A WING OPENING MECHANISM

Abstract

This invention comprises a fuselage (14) with a left and right wing (6, 7) that is initially closed and can be opened in a suitable position for flight according to user demand, a spacer (2) positioned on the fuselage (14), a vertical shaft (3) extending on the spacer (2), a lower center piece (4) on which the left wing (6) is positioned, an upper center piece (5) on which the right wing (7) is positioned, the lower and upper center pieces (4,5) are positioned on the vertical shaft (3) and a rising angled surface (41) that opens spirally onto the lower center piece (4) so ​​that they can move circularly in opposite directions along the central axis of the vertical shaft (3), and a descending angled surface (51) that opens onto the upper center piece (5) symmetrically to the rising angled surface (41).It includes a wing opening mechanism (1) characterized by a vertical spring (8) whose one end is attached to the intermediate piece (2) and the other end to the lower center piece (4), and which, by releasing its energy, causes the lower center piece (4) to move both linearly and circularly around the axis of the vertical shaft (3) along the vertical shaft (3), causing the descending and ascending angle surfaces (41, 51) to come into contact with each other, simultaneously moving the upper center piece (5). This wing opening mechanism (1) is structurally simple, enabling the left and right wings (6,7) to quickly transition from a closed position to an open position in the same vertical alignment, while the fuselage (14) moves synchronously with each other with respect to the symmetry axis, and when the left and right wings (6,7) are in the same vertical alignment, it can convert the aerodynamic lift force on the left wing (6) into a locking force that keeps the wings open, thus eliminating the need for an additional locking mechanism.

