Unmanned aerial vehicle type patrolling bomb and assembling method thereof

Abstract

The invention discloses an unmanned aerial vehicle type patrolling bomb which comprises a patrolling bomb body and is characterized in that a folding supporting frame is installed on the bottom face of the patrolling bomb body, and the invention further discloses an assembling method of the unmanned aerial vehicle type patrolling bomb. According to the unmanned aerial vehicle type patrolling bomb, the folding supporting frame is creatively added to the bottom face of the unmanned aerial vehicle type patrolling bomb, so that the supporting frame is convenient to store or support, and the placement convenience of the unmanned aerial vehicle type patrolling bomb is improved. The invention further discloses an unmanned aerial vehicle type patrolling bomb assembling method, the folding type supporting frame can be assembled conveniently, the folding type supporting frame can be installed in order, and assembling troubles are reduced.

Description

Technical Field

[0001] The invention discloses a UAV type cruise missile and an assembly method thereof. Background Art

[0002] A cruise missile is a precision munition that can cruise over a target area and execute combat orders. It is also the product of the organic combination of drone technology and ammunition technology. It mainly undertakes combat missions such as battlefield reconnaissance, target indication, precision strikes, damage assessment, communication relay, electronic countermeasures, air warning and special payload delivery. A cruise missile is an intelligent missile between a cruise missile and a drone. Its biggest feature is that it can fly in the target area for a period of time and conduct reconnaissance, and then launch an attack after the operator determines the target. A cruise missile consists of a warhead, a guidance device, a propulsion system, a control device (including missile wings), a stabilization device (including tail fins or parachutes), etc. Existing cruise missiles, such as micro-small drone-type cruise missiles, lack a suitable support structure when placed, making it inconvenient to place the cruise missile, causing trouble. Summary of the invention

[0003] In order to solve the existing problems, the present invention provides a drone-type cruise missile, including a cruise missile body, characterized in that: a foldable support frame is installed on the bottom surface of the cruise missile body, the foldable support frame includes a pair of support rods 1 and 2 and a pair of support rods 3 and 4, the bottom surface of the cruise missile body is respectively provided with slotted shaft connection blocks 1 and 2 for axially connecting the pair of support rods 1 and 2, and slotted shaft connection blocks 3 and 4 for axially connecting the pair of support rods 3 and 4, the tail ends of the pair of support rods 1 and 2 and the pair of support rods 2 and 3 are all provided with internal screw holes, the shaft connection blocks 1, 2 and the shaft connection blocks 3 and 4 are respectively embedded with corresponding internal screw holes corresponding to the internal screw holes, and are screwed and installed by long bolts; The bottom surface of the cruise missile body is also provided with a clamping block 1, a clamping block 2, a clamping block 3, and a clamping block 4 for clamping the support rods 1 and 2 arranged in pairs and the support rods 3 and 4 arranged in pairs.

[0004] As a further limitation of the present invention, the support rod one and the support rod two arranged in pairs are arranged at the inner ends of the support rod three and the support rod four arranged in pairs.

[0005] As a further limitation of the present invention, the clamping block 1 and the clamping block 2 are located at the inner ends of the shaft connection block 3 and the shaft connection block 4, and the distance between the clamping block 1 and the clamping block 2 is smaller than the distance between the shaft connection block 3 and the shaft connection block 4.

[0006] As a further limitation of the present invention, the clamping block three and the clamping block four are located at the inner ends of the shaft connection block one and the shaft connection block two, and the distance between the clamping block three and the clamping block four is smaller than the distance between the shaft connection block three and the shaft connection block four.

[0007] As a further limitation of the present invention, the card block 1, the card block 2, the card block 3, and the card block 4 are all provided with card slots, and magnetic sheets are respectively provided on both sides of the card slots.

[0008] As a further limitation of the present invention, magnetic blocks are embedded at the tail ends of the support rod 1 and the support rod 2, and are magnetically attracted to the clamping block 1 and the clamping block 2 respectively.

[0009] As a further limitation of the present invention, magnetic blocks are embedded at the tail ends of the support rod three and the support rod four, which are magnetically attracted and clamped on the clamping block three and the clamping block four respectively.

[0010] As a further limitation of the present invention, the support rods one, two, three and four are of the same length, and have through holes in the middle thereof, in which two studs are installed, and flange nuts are installed at both ends of the two studs.

