-tight. the F i g. 1 shown.
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19671578006 DE1578006C (en) | 1967-06-05 | 1967-06-05 | Tube for flight stabilized missiles |
IL30097A IL30097A (en) | 1967-06-05 | 1968-05-29 | Dismountable barrel for fin-stabilized projectiles in particular for mortars |
NO2122/68A NO121537B (en) | 1967-06-05 | 1968-05-30 | |
US733970A US3486411A (en) | 1967-06-05 | 1968-06-03 | Multiportion barrel for a launcher of fin-stabilized projectiles |
DK260368AA DK118807B (en) | 1967-06-05 | 1968-06-04 | Separate mortar pipe. |
SE07457/68A SE349140B (en) | 1967-06-05 | 1968-06-04 | |
GB26408/68A GB1222674A (en) | 1967-06-05 | 1968-06-04 | A barrel for a launcher for fin-stabilised projectiles |
FI681563A FI52773C (en) | 1967-06-05 | 1968-06-05 | Pipe for wing-stabilized munitions. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEE0034121 | 1967-06-05 | ||
DE19671578006 DE1578006C (en) | 1967-06-05 | 1967-06-05 | Tube for flight stabilized missiles |
Publications (2)
Publication Number | Publication Date |
---|---|
DE1578006A1 DE1578006A1 (en) | 1971-09-23 |
DE1578006C true DE1578006C (en) | 1973-04-19 |
Family
ID=
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