Description

1 TARIFF A WING OPENING MECHANISM Technical Area This invention improves the flight stability of aircraft and munitions with folding wings by 5. A wing opening mechanism that allows the wings to open synchronously without disrupting the flow. It is related to the mechanism. Previous Technique Unmanned aerial vehicles or winged vehicles carried by such aircraft ammunition, during transport, should not take up space or during the transport process 10 They are kept with their wings folded so that they do not experience any difficulties. (Word) the launching or release of munitions or aircraft Their wings are then spread open, allowing them to perform their flight tasks. In the known state of the art, the aircraft or munitions in question a folding mechanism to move the wings from closed to open position and 15 a lock to keep them in the desired positions (open or closed) The mechanisms are in place. In wing folding mechanisms found in the known state of the art, the wings, in configurations where they are folded side by side, on top of each other, or at certain angles It is observed that it is hidden. The wings are folded side by side, the wings are 20 flight dynamics because it maintains symmetry with respect to the symmetry axis of the fuselage to which it is attached. While this is beneficial in terms of surface area, for each wing, half of the usable wing surface area must be utilized. Since only that much space is available, providing the necessary wing surface area is a problem. This is possible. When the wings are folded on top of each other, the usable surface area increases. It allows the entire area to be used for each wing. However, this 25 This situation creates asymmetry with respect to the fuselage symmetry axis to which the wings are attached, and 2 This creates an undesirable situation in terms of flight stability. Wing Aerodynamic drag force caused by external airflow, This creates an effect that causes the wings to close. Therefore, wing folding. most of their systems have locking mechanisms that keep the wings open. These mechanisms are mostly based on the wings being brought to the open position. 5 They are spring-loaded pin-shaped structures that have a socket in a specific location. These structures serve both purposes. This increases both the complexity and the number of parts of the wing folding mechanism. The risk is that if it doesn't work, it could cause the wings to fold back. This is especially true in overlapping wing systems, where the wings overlap each other. Although it can move synchronously, its synchronous movement is limited to 10 degrees depending on the body it is attached to. This does not happen. This creates a problem in terms of flight stability. Brief Description of the Invention The purpose of this invention is to allow the wings to be folded on top of each other and, when unfolded, to remain in the same vertical position. a wing opening that allows it to be positioned symmetrically by reaching the level The mechanism is to implement it. 15 Another aim of this invention is to both increase the efficiency of usable space and... A wing span that increases flight stability with symmetrically deployed wings. The mechanism is to implement it. Another purpose of this invention is to regulate the airflow over the wing when the wings are opened. The use of the resulting aerodynamic lift force as a locking system 20 and to prevent the situation where the wings close again after they have opened. The goal is to create a wing opening mechanism that enables this. The invention concerns a wing-opening mechanism for aircraft and munitions. suitable for use, a left and right initially closed on a body. The wing and user requirements determine the appropriate flight position, left and right 25 There is an axis extending from the fuselage and a center that enables the wing to open. both circularly and linearly along the axis, with the axis being the center. It includes a movable lower center piece. On the lower center piece, left 3 The wing is positioned. An upper center piece is positioned on top of the lower center piece. It is positioned so that the upper center part center will be on the axis in question. It can move in a circular motion. A right wing is mounted on the upper central part. It is positioned so that the lower center part is both circular along the axis in question. and the energy required for it to move linearly is supplied by a vertical spring 5 It provides. The vertical arc in question will have its center point on the axis in question. positioned in this way, with one end attached to the body and the other end to the lower central part. It is in contact. Based on the energy provided by the vertical spring, the lower central part... The lower center allows for both linear and circular movement along the axis. a rising angle surface that opens spirally at an angle onto the piece, 10 an opening made on the upper central piece, symmetrical to the rising angle surface It includes a descending angle surface. The subject of the invention is a wing opening mechanism with a left wing opening mechanism. and the right wing can be folded over and unfolded to the same vertical level. Symmetrical positioning is ensured. The subject of the invention is a wing opening mechanism. The airflow and vertical arc formed on the right wing in the mechanism 15 With the force it has generated, the right wing will not return to its starting position and It is ensured that it remains in the open position. Detailed Description of the Invention A wing-opening mechanism has been added to achieve the purpose of this invention. as shown in the figures, and of these figures; 20 Figure 1 - The wing opening mechanism of the invention in the open state of the wings. It is a perspective view. Figure 2 - The wing opening mechanism of the invention in the closed state of the wings. It is a perspective view. Figure 3 - The wing opening mechanism of the invention, with the wings in the open position, is 25 It is an exploded perspective view. Figure 4 - Cross-sectional view of the wing opening mechanism subject to the invention. Figure 5 - Cross-sectional view of the wing opening mechanism of the invention. 4 The parts in the figures are individually numbered, and each number corresponds to the following: It is given below. 