RO89910B1 - Aviation fire bomb - Google Patents

Aviation fire bomb

Info

Publication number
RO89910B1
RO89910B1 RO116065A RO11606584A RO89910B1 RO 89910 B1 RO89910 B1 RO 89910B1 RO 116065 A RO116065 A RO 116065A RO 11606584 A RO11606584 A RO 11606584A RO 89910 B1 RO89910 B1 RO 89910B1
Authority
RO
Romania
Prior art keywords
bomb
incendiary
cap
metallic container
ogivale
Prior art date
Application number
RO116065A
Other languages
Romanian (ro)
Inventor
Adrian Neagu
Original Assignee
Institutul National Pentru Creatie Stiintifica Si Tehnica
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 Institutul National Pentru Creatie Stiintifica Si Tehnica filed Critical Institutul National Pentru Creatie Stiintifica Si Tehnica
Priority to RO116065A priority Critical patent/RO89910B1/en
Publication of RO89910B1 publication Critical patent/RO89910B1/en

Links

Landscapes

  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)

Abstract

Inventia se refera la o bomba incendiara de aviatie, destinata distrugerii, prin incendiere, a tintelor terestre, amplasate cu relief variat. Bomba incendiara, conform inventiei, este constituita dintr-un corp format dintr-un tronson cilindric tubular si o calota ogivala, asamblate într-un tot unitar, corpul bombei fiind prevazut, la partea sa superioara, cu un dispozitiv aspersor si un ampenaj stabilizator, la partea sa mediana, cu niste inele de acrosare si niste aripioare limitatoare de patrundere, în zona calotei sale ogivale, fiind dispuse niste aripioare de frânare, iar în partea sa inferioara, un con de patrundere, pe care sunt montate doua microîntrerupatoare electrice conectate la un bloc electronic de comanda, situat în interiorul calotei ogivale, la care sunt, de asemenea, conectate: un înclinometru, un generator de impulsuri, un acumulator electric si un microîntrerupator dispus pe suprafata exterioara a corpului bombei, interiorul tronsonului cilindric al acestuia adapostind un recipient metalic conectat la dispozitivul aspersor prin intermediul unui tub si, respectiv, al unei valve dublu-sens comandata electric cu ajutorul blocului electronic de comanda, în interiorul recipientului metalic aflându-se un lichid incendiar mentinut sub presiune cu ajutorul unei perne gazoase, lichidul incendiar fiind dispersat în spatiul înconjurator în momentul impactului bombei cusolul, iar pe partea inferioara a aceluiasi recipient metalic, fiind dispusa o încarcatura exploziva de siguranta.The invention relates to an incendiary aviation bomb destined to the destruction by fire of terrestrial targets with varied relief. According to the invention, the incendiary bomb consists of a body formed by a cylindrical tubular section and an ogival cap, assembled in a unitary manner, the body of the bomb being provided, at its upper part, with a sprinkler device and a stabilizing amperage, at its median side, with some stitching rings and some limiting flaps of penetration, in the area of its ogivale cap, some braking fins are arranged, and in its lower part a penetration cone, on which are mounted two electrical micro switches connected to an electronic control block located within the ogivale cap, to which are also connected: an inclinometer, a pulse generator, an electric accumulator and a microswitch arranged on the outer surface of the body of the bomb, the interior of the cylindrical section thereof accommodating a a metallic container connected to the sprinkler device by means of a tube and, respectively, of a double-sided valve by means of an electronic control unit, inside the metallic container there is an incendiary liquid maintained under pressure by means of a gas pillow, the incendiary liquid being dispersed in the surrounding space at the moment of impact of the cusp, and on the lower part of the same metallic container, an explosive charge of safety being dispensed.

RO116065A 1984-10-23 1984-10-23 Aviation fire bomb RO89910B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RO116065A RO89910B1 (en) 1984-10-23 1984-10-23 Aviation fire bomb

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RO116065A RO89910B1 (en) 1984-10-23 1984-10-23 Aviation fire bomb

Publications (1)

Publication Number Publication Date
RO89910B1 true RO89910B1 (en) 2002-06-28

Family

ID=40904034

Family Applications (1)

Application Number Title Priority Date Filing Date
RO116065A RO89910B1 (en) 1984-10-23 1984-10-23 Aviation fire bomb

Country Status (1)

Country Link
RO (1) RO89910B1 (en)

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