RU26515U1 - EASY AGRICULTURAL PLANE - Google Patents

Abstract

1. A light double-girder airplane of a one-and-a-half-winged scheme with a pushing propeller installation located in the fuselage, having a direct lateral force control system and parachute rescue system developed according to JAR-VLA standards, characterized in that the detachable parts of the lower wing and tail feathers are made by winding glass (carbon) thread, while the tail and controls are made by laying out the glass (carbon) with fabric material, and the fuselage and center wing of the upper wing are made of aluminum mini alloys using the plazo-template method, while the sealed fuel center tank is placed in the center section. 2. The aircraft according to claim 1, characterized in that the manufacturing technology of the lower wing and the detachable part of the upper wing, made by winding glass (carbon) with a thread, includes a separate winding of the bow, central and tail caissons in the form of a three-layer structure with an intermediate honeycomb followed by by connecting them with a winding glass (coal) thread in order to obtain a single wing structure. 3. The aircraft according to claim 1, characterized in that, in order to ensure the safety of personnel, the tail beams are installed above the wing and are raised to a height that provides free passage under them. Aircraft according to claim 1, characterized in that for the two-stroke engine mounted on the aircraft, a special resonant exhaust section is provided, which provides an increase in engine power by about 5% in take-off mode.

Description

The invention relates to aircraft, in particular to the design of aircraft.

I test different types and types of light aircraft designed to solve a wide variety of problems, including to perform agricultural work.

The proposed light agricultural aircraft with a slight increase in the safety of work under sexual conditions is a highly tail feathering beam on the lower surface of the upper wing, while the aircraft glider is made using a mixed metal-composite technology, which increases its protection against aggressive chemicals and often weighs less aerodynamic characteristics

All the upper parts of the upper wing and tail beams are made by winding glass (carbon) with thread, while the tail and controls are made by laying out stem (gle) fabric material, and the fuselage and center wing of the upper wing are made of aluminum alloys using the plasma-pattern method; in the center section there is a sealed fuel tank.

The manufacturing technology of the lower wing and the detachable part of the upper wing, made by winding stsklo (corner) drink, includes separate winding of the nasal central and tail caissons in the form of a three-layer structure (fiberglass-honeycomb-fiberglass) with subsequent winding of the glass (corner) with a thread for a single wing-like structure.

In order to increase the power of a two-stroke engine in the take-off mode installed on an airplane, a special resonant exhaust section is provided.

The structural diagram of a light agricultural aircraft is shown in Figure 1., where: 1 - the fuselage;

2-composition upper wings;

3-tail feathering;

4-removable lower wings;

5-plumage;

6-chassis.

no author would have thought to climb, and where only one customs official is allowed to climb. The inspector must have sufficient grounds for a personal search, and the head of customs or his deputy can resolve it. For some time, this sanction must be executed in writing. The alleged intruder is examined in a separate room in the presence of two witnesses. If they inspect a woman, then the customs officer and the witnesses are also women. At the end of the procedure, an appropriate act is drawn up, which the inspected must sign, but it is not issued to the hands.

If money or items illegally transported are discovered, then a protocol on violation of customs rules is compiled. The offender can be blamed for forging documents (for example, bank authorization), not declaring the transport of currency or goods (unless they are specially hidden) and, finally, concealing (in the case of using special devices such as a double bottom, etc.).

According to statistics, 99% of violation protocols are completely justified. In case of an administrative violation, smuggled items are confiscated. Violators can be fined between 100 and 300% of the customs value of the goods. In this case, the special decision must be made by the head of customs or his deputy. However, as a rule, fines are not immediately levied on our violators, they can even be released abroad with an indication of the time for the appearance in law enforcement agencies (usually up to ten days).

When trying to illegally transport any items on an especially large scale (from two hundred minimum wages), or drugs or weapons, a criminal offense is drawn up. The fate of the unsuccessful smuggler will determine the most humane court in the world.

OUR NEEDS GROW. FROM FLIGHT TO FLIGHT.

Claims (4)

1. A light double-girder airplane of a one-and-a-half-winged scheme with a pushing propeller installation located in the fuselage, having a direct lateral force control system and parachute rescue system developed according to JAR-VLA standards, characterized in that the detachable parts of the lower wing and tail feathers are made by winding glass (carbon) thread, while the tail and controls are made by laying out the glass (carbon) with fabric material, and the fuselage and center wing of the upper wing are made of aluminum mini alloys using the plazo-template method, while the sealed fuel center tank is placed in the center section.  2. The aircraft according to claim 1, characterized in that the manufacturing technology of the lower wing and the detachable part of the upper wing, made by winding glass (carbon) with a thread, includes separate winding of the bow, central and tail caissons in the form of a three-layer structure with an intermediate honeycomb core followed by connecting them with a winding glass (coal) thread in order to obtain a single wing structure.  3. The aircraft according to claim 1, characterized in that, in order to ensure the safety of personnel, the tail beams are installed above the wing and are raised to a height that provides free passage under them. 4. Aircraft according to claim 1, characterized in that for the two-stroke engine mounted on the aircraft, a special resonant exhaust section is provided, which provides an increase in engine power by about 5% in take-off mode.