DE2117145C3 - Missile carrier - Google Patents

Description

3 4

Dimensionally stable material, for example a light fertilizer, compacted layers are produced. the

metal tube, molded in. The tube 2 extends manufacture of the missile carrier is carried out so

over the entire body up to the vicinity of the front that you can put the polyurethane in a closed shape

the end and forms a central cylindrical guide and hardens, whereby previously in the mold the

tion for a rocket projectile 3, the tube 2 forming the middle guide in this tube 5, the anchoring

used and fired from this tube are approximately wall 5, the rods 4 and additional cores for

can. Furthermore, a plurality of the guides arranged in a ring are correctly positioned in the foam

of arms 4, which were used in the illustrated embodiment. After the body has hardened

form of round rods that is with, it is taken out of the mold. After one

Screws on an anchoring wall 5 from lightweight »o has removed the cores, the wall 7 is attached.

metal are screwed on, with cast. The sticks and with the help of the screws 6 on the top

Wall 5 is rigidly attached to the top of the pipe 2 with the body.

stigt. The rods are arranged in pairs and with the openings in the front of the body The distance over a considerable length of the pipe is covered with a conical nose part 11, Splits. They are arranged in such a way that the rods »5 of the end of the of each pair is matched against each other upward in a body, with the exception of a tip which The radial plane of the body 1 diverges and protrudes beyond the central tube. The conical nose extend substantially radially of the tube. The disadvantage is made of fragile plastic that is in The ends of the arms 4 protruding from the top can be broken up with screws. Since the koben 6 on a wall 7 made of light metal an- ao nical nose part on the front end of the body screwed on, which is fitted to the top of the body, its wall is made very thin, and a suspension device 8 with suspension eyes so that the explosive forces and the explosive parts, which has, with which the missile carrier hangs on the aircraft when the missile projectiles hit the koni can be. The tube 2, the rods 4 and see the nose part emerge, the aircraft does not operate Wall 7, which can damage the top of the housing.

impacts, together form a frame, which is a rocket projectile carrier according to the invention

it is sufficiently rigid to withstand the weight and the forces of the air, so light and so cheap to manufacture that it can be manufactured

to be recorded on the carrier. can also be used for all floors that are

In addition to the central guide, which can be stored from the right places and transported there 2 is formed, the body 1 contains an animal. The projectiles are good compared to the number of cylindrical guides 9, which, if you ßere transport and storage damage, protected and form Cross-section of the body viewed, ring-shaped the weapon units complete with their carriers, are arranged around the central tube. The outer ones that can easily be attached to an airplane. Daren Guides are arranged so that one of the through that the carrier is cheap, he can also Throw away the outer pipes immediately above the central pipe 2 35, which is a major advantage because lies between two diverging rods 4. Offer great air resistance in the empty carrier In contrast to the central guide, the ring-shaped speed of the aircraft is reduced and arranged guides molded into the plastic, and the fuel consumption on the flight home also doubled Similar to the central guide, all are larger on the outside.

guides designed so that they are a ejectable 40 You can use the described and illustrated missile projectile 10 can accommodate. form of management within the scope of the following

In a preferred embodiment, there is a modification of the claims. For example, such

the foam made of fermentable polyurethane, modification is that instead of the

with which arms written in the area when casting the body for the frame construction

the guide walls and the outer wall of the body 45 forierte web plates are used.

