Folding module assembly type airplane

Abstract

The utility model provides a folding module assembly type airplane which is an airplane model body with an assembly type structure and comprises an airplane nose part, an airplane body part, a main wing part, a front undercarriage part and a bracket part, the nose part, the fuselage part and the nose landing gear part are respectively in a three-dimensional shape formed by folding a nose plate, a fuselage plate and a nose landing gear plate in a first plane shape; and the main wing part is a two-dimensional main wing plate or a three-dimensional shape formed by folding the main wing plate in a first plane shape. According to the utility model, the nose part, the fuselage part, the main wing part, the nose landing gear part and the bracket part are modularly designed, and each part is in a three-dimensional shape formed by folding the surface plates, so that after the folding is completed, all the parts are spliced and assembled to form the airplane model body, the interestingness is strong, the operational ability of children is improved, and the interestingness of the children is improved. And each surface plate is made of a corrugated board, has the characteristics of high toughness, environmental protection and folding resistance, is environment-friendly and pollution-free, and is not easy to damage.

Description

TECHNICAL FIELD

[0001] The utility model relates to folding three -dimensional assembling toy technical field, especially a folding module assembling type airplane. BACKGROUND

[0002] At present, most of children's toys on the market are plastic toy classes, and high-quality plastic toys have relatively less harmful ingredients, but many inferior toys are usually made of "two materials", and the color and luster are poor after reprocessing, and the materials contain more toxic and harmful substances, which are harmful to the health of children.

[0003] In addition, the toy airplane model on the market is usually integrally formed by injection molding and cannot be disassembled and assembled, and is limited to observation and has no playability and strong interest, and the hand operation ability of children is not enough.

[0004] Therefore, we intend to develop an airplane which can be assembled, has high playability and strong interest, and is environmentally friendly.

[0005] In view of the above problems, we provide a new technical scheme. CONTENT OF THE UTILITY MODEL

[0006] The utility model aims at solving one of the technical problems in the prior art. To this end, the utility model provides a folding module assembling type airplane, which adopts the technical scheme that:

[0007] A folding module assembling type airplane is an airplane model body of an assembling type structure, comprising a nose section, a fuselage section, a main wing section, a front landing gear section and a support section; the nose section, the fuselage section and the front landing gear section are respectively formed by a nose plate, a fuselage plate and a front landing gear plate in a three-dimensional form folded in a first plane form; and the main wing section is a two-dimensional main wing plate or a three-dimensional form folded by a main wing plate in a first plane form.

[0008] According to the folding module assembling type airplane of the utility model embodiment, a fixed clamp plate is arranged between the nose section and the fuselage section, which is used for positioning the three-dimensional form of the nose section and the fuselage section and connecting the nose section and the fuselage section.

[0009] According to the folding module assembling type airplane of the utility model embodiment, the support section comprises a support body and a plug-in plate plugged and fixed to the support body, and the support body is a three-dimensional form folded by a support plate in a first plane form.

[0010] According to the folding module assembling type airplane of the utility model embodiment, a tail section is assembled at the rear end of the main wing section, and the tail section is a three-dimensional form folded by a tail plate in a first plane form.

[0011] According to an embodiment of the present invention, a foldable modular assembly aircraft has a tail section assembled below the rear end of the main wing section. The tail section is a three-dimensional shape formed by folding a tail section panel in a first planar shape.

[0012] According to an embodiment of the present invention, a foldable modular assembly aircraft has a cockpit canopy assembled on the top between the nose and the fuselage. The cockpit canopy is a three-dimensional shape formed by folding a cockpit canopy plate in a first planar shape.

[0013] According to an embodiment of the present invention, a foldable modular assembly aircraft has at least one tail nozzle section assembled at the rear end of the main wing section, wherein the tail nozzle section is a three-dimensional shape formed by folding a tail nozzle plate in a first planar shape.

[0014] According to an embodiment of the present invention, a folding modular assembly aircraft has a canard wing inserted in front of the main wing, wherein the canard wing is a three-dimensional shape formed by folding a canard wing plate in a first planar shape.

[0015] According to an embodiment of the present invention, a folding modular assembly aircraft has a fairing section assembled at the top middle of the fuselage. The fairing section is a three-dimensional shape formed by folding a fairing plate in a first planar shape.

[0016] Compared with the prior art, the beneficial effects of this utility model are:

[0017] In this invention, the nose section, fuselage section, main wing section, front landing gear section, and support section are modularly designed, and each part is a three-dimensional shape formed by folding flat plates. After folding, the various parts can be spliced ​​and assembled to form an airplane model, which is highly interesting and improves children's hands-on ability. In addition, each flat plate is made of corrugated cardboard, which has the characteristics of high toughness, environmental protection and folding resistance, and is environmentally friendly, pollution-free, and not easily damaged. Attached Figure Description

[0018] The above and / or additional aspects and advantages of this utility model will become apparent and readily understood from the description of the embodiments taken in conjunction with the following drawings, in which:

[0019] Figure 1 This is a disassembly diagram of Embodiment 1 of the present invention;

[0020] Figure 2 This is a disassembly diagram of Embodiment 2 of the present invention;

[0021] Figure 3 This is a disassembly diagram of Embodiment 3 of the present invention;

[0022] Figure 4 This is a disassembly diagram of Embodiment 4 of the present invention;

[0023] Figure 5 This is a disassembly diagram of Embodiment 5 of the present invention;

[0024] Figure 6 This is a disassembly diagram of the bracket portion in some embodiments of the present invention.

