NO130627B - - Google Patents

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Publication number
NO130627B
NO130627B NO03293/71A NO329371A NO130627B NO 130627 B NO130627 B NO 130627B NO 03293/71 A NO03293/71 A NO 03293/71A NO 329371 A NO329371 A NO 329371A NO 130627 B NO130627 B NO 130627B
Authority
NO
Norway
Prior art keywords
sight
grenade
devices
launch
grenades
Prior art date
Application number
NO03293/71A
Other languages
Norwegian (no)
Other versions
NO130627C (en
Inventor
Gerard Aguinet
Jean Manoury
Edouard Martin
Original Assignee
Ugine Kuhlmann
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 Ugine Kuhlmann filed Critical Ugine Kuhlmann
Publication of NO130627B publication Critical patent/NO130627B/no
Publication of NO130627C publication Critical patent/NO130627C/no

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D3/00Distillation or related exchange processes in which liquids are contacted with gaseous media, e.g. stripping
    • B01D3/14Fractional distillation or use of a fractionation or rectification column
    • B01D3/32Other features of fractionating columns ; Constructional details of fractionating columns not provided for in groups B01D3/16 - B01D3/30
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01JCHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J23/00Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00
    • B01J23/70Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00 of the iron group metals or copper
    • B01J23/76Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00 of the iron group metals or copper combined with metals, oxides or hydroxides provided for in groups B01J23/02 - B01J23/36
    • B01J23/84Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00 of the iron group metals or copper combined with metals, oxides or hydroxides provided for in groups B01J23/02 - B01J23/36 with arsenic, antimony, bismuth, vanadium, niobium, tantalum, polonium, chromium, molybdenum, tungsten, manganese, technetium or rhenium
    • B01J23/85Chromium, molybdenum or tungsten
    • B01J23/86Chromium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01JCHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J35/00Catalysts, in general, characterised by their form or physical properties
    • B01J35/50Catalysts, in general, characterised by their form or physical properties characterised by their shape or configuration
    • B01J35/58Fabrics or filaments
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01BNON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B21/00Nitrogen; Compounds thereof
    • C01B21/20Nitrogen oxides; Oxyacids of nitrogen; Salts thereof
    • C01B21/24Nitric oxide (NO)
    • C01B21/26Preparation by catalytic or non-catalytic oxidation of ammonia
    • C01B21/265Preparation by catalytic or non-catalytic oxidation of ammonia characterised by the catalyst

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Woven Fabrics (AREA)
  • Filtering Materials (AREA)
  • Catalysts (AREA)
  • Filtering Of Dispersed Particles In Gases (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Telescopes (AREA)
  • Laminated Bodies (AREA)

Description

Sikteinnretning for utskyting av geværgranater og lignende. Sighting device for launching rifle grenades and the like.

Der kjennes nå forskjellige typer av geværgranater (antitank-granater, anti-personell-granater, røkgranater etc), hvis ballistiske egenskaper, særlig vekt, er i be-tydelig grad forskjellige. Utskyning av disse granater foregår vanligvis ved hjelp av et avtagbar utskytningshåndtak forsynt med et siktegitter som for å gi gitteret en ålment anvendelig karakter har flere rek-ker av forskjellige avstandsmerker, hvilket ofte virker forvirrende ved avlesningen og øker faren for feilavlesing. There are now different types of rifle grenades (anti-tank grenades, anti-personnel grenades, smoke grenades, etc.), whose ballistic properties, especially weight, are significantly different. Launching of these grenades usually takes place with the help of a removable launch handle equipped with a sight grid which, in order to give the grid a generally applicable character, has several rows of different distance marks, which often seems confusing when reading and increases the risk of misreading.

Når på den annen side geværet bæres When, on the other hand, the rifle is carried

uforsiktig, er der fare for at disse gittere henger seg fast og at de under transport blir utsatt for støt, hvorved de vil bli unøy-aktige. Vekten av disse gittere som er an-bragt ved enden av geværløpet, forstyrrer endelig likevekten av våpnet i utskytings-øyeblikket. careless, there is a danger that these grids will get stuck and that they will be exposed to shocks during transport, whereby they will become inaccurate. The weight of these grids, which are placed at the end of the gun barrel, finally disturbs the equilibrium of the weapon at the moment of launch.

