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Flight system

A subsystem and empennage technology, applied in the field of flight systems, can solve problems such as low glide rate, inability to climb, lack of power and instant experience

Pending Publication Date: 2020-11-13
彼得于斯特尔
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, hang gliders / hang gliders cannot climb under their own power, instead they rely on exploiting updrafts or thermal lift to gain altitude, and similarly to gliders, have a significantly lower glide rate
In contrast, a glider that can cover considerable distances while gliding lacks the dynamics and instant feel that hang gliders and hang gliders typically have

Method used

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Embodiment Construction

[0026] Preferred non-exclusive exemplary embodiments of this patent are described below. Figure 1 to Figure 4 This preferred exemplary embodiment is shown schematically. Connecting elements, sensors, wiring and other details are not shown. exist image 3 and Figure 4 In , for clarity, this presentation is reduced to a preferred design of the skeleton structure of the half and the mechanical construction of the wing. Figure 5 A possible block diagram of a single system in the overall system is shown.

[0027] The flight system of this exemplary embodiment has an exoskeleton 1, a flapping wing device with two flapping wings 2, and an empennage 9 ( figure 1 ).

[0028]The exoskeleton 1 has an equipment backpack 11, a chest strap 12, a waist belt 13, a thigh cuff 14 for each thigh of the pilot (not shown here), and an upper arm cuff 15 for each arm of the pilot, a forearm cuff hoops 16 and gloves 17 and boots 18 for each foot of the pilot. Chest strap 12 and waist strap ...

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Abstract

The invention relates to a flight system having at least two actuated flapping wings (2), an actuated tail unit (9), a control device and an exoskeleton (1) for at least one person. The exoskeleton (1) is movable independently of the flapping wings (2). The control device is configured to receive motion sensor signals from the exoskeleton (1) and to use the motion sensor signals to define specified movement signals and to control the flapping wings (2) and / or the tail unit (9) by way of the specified movement signals. The specified movement signals can be defined such that the movements of theflapping wings (2) and / or of the tail unit (9) follow those of the exoskeleton (1).

Description

technical field [0001] The invention relates to a flight system with a driven flapping wing and a driven empennage. Background technique [0002] From DE-PS 652 170 a muscularly propellable glider is known, in which the wings moved by muscular power are connected to the fuselage by rubber cords, so that the strength of the pilot should be assisted, wherein the wings can be switched manually by The pawls are locked, and the aircraft is able to continue to function as a glider without power expenditure. [0003] From DE-PS 173 926 a flying machine with flapping wings is known, which can be actuated by the pilot's arm with the arm bent by means of a contour frame, wherein each elbow rests in the abutment, and each Each hand is gripped on a curved handle, the different gripping areas of the curved handle realizing different lever arms for driving the wings. [0004] A hover glider with motor-assisted wings is known from WO 2014 / 028083 A2. The wings can be manipulated and cont...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/00B64C39/02B64C31/04
CPCB64C31/04B64C33/00B64C39/026B64C9/00B64C13/04B64C33/025B64D27/16B64D43/00G06F3/14
Inventor 彼得·于斯特尔
Owner 彼得于斯特尔
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