1. Wing opening mechanism 2. Spacer 3. Vertical Shaft 5 4. Lower center piece 41. Ascending angle surface 5. Upper center piece 51. Descending angle surface 6. Left wing 10 7. Right wing 8. Vertical arc 9. Moving parts 10. Horizontal arc 11. First column 15 12. Second arm 13. Horizontal Shaft 14. Body A fuselage (14) suitable for use with aircraft and munitions. on which there is a left and right wing (6, 7) which is initially closed and user request 20 opening the left and right wings (6, 7) in the appropriate position for flight in line with a wing opening mechanism (1); - an axis extending from the body (14), with the centre being the said extension capable of moving both circularly and linearly along the axis a lower center piece (4) and 25 positioned on the lower center piece (4) left wing (6), - located on the lower center part (4), the center of the said axis an upper center piece (5) that can move in a circular manner and a right wing (7) positioned on the upper center piece (5), - the lower center part (4) is both circular along the axis in question. lower center to move linearly through a vertical spring (8) a rising that opens at an angle in a spiral manner onto the piece (4) The angled surface (41) will be symmetrical to the rising angled surface (41) on top It includes a descending angle face (51) that opens onto the central part (5). 5 The subject of the invention is a wing opening mechanism (1), for aircraft and munitions. suitable for use, a left and initially closed body (14) right wing (6, 7) and left wing in a suitable position for flight according to user request and an axis extending from the fuselage (14) that enables the opening of the right wing (6, 7) and With the axis in question as its center, it will be both circular and along the axis, 10 It includes a lower center piece (4) that can move linearly. Lower center The left wing (6) is positioned on part (4). On the lower center part (4) An upper center piece (5) is positioned. The upper center piece (5) is the center word. It can move circularly with the subject as its axis. Upper center A right wing (7) is positioned on part (5). The lower center part (4) is mentioned in 15 so that it can move both circularly and linearly along its axis The necessary energy is provided by a vertical spring (8). The vertical spring (8) in question is the center The point is positioned such that the axis in question will be the axis and one end is attached to the body (14) The other end touches the lower center part (4). Provided by the vertical spring (8) In relation to energy, the lower center part (4) is both linear and 20 along the axis. In order for it to move in a circular motion, spirally on the lower center piece (4) There is a rising angle surface (41) that opens at an angle. Rising A descending on the upper central piece (5) will be symmetrical to the angled surface (41) An angled surface (51) has been opened. Initially positioned one on top of the other, the left and right k nat (6, 7), and one end of the body (14) 25 a vertical spring (8) is stuck on it and the other end of it touches the lower center part (4) is in position. By releasing the vertical spring (8), in other words the axis When you apply a force linearly along the lower center part (4), the lower center part (4) moves linearly along the axis rising angle surface (41), It contacts the descending angle surface (51). Rising and descending angle surfaces (41, 30 6 51) thanks to their angular structures, the lower center part around the axis (4) Turning to the left causes the upper center piece (5) to rotate to the right. Lower center With the turning of part (4) to the left, the left wing (6) opens and the upper center part (5) By turning to the right, the right wing (7) is opened. The subject of the invention is a wing opening. With its mechanism (1), the left and right wings (6, 7) can be folded on top of each other and 5 When opened, it comes to the same vertical level and is positioned symmetrically. is provided. The subject of the invention is the right wing opening mechanism (1) located in a wing opening mechanism. the airflow created on the wing (7) and the force provided by the vertical spring (8) with the right wing (7) will not return to the starting position and will be in the open position It is ensured that it remains there. 10 The subject of the invention is a wing opening mechanism (1), for aircraft and munitions. a left and right wing (6, 7) which are suitable for use and are initially closed. left and right wings (6, 7) in suitable position for flight according to user request It includes a body (14) for opening. In one application of the invention, the body (14) an intermediate piece (2) positioned on it and 15 extending on this intermediate piece (2) A vertical shaft (3) is located. A lower center piece (4) is placed on the vertical shaft (3) It is positioned. The lower center piece (4) will be the vertical shaft (3) on the center axis. In the figure, it moves both circularly and linearly along the vertical shaft (3). It is able to do so. The left wing (6) is positioned on the lower center piece (4). Lower a top 20 on the center part (4) and with the center axis being the vertical shaft (3). The center piece (5) is positioned. The spacer (2) connects the upper center piece (5), both holding on the lower center part (4) and circular around the vertical y shaft (3). It contributes to its movement as follows: Right wing on the upper center piece (5) (7) is positioned. The upper center piece (5) will be the vertical shaft (3) on the center axis. It can move in a circular manner. The lower and upper center parts (4,5) 25 The lower and upper center parts (4,5) have vertical shafts to allow them to move in a controlled manner. (3) is positioned on and along the central axis of the vertical shaft (3) lower center piece (4) so ​​that they can move circularly in opposite directions a rising angle surface that opens up in a spiral shape (41), rising A symmetrical lower n 30 opening onto the upper central piece (5) on the angled surface (41). 7 An angled surface (51) is located. One end is connected to the intermediate piece (2) and the other end is connected to the lower center. connected to part (4) and releasing its energy, the lower center part (4), along the vertical shaft (3) both linearly and around the axis of the vertical shaft (3). By enabling circular motion of descending and ascending angle surfaces (41, 51) moving the upper center piece (5) simultaneously by contacting each other. It contains a vertical spring (8). The vertical spring (8) applies to the lower center part (4). linear force, by contact of descending and ascending angle surfaces (41, 51), The lower and upper center parts (4,5) will be symmetrical to each other and the vertical shaft (3) opening the left and right wings (6, 7) by moving in a circular motion around it It provides. As a result, the left and right wings (6, 7) initially overlap by 10 It has a compact structure that takes up little space. It features descending and ascending angles. both circular motion and linear motion provided by the surfaces (41, 51) When the left and right wings (6, 7) are opened, they come to the same vertical level, becoming symmetrical. Positioning is ensured. Initially, the left and right wings (6, 7) were positioned to overlap, the