Sikteinnretningen ifølge oppfinnelsen The sighting device according to the invention

avhjelper disse ulemper, og innretningen utmerker seg ved et avtagbart sikte forsynt med anordninger som før utskytingen tillater befestigelse av siktet på prosjektilet og som bevirket at sikten efter utskytingen faller av, idet innretningen tar så lite plass at den kan anbringes inne i granatens hale. remedies these disadvantages, and the device is distinguished by a removable sight equipped with devices that allow the sight to be attached to the projectile before launch and which cause the sight to fall off after launch, as the device takes up so little space that it can be placed inside the tail of the grenade.

Tegningen viser et utførelseseksempel The drawing shows a design example

på innretningen ifølge oppfinnelsen. Her er fig. 1 et lengdesnitt av en granathale som inneholder sprengladningen og sikteinnretningen, fig. 2 et sideriss av innretningen montert på granatens styrevinge, og fig. 3 et oppriss. on the device according to the invention. Here is fig. 1 a longitudinal section of a grenade tail containing the explosive charge and the aiming device, fig. 2 a side view of the device mounted on the grenade's control wing, and fig. 3 a survey.

Den på tegningen viste innretning dan-ner et sikte som tillater innstilling av sky-teobjektet på en rett linje som berører so-nen for den største diameter av granatle-gemet og passerer gjennom den til den ønskede avstand svarende siktehøyde. Siktet består av en stav 1, fortrinsvis av syntetisk gjennomsiktig materiale, som omfatter et antall utsparinger 2 anordnet i trinn og anordnet i innbyrdes avstander i overensstemmelse med den ønskede skyte-avstand. Staven kan selvsagt også fremstil-les av et annet materiale og omfatte malte eller graverte markeringer. The device shown in the drawing forms a sight which allows setting the shooting object on a straight line which touches the zone of the largest diameter of the shell body and passes through it to the desired distance corresponding to the sight height. The sight consists of a rod 1, preferably of synthetic transparent material, which comprises a number of recesses 2 arranged in steps and arranged at mutual distances in accordance with the desired shooting distance. The rod can of course also be made of another material and include painted or engraved markings.

Staven 1 er på forsiden forsynt med en klemme 3 som er bestemt til å gripe over den bakre del av en av syntetisk harpiks bestående styrevinge 4 anordnet ved enden av halen 5 i en geværgranat. Klemmen omfatter to elastiske blad som holder siktet fast til granatens styrevinge, idet dia-meterstillingen av siktet i forhold til granatens lengdeakse bestemmes av et anslag 6 som hviler mot den ytre kant av bærevingen og er anordnet loddrett på horisontalplanet. The rod 1 is provided on the front side with a clamp 3 which is intended to grip over the rear part of a synthetic resin control wing 4 arranged at the end of the tail 5 of a rifle grenade. The clamp comprises two elastic blades which hold the sight firmly to the grenade's guide wing, the diameter position of the sight in relation to the grenade's longitudinal axis being determined by a stop 6 which rests against the outer edge of the carrier wing and is arranged vertically on the horizontal plane.

Under transport og lagring kan sikteinnretningen plaseres i granatens hale 5 som er lukket med en propp 7 med spreng-ladning 8 (fig. 1). Når skytteren ved sky-ting fjerne proppen 7 for å anbringe granaten på skytehåndtaket, tar han ut fra granatens hale en sikteinnretning som der ligger fullstendig beskyttet og som svarer nøyaktig til den brukte granattype. Hver mulighet for feil er derved eliminert. During transport and storage, the sighting device can be placed in the grenade's tail 5, which is closed with a stopper 7 with an explosive charge 8 (fig. 1). When the shooter removes the plug 7 in order to place the grenade on the firing handle, he takes out from the tail of the grenade an aiming device which is completely protected there and which corresponds exactly to the type of grenade used. Every possibility of error is thereby eliminated.

Siktet festes til projektilet på en slik måte at hele sikteinnretningen efter av-skyting av granaten faller av og ned bare noen få skritt fra skyteren som følge av den kombinerte virkning av granatens ak-sellerasjon og luftmotstanden. The sight is attached to the projectile in such a way that, after firing the grenade, the entire aiming device falls off and down just a few steps from the shooter as a result of the combined effect of the grenade's acceleration and air resistance.

