below are a detailed description of the embodiments of the disclosure in view of the accompanying drawings , and the clear and detailed description of the technical schemes of the present disclosure . as shown in fig1 - 5 , the disclosure provides a model aircraft comprising a body 1 , a wing 2 , a vertical tail 3 and a horizontal tail 4 . at least one first male female buckle 5 is provided between the wing 2 and the body 1 . said wing is securely mounted on the body 1 through the first male female buckle 5 . at least one second male female buckle 6 is provided between the vertical tail 3 and the body 1 . the vertical tail 3 is securely mounted on the body 1 through the second male female buckle . said horizontal tail and body 1 is in the form of a one - piece unit . during disassembly and assembly , it is only needed to disassemble the wing 2 and vertical tail 3 from the body 1 , or assemble of the same . the disassembly and assembly is easy and helps to improve work efficiency . in the present embodiment , said model aircraft comprises two of the first male female buckles 5 and two of the second male female buckles 6 . in other embodiments , other numbers of the first male female buckles 5 and the second male female buckles 6 may be provided , such as three of the first male female buckles 5 and three of the second male female buckles 6 . said first male female buckle 5 comprises a first male buckle member 51 and a first female buckle member 52 that are configured to cooperate with each other . in the present embodiment , the first male buckle member 51 is configured to be mounted on the wing 2 , the first female buckle member 52 is configured to be mounted on the body 1 , and the first male buckle member 51 and the first female buckle member 52 are configured to cooperate to secure the wing 2 on the body 1 ; a mounting groove 25 is provided at a bottom of the wing 2 ; an end of the first male buckle member 51 is configured to be secured in the mounting groove 25 ; a mounting hole 15 is provided at a bottom of the body 1 , and an end of the first female buckle member 52 is configured to pass through the mounting hole 15 and is configured to be stopped by a bottom of the mounting hole 15 . without being limited to this , alternatively , the first male buckle member 51 is configured to be mounted on the body 1 , the first female buckle member 52 is configured to be mounted on the wing 2 , and the first male buckle member 51 and the first female buckle member 52 are configured to cooperate to secure the wing 2 on the body 1 . as shown in fig6 , the first male buckle member 51 comprises an inserting axis 511 and a plurality of connecting arms 512 formed from an extension of an end of the inserting axis 511 . a free end of one of the plurality of connecting arms 512 is provided with a first buckle tongue 513 . the plurality of connecting arms 512 are spaced apart , and a retaining space 514 is formed by the plurality of connecting arms 512 . according to the present embodiment , the first male buckle member 51 is made of elastic material . when being pressed by external force , said connecting arms 512 deform toward the retaining space 514 and retract to be closer . the first female buckle member 52 comprises a first base 521 and a blocking piece 522 provided on an end of the first base 521 ; the first base 521 is provided with a through - hole 523 in a center of the first base 521 , and the through - hole 523 passes through the blocking piece 522 . according to the present embodiment , the mounting hole 15 is a step - shaped through - hole with a step . when the first male female buckle 5 is buckled together , the first female buckle member 52 is configured to be inserted into the mounting hole 15 , and the blocking piece 522 of the first female buckle member 52 is configured to abut against the step of the step - shaped through - hole . therefore the blocking piece 522 of said first female buckle member 52 is retained within the mounting hole 15 , and this ensures the smooth look of the exterior of the aircraft . when the first male buckle member 51 and the first female buckle member 52 are buckled together , the plurality of connecting arms 512 of the first male buckle member 51 are configured to be inserted into the through - hole 523 of the first base , and the first buckle tongue 513 is configured to abut against the blocking piece 522 of the first female buckle member 52 . the blocking piece 522 is provided with a recess 524 in communication with the through - hole 523 , and the first buckle tongue 513 of the first male buckle member 51 is configured to abut against a bottom of the recess 524 . when the first male buckle member 51 and the first female buckle member 52 are buckled together , the connecting arms 512 of the first male buckle member 51 are inserted into the through - hole 523 ; the first buckle tongues 513 at the free end of the connecting arms 512 are deformed by the pressing force of the interior wall of through - hole 523 , and retract to be closer ; further insertion of the inserting axis 511 of the male buckle member 51 pushes the first buckle tongue 513 out of the through - hole 523 ; the first buckle tongue 513 bulges outwardly due to