same 15 In the figure, the lower and upper central parts (4, 5) to which the left and right wings (6,7) are attached stacked on top of each other on vertical shafts (3) that are symmetrical to each other It is positioned. Opened on the lower and upper center parts (4, 5) The descending and ascending angle surfaces (41, 51) are symmetrical so that they face each other. They are positioned as follows. In other words, they will be symmetrical with respect to each other. a spiral and angled surface positioned in such a way as to descend and ascend angles The surfaces (41, 51) are positioned so that they fit together opposite each other and the word The surfaces in question (41, 51) are in contact with each other. At the starting point, that is By positioning the left and right wings (6, 7) on top of each other, the bottom and top The distance between the center parts (4, 5) on the vertical shaft (3) axis is greater. Same 25 In the figure, the vertical part initially attached to the lower center part (4) and the intermediate part (2) The spring (8) is compressed, i.e., in a high-energy state. The vertical spring (8) has the energy of the user releasing the vertical spring (8). With the energy it has, the lower center part (4) around the vertical shaft (3) is circular. It moves both linearly and vertically along the shaft (3). Bottom 30 8 the central part (4) is circular around the vertical shaft (3) and also around the vertical shaft (3) The left side, connected to the lower center part (4), moves linearly along its length. The wing (6) opens by both rising and moving in a circular motion. Bottom the central part (4) is circular around the vertical shaft (3) and also around the vertical shaft (3) 5 is located on the lower center part (4) by moving linearly along its length. The area rises and moves circularly on the rising angle surface (41). It is in contact with the rising angle surface (41) and the said rising angle surface (41) has a descending angle surface (51) which is symmetrical. Circular around the vertical shaft (3) in the upper center part (5) but lower center It moves in opposite directions according to part (4). The vertical shaft of the upper center part (5) 10 (3) made circular around the lower center piece (4) in the opposite direction. The upper wing (7) which is connected to the upper central part (5) with movement, moves circularly. It opens by doing so. In one application of the invention, the left and right wings (6,7) are symmetrical to each other and 15 on the body (14) to open by moving synchronously a linearly moving along a positioned horizontal shaft (13) movable part (9), one end to the body (14) and the other end to the movable part (9) a horizontal spring (10) attached, one end to the movable part (9) and the other end to the intermediate part (2) a first arm (11) attached, one end to the movable part (9) the other end to the top It includes a second arm (12) connected to the central part (5). Lower and upper center 20 part (4,5) circular around the vertical shaft (3) opposite each other with the movement it makes, the first arm, one end of which is positioned on the intermediate piece (2) (11) and the second arm, one end of which is positioned on the upper central piece (5) (12) the movable part (9) located at the other ends, horizontal shaft (13) It moves linearly along its length. However, Horizontal publication (10) 25 by releasing the energy on it, the moving part (9) moves linearly. Applying force to make it work also contributes to the linear motion of the moving part (9). It provides. The horizontal of the movable part (9) connected to the first and second arms (11,12). The linear motion of the shaft (13) along the axis of the first and second arms (11,12) connected spacer (2), sub-center piece (4) connected to spacer (2), sub-center 30 9 left wing (6) and upper center piece (5) and upper center piece (4) attached to the part (4) (5) the right wing (7) which is connected to each other will be synchronous and symmetrical It allows for movement. In one application of the invention, the left and right wings (6, 7) are switched from the closed position to the open position. The transition to this situation is applied to the aforementioned wing opening mechanism (1) 5 This occurs symmetrically with respect to the aircraft's axis of symmetry, i.e., left and The right wing (6,7) opens symmetrically. More specifically, the right wing (7) When the aircraft is at a certain angle to the axis of symmetry, the left wing (6) is also at the same angle. This situation occurs when the left and right wings (6,7) switch from the closed position to the open position. It occurs at all angles. This movement synchronization, body (14) 10 horizontal shaft (13) integrated on it and linearly on the horizontal shaft (13) This is provided by the movable part (9). The movable part (9) is connected to it. the first and second arms (11,12), the intermediate piece (2) to which they are connected, the lower and upper centers by making the part (4,5) move in opposite directions around the vertical shaft (3) to the left and allows the right wing (6,7) to move symmetrically and at the same angle. 15 It provides. More details are located on the lower and upper center parts (4,5). The area is limited by the vertical direction of the descending and ascending angle surfaces (41,51) with each other. This ensures that the same cyclical movement is performed without the upper center. right wing (7) attached to part (5) and left wing (6) attached to lower center part (4) The vehicle moves symmetrically with respect to the axis of symmetry. The left and right wings (6,7) 20 circular motion of the movable part (9) to which the first and second arms (11,12) are attached Moving linearly along the horizontal shaft (13), the movable part (9) horizontal The process stops and is limited when the shaft reaches its endpoint. However, the contact surface geometry of the lower and upper center parts (4,5) is descending and ascending angle surfaces (41,51) rotation of these two parts relative to each other 25 It is ending its movement. The cross-section profiles of the left and right wings (6,7) are aerodynamically accurate in flight. It is designed to generate lift force. The right wing (7) is in the vertical direction. Its movement is limited. The left wing (6) can move vertically. This aerodynamic lift force, left wing (6) and the lower 30 to which the left wing (6) is attached the same as the vertical pressure force produced by the vertical spring (8) on the central part (4) This force is in the direction where the upper center piece (5) and the lower center piece (4) are in contact. Due to the surface geometry, namely the descending and ascending angle surfaces (41,51), the left and This forces the right wing (6,7) to remain in an open position.