[0025] Explanation of key component symbols:

[0026] 10. Nose panel; 20. Fuselage panel; 30. Front landing gear panel; 40. Main wing panel; 50. Fixing clamp; 51. Front clamp slot; 52. Rear clamp slot; 60. Bracket plate; 61. Connecting plate; 70. Tail wing panel; 71. Tail wing bottom plate; 72. Tail wing flap; 80. Tail compartment panel; 90. Cockpit canopy; 100. Tail nozzle panel; 110. Canard; 120. Fairing panel. Detailed Implementation

[0027] The embodiments of this utility model are described in detail below. Examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout.

[0028] The orientation shown in the accompanying drawings should not be construed as limiting the specific protection scope of this utility model, but is only for reference and understanding of preferred embodiments. The product components shown in the drawings can be changed in position, increased in number, or simplified in structure.

[0029] The “connection” described in the specification and the “connection” relationship between the components shown in the accompanying drawings can be understood as a fixed connection, a detachable connection, or a connection that forms an integral unit; it can be a direct connection or a connection through an intermediate medium. Those skilled in the art can understand the connection relationship according to the specific circumstances and can derive different implementation methods such as screwing, riveting, welding, snap-fitting, or embedding to suitably replace the connection.

[0030] The directional terms such as up, down, left, right, top, and bottom mentioned in the instruction manual and the directions shown in the attached drawings indicate that the components can directly contact each other or contact each other through other features; for example, "up" can mean directly above or diagonally above, or it simply means above other objects; other directions can be understood by analogy.

[0031] The materials used to manufacture solid-shaped parts as shown in the specification and drawings may be metallic, non-metallic, or other synthetic materials. The machining processes used for solid-shaped parts may include stamping, forging, wire cutting, laser cutting, casting, injection molding, CNC milling, 3D printing, machining, etc. Those skilled in the art may adapt or combine the above materials and manufacturing processes according to different processing conditions, costs, and precision requirements.

[0032] This utility model provides a foldable modular assembly aircraft, such as Figures 1 to 6 As shown, it is an assembled aircraft model, including a nose section, fuselage section, main wing section, nose landing gear section, and support section; the nose section, fuselage section, and nose landing gear section are respectively formed by folding the nose plate 10, fuselage plate 20, and nose landing gear plate 30 in a first planar shape to form a three-dimensional solid shape; the main wing section is a two-dimensional main wing plate 40 or a three-dimensional solid shape formed by folding the main wing plate 40 in a first planar shape.

[0033] In this invention, the nose section, fuselage section, main wing section, front landing gear section, and support section are modularly designed, and each part is a three-dimensional shape formed by folding flat plates. After folding, the various parts can be spliced ​​and assembled to form an airplane model, which is highly interesting and improves children's hands-on ability. In addition, each flat plate is made of corrugated cardboard, which has the characteristics of high toughness, environmental protection and folding resistance, and is environmentally friendly, pollution-free, and not easily damaged.

[0034] In this embodiment, the nose section, fuselage section, main wing section, nose landing gear section, and support section are all equipped with insertion holes, snap-fit ​​grooves, snap-fit ​​seams, and other insertion and snap-fit ​​structures at their joints for assembly. For example, the main wing plate 40 has insertion holes for inserting the nose landing gear section. In addition, the fuselage plate 20 is designed with a main landing gear, which forms the main landing gear after folding.

[0035] Furthermore, in some embodiments of this utility model application, such as Figures 1 to 5 As shown, a fixing plate 50 is provided between the nose and the fuselage to position the three-dimensional shape of the nose and the fuselage and connect the nose and the fuselage. The fixing plate 50 includes a front clamping groove 51 and a rear clamping groove 52. After the fuselage is folded, the rear clamping groove 52 of the fixing plate 50 is inserted into it to clamp and fix it, preventing the folded part from loosening and stabilizing the three-dimensional shape of the fuselage. Then, the rear end of the folded nose is inserted into the front clamping groove 51 of the fixing plate 50 to realize the connection and fixation between the nose and the fuselage.

[0036] Furthermore, in some embodiments of this utility model application, such as Figure 6 As shown, the bracket part includes a bracket body and a plug plate 61 that is plugged into and fixed to the bracket body. The bracket body is a three-dimensional shape formed by folding the bracket plate 60 in a first planar shape.