[0011] The present invention also discloses a method for assembling a drone-type cruise missile, which is characterized in that the assembly method comprises the following steps: The first step is to assemble the shaft connection block 1, the shaft connection block 2, the shaft connection block 3 and the shaft connection block 4: screw or glue the shaft connection block 1, the shaft connection block 2, the shaft connection block 3 and the shaft connection block 4 on the bottom surface of the cruise missile; The second step is to assemble the card block 1, the card block 2, the card block 3 and the card block 4: according to the distance between the matching block 1 and the matching block 2, the card block 3 and the card block 4 are assembled at the inner ends of the matching block 1 and the matching block 2, and the distance is less than the distance between the matching block 1 and the matching block 2; according to the distance between the matching block 3 and the matching block 4, the card block 1 and the card block 2 are assembled at the inner ends of the matching block 3 and the matching block 4, and the distance is less than the distance between the matching block 3 and the matching block 4; The third step is to assemble the support rod 1, the support rod 2, the support rod 3 and the support rod 4: respectively make the inner screw holes embedded at one end of the support rod 1 and the support rod 2 correspond to the matching inner screw holes embedded at the matching block 1 and the matching block 2, and screw them with long bolts and then fix them with nuts; respectively make the inner screw holes embedded at one end of the support rod 2 and the support rod 3 correspond to the matching inner screw holes embedded at the matching block 2 and the matching block 3, and screw them with long bolts and then fix them with nuts; Step 4: Prop up support rod 1, support rod 2, support rod 3 and support rod 4: Align support rod 1 and support rod 2 with the through holes in the center of support rod 3 and support rod 4 respectively and penetrate them with studs at both ends, and then install flange nuts at both ends; The fifth step is to assemble support rod 1, support rod 2, support rod 3 and support rod 4: magnetically attach the tail ends of support rod 1 and support rod 2 to block 1 and block 2 respectively; magnetically attach the tail ends of support rod 3 and support rod 4 to block 3 and block 4 respectively.

[0012] The technical effect of the present invention is that a foldable support frame is creatively added to the bottom surface of the drone-type cruise missile, so that the support frame is convenient for storage or support, and the convenience of placing the drone-type cruise missile is increased. In addition, the present application also discloses a method for assembling the drone-type cruise missile, which facilitates the assembly of the foldable support frame, enables it to be installed in an orderly manner, and reduces the trouble of assembly. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the structure of the present invention; Figure 2 yes Figure 1 Schematic diagram of the usage status structure; Figure 3 It is a schematic diagram of the shaft connection block structure; Figure 4 It is a schematic diagram of the card block structure; Figure 5 is a schematic diagram of the support rod structure; Figure 6 It is a schematic diagram of the assembly method of the present invention; In the figure: a cruise missile body 1, a foldable support frame 2, a support rod 1 21, a support rod 2 22, a support rod 3 23, a support rod 4 24, an inner screw hole 25, a through hole 26, studs at both ends 27, a flange nut 28, an axial connection block 1 3, an axial connection block 2 31, an axial connection block 3 32, an axial connection block 4 33, a long bolt 36, a fixing nut 37, a clamping block 1 4, a clamping block 2 41, a clamping block 4 43, a clamping slot 44, a magnetic sheet 45, and a magnetic block 46. DETAILED DESCRIPTION

[0014] Embodiment 1 like Figure 1-6 As shown, this embodiment provides a drone-type cruise missile, including a cruise missile body 1. In this application, a suitable folding support frame is creatively installed on the bottom surface of the cruise missile body, so that the cruise missile body can fold the folding support frame on the bottom surface when in use. When not in use, it can support the formation of Figure 2 The supporting state of the cruise missile body of the present application is therefore very creative. A folding support frame 2 is installed on the bottom surface of the cruise missile body 1, and the folding support frame 2 includes a pair of support rods 1 21, 22 and a pair of support rods 3 23, 24, which are the same length. The pair of support rods 1 21 and 22 are arranged at the inner side ends of the pair of support rods 3 23 and 4 24. It is convenient for assembly.

[0015] The bottom surface of the cruise missile body 1 is respectively provided with slotted shaft connection blocks 1 3 and 31 for axially connecting the paired support rods 1 21 and 22, and slotted shaft connection blocks 3 32 and 33 for axially connecting the paired support rods 3 23 and 4 24. The shaft connection blocks 1 21 and 22 and the paired support rods 3 23 and 4 24 are all provided with inner screw holes 25. The shaft connection blocks 1 3 and 31 and the shaft connection blocks 3 32 and 4 33 are respectively embedded with corresponding inner screw holes corresponding to and communicating with the inner screw holes 25, which are screwed and installed by long bolts 36 and fixed by fixing nuts 37. When the support rods 1, 2, 3 and 4 are axially connected, the fixing nuts can be loosened to form an axially connected support or folding structure for the support rods 1, 2, 3 and 4. When fixing the support rods one, two, three and four, the fixing nuts can be screwed to fix the support rods one, two, three and four axes.