Claims

11 REQUESTS 1. A fuselage (14) suitable for use with aircraft and munitions. on which there is a left and right wing (6, 7) which is initially closed and user request opening the left and right wings (6, 7) in the appropriate position for flight in line with an axis extending from the body (14) providing the center of the said axis 5 The figure shows movement both circularly and linearly along the axis. a sub-center piece (4) and on the sub-center piece (4) positioned left wing (6), on lower center piece (4) positioned circularly with the axis in question as its center. a movable upper center piece (5) and 10 on the upper center piece (5) The lower center part (4) which includes a positioned right wing (7) a vertical arc both circularly and linearly along the axis (8) spirally on the lower center piece (4) so ​​that it can move through a rising angle surface that opens at an angle (41), rising angle surface (41) a descending angle opened on the upper central piece (5) to be symmetrical 15 a wing opening mechanism characterized by surface (51) (1).

2. A spacer (2) positioned on the body (14) and this spacer (2) a vertical shaft (3) extending over it, as in claim 1 Wing opening mechanism (1). 20 3. Linear along a horizontal shaft (13) positioned on the body (14). a request characterized by a movable part (9) that can act as A wing opening mechanism like the one in 1 (1).

4. A horizontal wire with one end attached to the body (14) and the other end attached to the movable part (9) A wing opening mechanism as in request 3 characterized by a spring (10) 25 (1).

5. A primary wire with one end connected to the movable part (9) and the other end connected to the intermediate part (2). arm (11) and one end to the movable part (9) and the other end to the upper center part (5) a wing as in claim 3 characterized by a second arm (12) attached. opening mechanism (1). 30

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