1 sheet of drawings

Claims (2)

1 2 claims - a large diameter made of thin material "very sensitive to the hollow cylinder. 1. Missile projectile carrier for aircraft, wel- twisting. Not even the middle leadership rather from an elongated cast body torsion stiff with the suspension means of the Rakeper consists of porous plastic and is connected to the 5! Absorbing and ejecting rocket form practically all plastic fired a majority of themselves longitudinally- burdened by the weight of all the missiles in that device has extending guides, of which hollow cylinders. extends centrally through the body, while the object of the present invention is therefore, the others in a ring around the middle guide a cheap rocket suitable for throwing away. tion are arranged, and the one stiff long beam to create the one with low weight stretched out over the top of the body, showing great strength. has stretching wall, which is provided with means for solving this problem, the invention releasable suspension of the carrier on the aircraft would have missile carrier characterized in that is provided, characterized in that 15 a rigid tube forming the central guide that a central guide forming rigid arms extending radially upward with the Tube (2) with a radially upwardly extending wall rigid to a stiff, the weight and the Arms (4) are rigidly connected to the wall (7) to form a frame that absorbs stiff air forces, to absorb the weight and the air forces - and that the additional guides arranged in a ring the frame are connected, and that the ring ao ments and the walls surrounding the body further guides (9) arranged in a shape and cast from the porous material, the the walls surrounding the body (1) from both arms on both sides of the the porous material are cast, with the NEN guide extending. two arms (4) on both sides of the above the tube (2) in this missile carrier according to the invention provided tour. 25 whose upper half by arms to which is about the 2. missile carrier according to claim 1, da- top of the body extending wall abgefandurch characterized in that the porous plastic gen. Only the weight of the in the lower half consists of fermentable polyurethane, loaded with the missile carrier lying rockets from the when molding the body (1) in the area finally the plastic. Trained that as leadership Guide walls and the outer center tube, which because of its small through wall densified layers have been produced. knife is very torsion-resistant, is on a Quarter of its surface is supported by the arms, so that the body of the missile carrier is otherwise gen can only be made from plastic, 35 without having to support its outer walls towards the above-mentioned upper longitudinal wall. Through this The invention relates to a missile projectile carrier, the missile carrier is very light in weight and for aircraft, which consists of an elongated one cheap to manufacture. cast body made of porous plastic and the known measure, a rocket to provide the 40 with a rigid jacket tube for receiving and ejecting rocket carriers and A plurality of them shot in the longitudinal direction of this over a plurality of radial partitions has extending guides, one of which can be connected to the central guide tube extends centrally through the body, while the other measure, the measure according to the invention, only one out Ren arranged in a ring around the central guide plastic existing rocket carrier with upwards are, and the one stiff elongated, supported by the 45 protruding arms, do not suggest. Having top of the body extending wall, According to a preferred embodiment of the the invention, the porous plastic consists of fermen- is provided on the aircraft. animalable polyurethane, with which when molding the. These previously known rocket projectile carriers need body in the area of the guide walls and the In order to reinforce the plastic, layers compressed around the body are created Telndes hollow cylinder piece made of expanded metal or the like. Have been. Since a chain holder consisting exclusively of plastic, further details of the invention are not able to absorb considerable chain weights from the following detailed description, ketenweeights and air forces. Because of the drawings, in which a preferred embodiment of this complex design, such reinforced forms of the invention are, for example, rocket projectile carriers expensive to manufacture, is shown. In the drawings shows
times they have a carefully manufactured hollow cylinder F i g. Fig. 1 need a side view of a missile sized cross-section, carefully applied to the carrier according to the invention, F i g extending over the top of the body. 2 shows a longitudinal section of FIG. 1 in enlarged ■ Wall and the 60 tem scale and made of reinforced plastic Layer needs to be aligned. In the case of a lack of F i g. 3 shows a cross section according to the cutting line Alignment would be the upper part of the hollow cylinder III-III of FIG. 2 on an even larger scale, otherwise not on a sufficiently large area and supported and there would be deformations and cracks elongated spindle-shaped body 1 of circular in the hollow cylinder jacket, which leads to the 65 migem cross-section being torn off. The body 1 tapers co- Missile carrier can lead if abruptly up- front. The body 1 is made in one piece Forces stepping in gusts of wind or when pushing a foam made. When making a individual missiles are to be expected. In addition, the central guide makes the tube 2 of a rigid one