[0037] Furthermore, in some embodiments of this utility model application, such as Figures 1 to 3As shown, a tail fin is assembled at the rear end of the main wing. The tail fin is a three-dimensional shape formed by folding a tail fin plate 70 in a first planar configuration. The tail fin plate 70 includes a tail fin base plate 71 and two tail fin flaps 72 on both sides. After the tail fin is folded, the tail fin base plate 71 is located below the rear end of the main wing, and the two tail fin flaps 72 on both sides protrude above the main wing through pre-drilled holes on the main wing.

[0038] Furthermore, in some embodiments of this utility model application, such as Figures 4 to 5 As shown, a tail section is assembled below the rear end of the main wing. The tail section is a three-dimensional structure formed by folding a tail section panel 80 in a first planar configuration. After folding, the tail section is inserted and fixed to the lower rear end of the main wing.

[0039] Furthermore, in some embodiments of this utility model application, such as Figure 1 , 2 As shown in Figures 3 and 4, a cockpit canopy is assembled on top between the nose and fuselage sections. The cockpit canopy is a three-dimensional shape formed by folding a cockpit canopy plate 90 in a first planar configuration. After folding, the cockpit canopy is inserted and fixed between the nose and fuselage sections. Specifically, the front end of the cockpit canopy is inserted into a pre-drilled hole in the nose section, and the rear end is inserted into a pre-drilled hole in the fuselage section.

[0040] Furthermore, in some embodiments of this utility model application, such as Figure 1 , 2 As shown in Figure 3, at least one tail nozzle is assembled at the rear end of the main wing section. The tail nozzle is a three-dimensional shape formed by folding the tail nozzle plate 100 in a first planar shape. After folding, the tail nozzle is inserted and fixed to the rear end of the main wing section, specifically, it is inserted into a pre-set tail fork at the rear end of the main wing plate 40, as shown in Figure 3. Figure 1 , Figure 2 The dual-tail nozzle design was showcased. Figure 3 The design of the single tail nozzle section was showcased.

[0041] Furthermore, in some embodiments of this utility model application, such as Figure 2 As shown, a canard wing is inserted into the front of the main wing. The canard wing is a three-dimensional shape formed by folding the canard wing plate 110 in a first planar shape. After folding, the canard wing is inserted and fixed to the front of the main wing, specifically, it is inserted into a pre-drilled hole on the main wing plate 40.

[0042] Furthermore, in some embodiments of this utility model application, such as Figure 4As shown, a fairing is assembled at the top center of the fuselage. The fairing is a three-dimensional shape formed by folding a fairing plate 120 in a first planar configuration. After folding, the fairing is inserted and fixed to the front of the fuselage, specifically into a pre-drilled hole on the fuselage.

[0043] Although the present invention has been described in detail with reference to the above embodiments, it will be apparent to those skilled in the art that various changes or modifications can be made to the present invention without departing from the principles and spirit of the present invention as defined by the claims. Therefore, the detailed description of the embodiments in this disclosure is for explanation only and not for limiting the present invention, but rather the scope of protection is defined by the content of the claims.

Claims

1. A folding modular aircraft, characterized in that, The model body of the aircraft is of an assembled structure, comprising a nose part, a fuselage part, a main wing part, a front landing gear part and a support part; the nose part, the fuselage part and the front landing gear part are respectively formed by a nose plate (10), a fuselage plate (20) and a front landing gear plate (30) in a three-dimensional form folded in a first plane form; the main wing part is a two-dimensional main wing plate (40) or a three-dimensional form folded in a first plane form by the main wing plate (40).

2. A foldable modular aircraft according to claim 1, wherein, A fixing clamp plate (50) is arranged between the nose part and the fuselage part, for positioning the three-dimensional form of the nose part and the fuselage part and connecting the nose part and the fuselage part.

3. A foldable modular aircraft as in claim 1, wherein, The support part comprises a support body and a plug-in plate (61) plugged and fixed to the support body, and the support body is a three-dimensional form folded in a first plane form by a support plate (60).

4. A foldable modular aircraft as in claim 1, wherein, A tail part is assembled at the rear end of the main wing part, and the tail part is a three-dimensional form folded in a first plane form by a tail plate (70).

5. A foldable modular aircraft as in claim 1, wherein, A tail cabin part is assembled below the rear end of the main wing part, and the tail cabin part is a three-dimensional form folded in a first plane form by a tail cabin plate (80).

6. A foldable modular aircraft as claimed in claim 4, wherein, A cockpit cover part is assembled at the top between the nose part and the fuselage part, and the cockpit cover part is a three-dimensional form folded in a first plane form by a cockpit cover plate (90).

7. A foldable modular aircraft as in claim 4, wherein, At least one tail nozzle part is assembled at the rear end of the main wing part, and the tail nozzle part is a three-dimensional form folded in a first plane form by a tail nozzle plate (100).

8. A foldable modular aircraft as in claim 1, wherein, A canard part is plugged in front of the main wing part, and the canard part is a three-dimensional form folded in a first plane form by a canard plate (110).

9. A foldable modular aircraft as in claim 1, wherein, A fairing part is assembled at the middle top of the fuselage part, and the fairing part is a three-dimensional form folded in a first plane form by a fairing plate (120).

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