[0016] The foldable support frame is not used and is a structure that is integrated with the bottom surface of the cruise missile body. Figure 1 As shown, the bottom surface of the cruise missile body 1 is also provided with a block 1 4, a block 2 41, and a block 3, a block 4 43 for clamping the support rod 1 21, the support rod 2 22, and the support rod 3 23, and the support rod 4 arranged in pairs. Block 1 4 and block 2 41 are located at the inner side ends of the shaft connection block 3 32 and the shaft connection block 4 33, and the distance between block 1 4 and block 2 41 is smaller than the distance between the shaft connection block 3 32 and the shaft connection block 4 33. Block 3 and block 4 43 are located at the inner side ends of the shaft connection block 1 and the shaft connection block 2, and the distance between block 3 and block 4 43 is smaller than the distance between the shaft connection block 3 32 and the shaft connection block 4 33. This makes it easy to fold or support. Block 1 4, block 2 41, block 3, and block 4 43 are all provided with a slot 44, and magnetic sheets 45 are provided on both sides of the slot 44. When the support rods are closed, the tail ends of the support rods 1 21 and 22 are embedded with magnetic blocks 46, which are magnetically clamped on the clamping blocks 1 4 and 2 41 respectively. The tail ends of the support rods 3 23 and 4 24 are embedded with magnetic blocks 46, which are magnetically clamped on the clamping blocks 3 and 4 43 respectively, forming a closed structure.

[0017] like Figure 2 As shown, when the support rods are supported, the support rods 1 21, 22, 3 and 4 are of the same length, and through holes 26 are opened in the middle thereof, studs 27 are installed at both ends of the studs 27, and flange nuts 28 are installed at both ends of the studs 27 to form a support structure.

[0018] like Figure 6 As shown, as a convenient installation method for UAV-type cruise missiles, using the following steps can reduce the installation time of workers and improve installation efficiency.

[0019] The assembly method comprises the following steps: The first step is to assemble the shaft connection block 1, shaft connection block 2, shaft connection block 3 and shaft connection block 4 on S101: screw or glue the shaft connection block 1, shaft connection block 2, shaft connection block 3 and shaft connection block 4 on the bottom surface of the cruise missile; The second step, S102, is to assemble the card block 1, the card block 2, the card block 3 and the card block 4: according to the distance between the matching block 1 and the matching block 2, the card block 3 and the card block 4 are assembled at the inner ends of the matching block 1 and the matching block 2, and the distance is less than the distance between the matching block 1 and the matching block 2; according to the distance between the matching block 3 and the matching block 4, the card block 1 and the card block 2 are assembled at the inner ends of the matching block 3 and the matching block 4, and the distance is less than the distance between the matching block 3 and the matching block 4; The third step, S103, assemble the support rod 1, the support rod 2, the support rod 3 and the support rod 4: respectively make the inner screw holes embedded at one end of the support rod 1 and the support rod 2 correspond to the matching inner screw holes embedded at the matching block 1 and the matching block 2, and screw them with long bolts and then fix them with nuts; respectively make the inner screw holes embedded at one end of the support rod 2 and the support rod 3 correspond to the matching inner screw holes embedded at the matching block 2 and the matching block 3, and screw them with long bolts and then fix them with nuts; Step 4, S104 props up support rod 1, support rod 2, support rod 3 and support rod 4: match support rod 1 and support rod 2 with the through holes in the center of support rod 3 and support rod 4 respectively and penetrate them with studs at both ends, and then install flange nuts at both ends; The fifth step, S105, close the support rod 1, the support rod 2, the support rod 3 and the support rod 4: magnetically attract the tail ends of the support rod 1 and the support rod 2 to the card block 1 and the card block 2 respectively; magnetically attract the tail ends of the support rod 3 and the support rod 4 to the card block 3 and the card block 4 respectively.

[0020] It should be pointed out that the above preferred embodiments are only for illustrating the technical concept and features of the present invention, and their purpose is to enable people familiar with the technology to understand the content of the present invention and implement it accordingly, and they cannot be used to limit the protection scope of the present invention. Any equivalent changes or modifications made according to the spirit of the present invention should be included in the protection scope of the present invention.