the lack of the pressing force from the wall of the through - hole 523 ; when the inserting axis 511 is pulled back , the first buckle tongue 513 abuts against the blocking piece 522 of the first female buckle member 52 , and therefore cannot retract back into the through - hole 523 ; thus , the first male buckle member 51 and the first female buckle member 52 are buckled together , and the first buckle tongue 513 is retained in the recess 524 . when the first male female buckle is to be separated , the first buckle tongues 513 are to be pressed toward their center so that multiple first buckle tongues 513 are closed together and inserted into the through - hole 523 of the first female buckle member 52 ; the first male buckle member 51 is then applied a force away from the first female buckle member 52 , and the first male buckle member 51 is pulled back from the first female buckle member 52 , so that the first male female buckle is separated ; the wing 2 is also separated from the body 1 . therefore , the disassembly of the wing 2 from the body 1 is simple and convenient . furthermore , the first male buckle member 51 further comprises a position - restraining portion 515 provided on the inserting axis 511 . the position - restraining portion 515 is projected on an outer surface of the inserting axis 511 . the position - restraining portion 515 is configured to abut against an inner surface of the through - hole 523 , so that the first male buckle member 51 is secured with the first female buckle member 52 . this restricts the buckle position of the first female buckle member 52 , and prevents the first male buckle member 51 to become loose from the first female buckle member 52 after the first male buckle member 51 and first female buckle member 52 are buckled together . according to the present embodiment , the position - restraining portion 515 is a protruding rib in parallel to an axial direction of the inserting axis 511 . a height of the protruding rib above the inserting axis 511 is gradually increased from an end adjacent to the plurality of connecting arms 512 toward the other end . that is , the outer surface of the protruding rib is at an angle to the axial direction of the inserting axis 511 ; when inserting axis 511 enters the through - hole 523 of the first female buckle member 52 , the first female buckle member 52 may not go through the other end of the inserting axis 511 due to the position restriction function of the protruding ribs . furthermore , the first male buckle member 51 further comprises a first mounting portion 516 . the first mounting portion 516 is configured to be disposed on the first male buckle member 51 at an end remote from end with the first buckle tongue 513 . the first mounting portion 516 and the mounting groove 25 are configured to cooperate so that the first male buckle member 51 is secured to the wing . according to an embodiment , the first mounting portion 516 comprises a horizontal plate 5161 and a pair of vertical plates 5162 . the horizontal plate 5161 is provided on an end of the first male buckle member 51 away from end of the first buckle tongue 513 . the pair of vertical plates 5161 extends from a side of the horizontal plate 5161 . the pair of vertical plates 5162 is disposed to intersect each other ; fig6 shows a vertical cross . the mounting groove 25 comprises a pair of insertion slots disposed to intersect each other . during assembly , the pair of vertical plates 5162 is respectively inserted into the pair of insertion slots , and the first male buckle member 51 is secured with the wing 2 by interference fit . in other embodiments , the first male buckle member 51 may be secured with the wing 2 through other fixing methods such as through bonding . the second male female buckle 6 comprises a second male buckle member 61 and a second female buckle member 62 that are configured to cooperate with each other . the second male buckle member 61 is configured to be mounted on the body 1 , the second female buckle member 62 is configured to be mounted on the vertical tail 3 , and the second male buckle member 61 and the second female buckle member 62 are configured to cooperate to secure the vertical tail 3 on the body 1 . without being limited to the above , alternatively , the second male buckle member 61 is configured to be mounted on the vertical tail 3 , the second female buckle member 62 is configured to be mounted on the body 1 , and the second male buckle member 61 and the second female buckle member 62 are configured to cooperate to secure the vertical tail 3 on the body 1 . the body 1 and vertical tail 3 are respectively provided with a first mounting position 16 and a second mounting position 36 , to secure the assembly of the second male buckle member 61 and second female buckle 62 . the second male buckle member 61 and second female buckle 62 are respectively bonded to the first mounting position 16 and the second mounting position 36 by sticky materials such as glue or double - sided tape . as shown in fig7 , the second male buckle member 61 comprises a second mounting portion 611 , a neck portion 612 projected on a side of the second mounting portion 611 , and a second buckle tongue 613 