RU189728U1 - A block of several aircraft with a starting engine in a transport and launch container - Google Patents

Abstract

A block of several aircraft with a starting engine in a transport-launch container is made detachable from the carrier, contains an aircraft fixation device in it, made in the form of clamps and guide elements, the starting propulsion system made in the form of a starting engine fixed to the rear of the devices, node breeding aircraft, located in the front of the unit and associated with the power farm.

Description

The invention relates to aviation and rocket technology, to unmanned aerial vehicles and devices for their launch.

The prototype is missing.

The transport and launch container in which the block of aircraft is placed is made detachable from the carrier, the starting propulsion system is designed as a starting engine fixed to a power farm located in the rear part of the block of aircraft, the aircraft are fixed into the block with the help of rods fixed to the power farm, on the outer surface of the rods there are sliders, and on the inner surface of the rods there are attachment points for aircraft. In this case, the slide blocks enter the guides on the transport-launch container and are fixed to them by pyro-locking devices, and the attachment points for aircraft on the rods are fixed with mating parts of the nodes on the aircraft by pyro-necking devices. On the front part of the rods there are opening brake flaps, which have visors in the front portion in the form of bent flaps. The aircraft unit has an aircraft dilution unit located in the front of the unit and connected, for example, with a rope to a power farm.

Due to this, the following technical result is achieved - increasing the reliability and efficiency of using the aircraft unit, and reducing the mass of the structure as a whole.

The proposed technical solution can be used in military equipment for unmanned aerial vehicles with accelerating detachable compartments installed on various types of carriers.

The composition of the block of three aircraft with a starting engine in the transport and launch container is shown in FIG. 1 ... 6.

FIG. 1 shows a block of three aircraft pos. 1 with folded wings and tail, power farm pos. 2, barbells pos. 3 and the starting engine pos. 4. The unit is located in the transport and launch container pos. 5, with dumping fairing pos. 6 and the back cover pos. 7

FIG. 2 shows a cross-section A-A along the block of aircraft pos. 1 in the transport and launch container pos. 5. The slit shows the sliders pos. 8 on the transport and launch container, sliders pos. 9 on aircraft, sliders pos. 10 on the rod pos. 3, guides for them pos. 11 in the container, pyrofippers pos. 12 for sliders pos. 9 on aircraft and pyrofippers pos. 13 for sliders pos. 10 on the rods, the node breeding aircraft pos. 14.

FIG. 3 shows a block of three aircraft pos. 1 after exiting the transport and launch container in axonometric projection with the starting engine pos. 4, with the node breeding aircraft pos. 14 aircraft pos. 1, brake flaps pos. 15 and the front and rear sliders pos. 10 on the rod pos. 3

FIG. 4 shows the hinge fastening power farm pos. 2. with the rod pos. 3

FIG. 5 shows the brake flap pos. 15 with a visor pos. 16, front slider pos. 10 and pyrofixer pos. 12 rod mounting points pos. 3 and the aircraft pos. one.

FIG. 6 shows the node breeding poses. 14 aircraft pos. 1 and rope pos. 17 communication breeding site with the power plate pos. 2

The device works as follows.

In the initial state, the three aircraft are fixed in the block pos. 1 using the rod pos. 3 and sliders pos. 9, secured to the rod pyrofikatoryami poses. 12. Bars Pos. 3 sliders pos. 10 are included in the guide poses. 11 on the transport and launch container pos. 5 and secured to him pyrofiksami poses. 13. Bars Pos. 3 are attached by hinges to the power farm pos. 2, to which the starting engine pos. 4. The aircraft unit with the starting engine in the transport and launch container is placed in the launch device of the carrier and attached to it with the help of sliders pos. eight.

When using this system, the unit of aircraft with the starting engine in the transport and launch container from the launch device of the carrier is ejected first. Then the starting engine turns on, the pyro-fixers pos. 13 and the block of aircraft with rods pos. 3, power farm pos. 2 and the starting engine pos. 4 exits the transport and launch container pos. 5 (see Fig. 2 and Fig. 3).

After the exit of the aircraft unit from the transport and launch container, the pyro-fixers pos. 12, the rod pos. 3 are exempt from mounting with sliders pos. 9 aircraft. As the block accelerates, the force of aerodynamic drag (velocity head) increases, affecting the visors of pos. 16 brake plates pos. 15, under the action of this force, the brake flaps open. The force of aerodynamic drag increases, which leads to the rotation of the poses pos. 3 relative to the axis of the hinge rod mounting to the power farm pos. 2. Next comes the gathering of the “bar-power farm-starting engine” system from the aircraft unit. In the process of this gathering, the longitudinal movement receives the node breeding poses. 14, connected by a rope 17 (see Fig. 6) with power farm pos. 2. There is a fan turn of the aircraft, which ensures the safe folding of the wings and feathers and the beginning of the autonomous flight of the aircraft.

Claims (1)

A block of aircraft with a starting engine in a transport-launch container, characterized by the fact that the aircraft are fixed into the block using a power farm and rods hinged to the power farm, on the outer surface of the rods there are slide blocks, and on the inner surface of the rods there are attachment points for adjacent aircraft, including a breeding unit with a rope connected to a power farm, sliders enter the guides on the transport and launch container and are secured to them with pyrofixers, and Ia aircrafts on rods fixed with mates nodes on aircraft pirofiksatorami, wherein the starter motor is secured to the back of the block aircraft and transport and launch container is configured to separate from the carrier.

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