Claims

1. A drone-type cruise missile, comprising a cruise missile body, characterized in that: A foldable support frame is installed on the bottom surface of the cruise missile body, and the foldable support frame includes support rod 1 and support rod 2 arranged in pairs, and support rod 3 and support rod 4 arranged in pairs. The bottom surface of the cruise missile body is respectively provided with slotted shaft connection blocks 1 and shaft connection blocks 2 for axially connecting the support rod 1 and support rod 2 arranged in pairs, and slotted shaft connection blocks 3 and shaft connection blocks 4 for axially connecting the support rod 3 and support rod 4 arranged in pairs. The support rods 1 and support rod 2 arranged in pairs and the support rods 2 and support rod 3 arranged in pairs are all embedded with internal screw holes, and the shaft connection blocks 1 and shaft connection blocks 2 and shaft connection blocks 3 and shaft connection blocks 4 are respectively embedded with corresponding internal screw holes corresponding to the internal screw holes and connected, and are screwed and installed by long bolts; The bottom surface of the cruise missile body is also provided with a clamping block 1, a clamping block 2, a clamping block 3, and a clamping block 4 for clamping the support rods 1 and 2 arranged in pairs and the support rods 3 and 4 arranged in pairs.

2. The drone-type loitering missile according to claim 1, characterized in that: The support rod one and the support rod two arranged in pairs are arranged at the inner ends of the support rod three and the support rod four arranged in pairs.

3. The drone-type loitering missile according to claim 1, characterized in that: The clamping block 1 and the clamping block 2 are located at the inner side ends of the shaft connection block 3 and the shaft connection block 4, and the distance between the clamping block 1 and the clamping block 2 is smaller than the distance between the shaft connection block 3 and the shaft connection block 4.

4. The drone-type loitering missile according to claim 1, characterized in that: The clamping block three and the clamping block four are located at the inner side ends of the shaft connection block one and the shaft connection block two, and the distance between the clamping block three and the clamping block four is smaller than the distance between the shaft connection block three and the shaft connection block four.

5. The drone-type loitering missile according to claim 1, characterized in that: The card block 1, the card block 2, the card block 3 and the card block 4 are all provided with card slots, and magnetic sheets are respectively arranged on both sides of the card slots.

6. The drone-type loitering missile according to claim 1, characterized in that: The tail ends of the support rod 1 and the support rod 2 are embedded with magnetic blocks, which are magnetically clamped on the clamping block 1 and the clamping block 2 respectively.

7. The drone-type loitering missile according to claim 1, characterized in that: The tail ends of the support rod three and the support rod four are embedded with magnetic blocks, which are magnetically attracted and clamped on the clamping block three and the clamping block four respectively.

8. The drone-type loitering missile according to claim 1, characterized in that: The support rods 1, 2, 3 and 4 have the same length, and are all provided with through holes in the middle thereof, in which two studs are installed, and flange nuts are respectively installed at both ends of the two studs.

9. A method for assembling a drone-type cruise missile as described in claims 1-8, characterized in that: The assembly method comprises the following steps: The first step is to assemble the shaft connection block 1, the shaft connection block 2, the shaft connection block 3 and the shaft connection block 4: screw or glue the shaft connection block 1, the shaft connection block 2, the shaft connection block 3 and the shaft connection block 4 on the bottom surface of the cruise missile; The second step is to assemble the card block 1, the card block 2, the card block 3 and the card block 4: according to the distance between the matching block 1 and the matching block 2, the card block 3 and the card block 4 are assembled at the inner ends of the matching block 1 and the matching block 2, and the distance is less than the distance between the matching block 1 and the matching block 2; according to the distance between the matching block 3 and the matching block 4, the card block 1 and the card block 2 are assembled at the inner ends of the matching block 3 and the matching block 4, and the distance is less than the distance between the matching block 3 and the matching block 4; The third step is to assemble the support rod 1, the support rod 2, the support rod 3 and the support rod 4: respectively make the inner screw holes embedded at one end of the support rod 1 and the support rod 2 correspond to the matching inner screw holes embedded at the matching block 1 and the matching block 2, and screw them with long bolts and then fix them with nuts; respectively make the inner screw holes embedded at one end of the support rod 2 and the support rod 3 correspond to the matching inner screw holes embedded at the matching block 2 and the matching block 3, and screw them with long bolts and then fix them with nuts; Step 4: Prop up support rod 1, support rod 2, support rod 3 and support rod 4: Align support rod 1 and support rod 2 with the through holes in the center of support rod 3 and support rod 4 respectively and penetrate them with studs at both ends, and then install flange nuts at both ends; The fifth step is to assemble support rod 1, support rod 2, support rod 3 and support rod 4: magnetically attach the tail ends of support rod 1 and support rod 2 to block 1 and block 2 respectively; magnetically attach the tail ends of support rod 3 and support rod 4 to block 3 and block 4 respectively.

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