Det er klart at den måte på hvilken It is clear that the way in which

siktet festes til granaten, kan varieres og the sight is attached to the grenade, can be varied and

at tegningen bare viser ett eksempel. Hvis that the drawing only shows one example. If

styrevingen omfatter en ringformet del the control vane comprises an annular part

som omgir vingene kan siktet anbringes der which surrounds the wings, the scope can be placed there

eller på en radial vinge. or on a radial wing.

Oppfinnelsens gjenstand kan brukes The subject matter of the invention can be used

ved granater som skytes ut ved hjelp av by grenades launched by means of

hvilket som helst skytevåpen, f. eks. et any firearm, e.g. a

gevær, en pistol eller lignende. rifle, a pistol or the like.

Claims (4)

1. Sikteinnretning for utskyting av geværgranater og lignende, karakterisert ved1. Sighting device for launching rifle grenades and the like, characterized by et avtagbart sikte med anordninger som før utskytingen tillater befestigelse av sik- tet til prosjektilet og som bevirker at sik tet efter utskytingen faller av, idet innretningen tar så lite plass at den kan anbringes inne i granatens hale. a removable sight with devices that before launch allow the sight to be attached to the projectile and which causes the sight soon after launch falls off, as the device takes up so little space that it can be placed inside the grenade's tail. 2. Innretning ifølge påstand 1, karakterisert ved anordninger som tillater befestigelse av siktet til en styrevinge på granaten. 2. Device according to claim 1, characterized by devices that allow attachment of the sight to a control wing on the grenade. 3. Innretning ifølge påstand 1 og 2, karakterisert ved at nevnte anordninger består av en klemme som er fast forbundet med forsiden av siktet og som griper om den bakre del av styrevingen. 3. Device according to claims 1 and 2, characterized in that said devices consist of a clamp which is firmly connected to the front of the sight and which grips the rear part of the control wing. 4. Innretning ifølge påstand 1, karakterisert ved at den omfatter et anslag (6) på siktet, som bestemmer diameterstillin-gen av siktet i forhold til granatens lengdeakse.4. Device according to claim 1, characterized in that it comprises a stop (6) on the sight, which determines the diameter position of the sight in relation to the grenade's longitudinal axis.
NO3293/71A 1970-09-04 1971-09-03 NO130627C (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7032304A FR2104921B1 (en) 1970-09-04 1970-09-04

Publications (2)

Publication Number Publication Date
NO130627B true NO130627B (en) 1974-10-07
NO130627C NO130627C (en) 1975-01-15

Family

ID=9060926

Family Applications (1)

Application Number Title Priority Date Filing Date
NO3293/71A NO130627C (en) 1970-09-04 1971-09-03

Country Status (16)

Country Link
JP (1) JPS524509B1 (en)
AT (1) AT314483B (en)
AU (1) AU466822B2 (en)
BE (1) BE771484A (en)
BR (1) BR7105727D0 (en)
CA (1) CA989747A (en)
CH (1) CH539506A (en)
DE (1) DE2141106C3 (en)
ES (1) ES196796Y (en)
FR (1) FR2104921B1 (en)
GB (1) GB1353979A (en)
IE (1) IE35584B1 (en)
NL (1) NL144170B (en)
NO (1) NO130627C (en)
SE (1) SE393934B (en)
SU (1) SU604465A3 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2000045B (en) * 1977-06-20 1982-01-20 Atomic Energy Authority Uk Improvements in or relating to fluid treatment devices

Also Published As

Publication number Publication date
DE2141106B2 (en) 1975-04-10
NL7111858A (en) 1972-03-07
ES196796Y (en) 1975-08-16
JPS524509B1 (en) 1977-02-04
SU604465A3 (en) 1978-04-25
CA989747A (en) 1976-05-25
IE35584L (en) 1972-03-04
FR2104921A1 (en) 1972-04-28
AT314483B (en) 1974-04-10
DE2141106C3 (en) 1975-11-27
AU466822B2 (en) 1975-11-13
CH539506A (en) 1973-07-31
BE771484A (en) 1972-02-18
IE35584B1 (en) 1976-03-31
AU3299671A (en) 1973-03-08
NL144170B (en) 1974-12-16
DE2141106A1 (en) 1972-03-09
GB1353979A (en) 1974-05-22
NO130627C (en) 1975-01-15
FR2104921B1 (en) 1973-11-23
ES196796U (en) 1975-04-16
SE393934B (en) 1977-05-31
BR7105727D0 (en) 1973-04-26

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