formed from an extension of the neck portion 612 . the second mounting portion 611 is configured to secure the second male buckle member 61 on the wing 1 ; and the second buckle tongue 613 is configured to buckle with the second female buckle member 62 . furthermore , the second mounting portion 611 is mounted on the first mounting position 16 . the first mounting position 16 is a recess slot or a plane surface . the second mounting portion 611 is bonded on the first mounting position 16 . the second female buckle member 62 comprises a second base 621 and an engaging groove 622 provided on the second base 621 . the second buckle tongue 613 is configured to be inserted into the engaging groove 622 and abut against the engaging groove 622 , so that the second male buckle member 61 is secured with the second female buckle member 62 . the second base 621 is provided with a pair of oppositely disposed snap buckles 623 , with the snap portions being arranged to be opposing to each other . the engaging groove 622 is formed between the snap buckles 623 , and the second buckle tongue 613 is configured to be stopped by the snap buckles 623 . when the second male female buckle 6 is buckled , the second buckle tongue 613 is inserted into the engaging groove 622 through the opening of the engaging groove 622 ; interior walls of the snap buckles 623 are pushed to expand outwardly ; the opening of the engaging groove 622 expands so that the second buckle tongue 613 may be inserted into the engaging groove 622 . when the second buckle tongue 613 is completely inserted into the engaging groove 622 , the snap buckles 623 springs back to snap the second buckle tongue 613 , so that the second male female buckle is buckled together ; thus the vertical tail 3 is mounted on the wing 1 and the assembly process is convenient . when the vertical tail 3 is to be disassembled from the wing 1 , the second male buckle member 61 and the second female buckle member 62 are applied with forces toward opposite directions . snap buckle 23 is pushed outwardly by the second buckle tongue 613 and is expanded . the second buckle tongue 613 is pulled back from the opening of the engaging groove 622 , so that the second male buckle member 61 is separated from the second female buckle member 62 . the disassembly process is very convenient as well . according to an embodiment , the second base 621 comprises a base piece 6211 and a pair of symmetrically disposed l - shaped pieces 6212 at both ends of the base piece 6211 . the snap buckles 623 are projected on the base piece 6211 . when the second male buckle 61 and the second female buckle member 62 are buckled together , the neck portion 612 is sandwiched between the snap buckles 623 . the l - shaped pieces 6212 are configured to abut against the second mounting portion 611 of the second male buckle member 61 . the second base 621 is to be bonded on the second mounting position 36 ; the second mounting position 36 is a recess groove , with a shape matching the exterior shape of the second base 621 ; thus the second female buckle member is configured to be accommodated in the second mounting position 36 . as a further improvement in the disclosure , at least one third male female buckle 7 is provided between the wing 2 and the body 1 to further secure the wing 2 , and the wing 2 is more securely assembled on the body 1 . according to an embodiment , preferably two of third male female buckles 7 are provided . the third male female buckles 7 may have the same structure of the second male female buckle , and have the same mode of assembly , which are not described in detail herein . the third male female buckle 7 and the first male female buckle 5 are respectively provided on different connecting interfaces of the wing 2 and the body 1 , to ensure that each connecting interface is securely connected and the wing 2 is tightly assembled on the body 1 . the structures of the first , second and third male female buckle 5 , 6 and 7 are not limited to the above disclosures and other male female buckles that implement disassembly and assembly functions may also be employed . the descriptions above are preferred embodiments . thus , it will be apparent to one skilled in the art that modifications may be made without departing from the protection scope of the claims set out below , and such modifications are within the protective scope of the present disclosure .
the present disclosure provides a model aircraft , comprising a body , a wing and a vertical tail . at least one first male female buckle is provided between the wing and the body . the wing is configured to be securely mounted on the body by the first male female buckle . at least one second male female buckle is provided between the vertical tail and the body . the vertical tail is configured to be securely mounted on the body by the second male female buckle . in the disclosed model aircraft , the wing and the vertical tail can be removably assembled on the body by multiple male female buckles . it is structurally simple ; it is convenient to disassemble the aircraft during storage to save space , and it is convenient and fast to assemble the aircraft during use , thereby improving the ease of assembly .