JP6383901B1 - Energy-saving jet machine with horizontal fins - Google Patents

Abstract

When a jet aircraft flies at high altitude, it is possible to fly at an elevation angle of 3 degrees in order to maintain a predetermined height.
A horizontal fin 1 is attached to both sides of the nose, and the horizontal fin is interlocked with an auxiliary wing of a main wing. Thereby, since it is possible to fly stably at an elevation angle of 3 degrees in the high sky, an energy-saving jet machine can be obtained. In addition, because it is linked to the auxiliary wings of the main wing, the lift increases during takeoff and the brakes during landing. Therefore, the take-off and landing distance can be shortened, and the jet machine can be operated even on a short runway.
[Selection] Figure 1

Description

  The present invention relates to an energy-saving jet machine with a horizontal fin.

  When the jet plane flies in the high sky, it flies at an elevation angle of 3 degrees in order to maintain a predetermined height.

  This operation is performed with the main wing and horizontal tail wing, but the nose of the jet aircraft is considerably away from the main wing, in other words, the nose is protruding from the main wing, so that the nose moves up and down. The current situation is that accurate elevation flight is not possible.

  Therefore, manual operation must be corrected manually and automatically in automatic operation each time.

  It is an object of the present invention to make an energy-saving jet machine that eliminates the fluctuation of the nose of the nose and performs stable flight, eliminates unnecessary fuel consumption.

Means for Solving the Invention

  1 and 2 of the first embodiment of the present invention are obtained by attaching lateral fins at an elevation angle of 3 degrees on both sides of the nose of the jet machine.

  3 to 5 of the second embodiment, a horizontal shaft is passed from inside the nose to both outsides of the nose, and a horizontal fin is attached to the horizontal shaft at an elevation angle of 3 degrees, and both sides inside the horizontal shaft can be rotated by bearings. And mount the lever upward in the middle of both bearings. Also, set up the receiving bracket in the lever direction, install a screw jack between the upper end of the lever and the receiving bracket, and install the horizontal fin on the auxiliary wing of the main wing. It is designed to operate in conjunction with. In addition, you may operate independently instead of interlocking.

  In addition, although this invention attached the screw jack, you may attach another type.

Effect of the invention

In FIG. 1 and FIG. 2 of the first embodiment, the nose does not shake during the flight because the side fins are attached to both sides of the nose to increase the lift of the nose.
Further, in high altitude flight, when the main wing and tail wing auxiliary wings are set to an elevation angle of 3 degrees, an elevation angle of 3 degrees lateral fin is also added, so that the elevation angle effect extends to the entire aircraft.
Therefore, stable flight can be achieved and subtle shaking during flight can be suppressed.

In FIGS. 3 to 5 of the second embodiment, the horizontal fin is operated in conjunction with the auxiliary wing of the main wing, so that not only the flight effect of the elevation angle of 3 ° but also the elevation angle becomes large at the time of taking off and landing. When taking off, the lift increases, and when landing, it becomes a brake.
Therefore, the take-off and landing distance can be shortened from now, and the jet machine can be operated even on a short runway.

As described above, if the present invention is carried out, it effectively works not only in flight but also in takeoff and landing, so that an energy-saving jet machine with reduced fuel consumption can be obtained.
Further, the present invention can be implemented not only for a large size but also for a small-sized jet machine.

Example 1
Front view of Example 1 Plan view of FIG. Example 2
Front view of horizontal fin Plan view of FIG. A direction view of FIG.

  1 of FIG. 1 and FIG. 2 of Example 1 are horizontal fins attached to both sides of the nose and are attached at an elevation angle of 3 degrees.

In FIG. 3 to FIG. 5 of the second embodiment, reference numeral 2 denotes a horizontal shaft that passes from inside the nose to both sides of the nose. A horizontal fin 1 is attached to the horizontal shaft 2 at an elevation angle of 3 degrees. Further, both sides inside the horizontal shaft 2 are bearings 3 that rotatably support the horizontal shaft 2, a lever 4 is mounted upward in the middle of both bearings 3, and a metal fitting 5 is erected in the direction of the lever 4. ing.
Thus, the screw jack 6 is attached between the upper end of the lever 4 and the receiving bracket 5.

  In the figure, reference numeral 7 denotes a horizontal fin fixing rod for firmly fixing the horizontal fin 1, which is made of stainless steel that does not rust. 1 and 3 may be attached with an elevation angle of 0 °.

1 Horizontal fin 4 Lever 7 Horizontal fin fixing rod 2 Horizontal shaft 5 Bracket 3 Bearing 6 Screw jack

Claims (2)

An energy-saving jet with a horizontal fin that is mounted on both sides of the nose of the jet so that it can be raised and lowered. A horizontal axis is passed from inside the nose of the jet to both sides of the nose, and the horizontal fin is at an elevation angle of 3 degrees. Mounted on the both sides of the horizontal shaft with bearings so that it can rotate freely. At the middle of both bearings, the lever is mounted upward. Also, the receiving bracket is erected in the direction of the lever. An energy-saving jet with a horizontal fin, characterized in that a screw jack is installed in between and the horizontal fin is operated in conjunction with the auxiliary wing of the main wing. 2. The energy-saving jet with a horizontal fin according to claim 1, wherein the horizontal fin is operated independently .

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