DE102018005177A1 - Common computer program for the optimal use of multiple turbine forces for all gravity helicopter flight maneuvers - Google Patents

Abstract

Common computer program for the optimal operational use of several turbine forces for all gravity helicopter flight maneuvers, whereby it is provided that all turbine forces of the gravity helicopter (SKHS) can be fully used in all flight maneuvers, whereby a first rotor turbine drive and a second large turbine plant (GTW) are provided, whereby a GTW is provided , which has an acceptable weight and construction, has strong forces and can be inserted vertically into the SKHS fuselage, the vertical GTW position being provided as the base with a GTW swivel axis arranged between the two GTW broad sides and a GTW rotation angle, adjustable by computer application programs for GTW force assignments for GTW shares in the SKHS forward movement if GTW-SKHS forces can be diverted by the SKHS lifting process, whereby jointly calculated Be for the equipment of the computer program (CP) with effective operating instructions drive inserts are provided, whereby an entire aircraft wing structure is rotatably mounted, is provided on the SKHS underbody in the longitudinal direction of the SKHS, in order to reach a flight active position with a 90 degree rotation by means of a CP operation command, CFRP material use being provided primarily

Description

introduction

The category of horizontally flying aircraft has some properties that cannot be achieved by the category of helicopters. The helicopters have other advantages.

> It is therefore understandable that attempts have been made repeatedly, e.g. to introduce so-called combination aircraft screwdrivers.

These have e.g. to the rotor engines also short wings. Their properties have changed somewhat compared to those of the usual helicopters. However, such requirements were not adopted for practical use.

> Double rotors one above the other are also known.

This concept also found no entry for mass production.

> Another variation are so-called flight screwdrivers. For this purpose, the rotor blades are provided on a high engine tower and, in this concept, short wings on the fuselage with horizontally aligned engines. This elaborate and complicated construction also has no access to the production of series production.

> A similar variation are so-called convertible helicopters. For this, e.g. provided to completely switch off the rotor motor for horizontal flight. From a physical point of view, however, this concept is not effective enough and will probably not find a strong entry into the industry, although at times relatively high values for the speed are reached.

The task of the new development is a concept in which, from a physical point of view, all the engines used are permanently fully used for the flight. Claim 1 describes the solution with the solution ..

function Description

Common computer program for the optimal use of multiple turbine forces for all gravity helicopter flight maneuvers

A common computer program of several turbine forces is to ensure that all turbine forces of the gravity helicopter are optimally used in all helicopter flight maneuvers.

A first rotor-turbine drive and a second large turbine plant (GTW) are planned.

Such a GTW of a turbine manufacturer, which is provided as standard for the horizontal flight of passenger aircraft, is provided. to modify. A GTW is envisaged that has an acceptable weight and design and has strong forces to be inserted vertically into the helicopter fuselage.

Such a vertically used GTW is intended on the one hand for large lifting forces of the newly developed gravity helicopter.

On the other hand, a swivel axis between the two broad sides of the gravity helicopter is provided for this GTW.

This pivot axis is provided so that the task of the GTW can be angularly adjusted from the vertical position according to the program according to computer instructions via this pivot axis.

In this way, an additional force contribution can be used for the forward movement of the gravity helicopter when the GTW lifting forces are no longer required.

With maximum force requirements of the gravity helicopter, no matter what maneuver, all forces of the rotor-turbine drive and the GTW can always be used,

Should the computer program also request further use of the entire aircraft wing construction for a flight situation, this component would move out of the longitudinal storage position on the underbody of the gravity helicopter by 90 degrees.

The same scheme can be used for e.g. a gravity helicopter with e.g. a total of two rotor turbine drives and two GTWs.

Claims (2)

Common computer program for the optimal operational use of several turbine forces for all gravity helicopter flight maneuvers, it being provided that all turbine forces of the gravity helicopter (SKHS) can be used fully in all flight maneuvers, a first rotor turbine drive and a second large turbine plant (GTW) being provided, one GTW being provided is provided, which has an acceptable weight and an acceptable design, has strong forces and can be inserted vertically into the SKHS fuselage, the vertical GTW position being provided as a base with a GTW swivel axis arranged between the two broad GTW sides and a GTW rotation angle provided, adjustable by computer application programs for GTW force assignments for GTW shares in the SKHS forward movement, if GTW-SKHS forces can be diverted by the SKHS lifting process, for which the computer program (CP) is equipped with effective operating instructions, calculated operating operations are provided, with an overall aircraft wing structure being rotatably mounted on SKHS sub-floor is provided in the longitudinal direction of the SKHS in order to reach the active flight position with a 90 degree rotation by means of a CP operational command, CFRP material use being provided primarily Common computer program for the optimal use of several turbine forces for all gravity helicopter maneuvers, the same scheme as in patent 1 is provided for a total of two rotor turbine drives and two GTWs for a gravity helicopter