Separating spring mounting structure of aircraft and aircraft
By setting a first and a second fixed mounting component on the tail cover of the aircraft, and using snap-fit welding and threaded connections, the problem of spring fixing difficulties was solved, realizing a reliable connection and synchronous movement between the spring and the tail cover, which is suitable for tail cover separation of various booster aircraft.
Patent Information
- Application Number
- CN202511714423.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-11-21
- Publication Date
- 2026-01-20
AI Technical Summary
During the separation process of the tail cover of existing aircraft, the spring is difficult to fix and is prone to detachment, resulting in low reliability and the risk of impact.
The spring is connected to the first and second fixed mounting parts by means of snap welding and threaded connection to achieve reliable fixation between the spring and the tail cover, prevent the spring from rotating, and meet the synchronous movement under the spring compression and release action.
It achieves a reliable connection between the spring and the tail cover, facilitates disassembly and assembly, has strong adaptability, is suitable for tail cover separation of various booster aircraft, and improves the working performance of the aircraft.
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Figure CN121361573A_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to the technical field of aerospace vehicle structure, and particularly relates to a separation spring mounting structure for a vehicle and the vehicle. BACKGROUND
[0002] The upper stage is sent into the air by using a vehicle as a carrier, and is usually composed of several stages. When the lower stage completes the work, the lower stage must be discarded to improve the carrying capacity and ensure the effective load into the air, so the interstage separation structure needs to be designed. The box-type launch vehicle separates the first stage tail cover mainly by using the engine starting thrust as the separation impulse source. The spring installed on the tail cover is used as the lateral power source of the tail cover, so that the tail cover is thrown away along the specified trajectory during the separation process. Although this separation method can realize reliable separation, the dynamic disturbance of the separation process is large, and the vibration load of the separation body is large. The spring on the tail cover is easy to be separated from the tail cover, which has the risk of impacting the vehicle, so the reliability is not high. During the working process, the spring and the card at both ends must be reliably fixed, otherwise the spring is easy to be separated to form the redundant object. The existing spring and card connection at both ends only has the whole wrapping type and the elastic sheet friction fixing type, and the spring is often separated from the tail cover during the use process. Therefore, an urgent need exists for a spring end connection technology to meet the connection requirements of the spring. SUMMARY
[0003] The present application provides a separation spring mounting structure for a vehicle and the vehicle, which can solve the technical problem of difficult spring fixation in the prior art.
[0004] According to an aspect of the present application, a separation spring mounting structure for a boost aircraft is provided, the separation spring mounting structure comprising: a first fixed mounting member having a first mounting hole; a second fixed mounting member having a second mounting hole; a spring, one end of the spring being connected to the first fixed mounting member and the other end of the spring being connected to the second fixed mounting member; a threaded connecting member for fixedly connecting the spring and a tail cover body; the tail cover body having a threaded connecting hole, the threaded connecting member passing through the first mounting hole, the spring and the second mounting hole in sequence and cooperating with the threaded connecting hole on the tail cover body to achieve fixed connection of the second fixed mounting member and the tail cover body; the first fixed mounting member having a first fixed mounting base, a first clasp and a second clasp, the first fixed mounting base having a first bevel and a second bevel, the first bevel being oppositely arranged with the first clasp and the second bevel being oppositely arranged with the second clasp, the first clasp being arranged on one side of the first fixed mounting base and the second clasp being arranged on the other side of the first fixed mounting base, when connected, the first clasp and the second clasp wrap around one end of the spring, the free end of the first clasp is welded to the first fixed mounting base at the first bevel, the free end of the second clasp is welded to the first fixed mounting base at the second bevel, after welding, the excess first clasp and the second clasp are cut off, the weld joint is polished flat, thereby achieving fixed connection between the first fixed mounting member and one end of the spring; the second fixed mounting member having a second fixed mounting base, a third clasp and a fourth clasp, the second fixed mounting base having a third bevel and a fourth bevel, the third bevel being oppositely arranged with the third clasp and the fourth bevel being oppositely arranged with the fourth clasp, the third clasp being arranged on one side of the second fixed mounting base and the fourth clasp being arranged on the other side of the second fixed mounting base, the third clasp cooperating with one side of the spring and the fourth clasp cooperating with the other side of the spring, when connected, the third clasp and the fourth clasp wrap around the other end of the spring, the free end of the third clasp is welded to the second fixed mounting base at the third bevel, the free end of the fourth clasp is welded to the second fixed mounting base at the fourth bevel, after welding, the excess third clasp and the fourth clasp are cut off, the weld joint is polished flat, thereby achieving fixed connection between the second fixed mounting member and the other end of the spring.
[0005] Further, the separation spring mounting structure comprises a plurality of threaded connecting members, the second fixed mounting member has a plurality of second mounting holes, the tail cover body has a plurality of threaded connecting holes, the plurality of threaded connecting members, the plurality of second mounting holes and the plurality of threaded connecting holes are arranged one-to-one.
[0006] Further, the threaded connecting member comprises a screw.
[0007] Further, the spring is a helical compression spring, and the material of the spring comprises spring steel.
[0008] Further, the material of the first and second fixed mounting members comprises aluminum alloy, titanium alloy, steel or high-temperature alloy.
[0009] Further, the material of the threaded connecting member comprises aluminum alloy, titanium alloy, steel or high-temperature alloy.
[0010] Further, the thickness of the first and second fixed mounting members is 0.2mm to 5mm.
[0011] According to another aspect of the present application, a boost vehicle is provided, which comprises a separation spring mounting structure as described above and a tail cover body, the separation spring mounting structure being arranged on the tail cover body.
[0012] Further, the tail cover body has a spring accommodating cavity, the threaded connecting hole is arranged on the cavity bottom surface of the spring accommodating cavity, and the separation spring mounting structure is arranged in the spring accommodating cavity.
[0013] Further, the boost vehicle comprises a plurality of separation spring mounting structures, the tail cover body has a plurality of spring accommodating cavities, and the plurality of separation spring mounting structures are arranged one by one in the plurality of spring accommodating cavities.
[0014] The technical scheme of the present application provides a separation spring mounting structure for a boost vehicle, which is arranged by providing a first fixed mounting member and a second fixed mounting member, and the two ends of the spring are connected with the first and second fixed mounting members respectively, wherein the spring is fixed with the mounting members through buckle bending welding on the mounting member and special welding at the tail end of the spring, which can effectively prevent the spring from rotating, and when mounted, the threaded connecting member passes through the first mounting hole of the first fixed mounting member into the inside of the spring, and is connected with the tail cover body through the second mounting hole of the second fixed mounting member, which realizes reliable mounting of the separation spring on the tail cover, satisfies synchronous movement of the spring and the tail cover under spring compression and release actions, and realizes convenient disassembly and assembly of the tail cover and the spring, and can well realize separation action of the boost vehicle and the tail cover. Meanwhile, since the structure shape of the present application is not limited, it has strong adaptability and can be suitable for tail cover separation of various boost vehicles. Therefore, compared with the prior art, the separation spring mounting structure for the boost vehicle can effectively solve the spring mounting problem, the spring is reliably fixed with the connected member, convenient disassembly and assembly and good connection effect are realized, and it is suitable for installation requirements in the field of high-speed vehicles. BRIEF DESCRIPTION OF DRAWINGS
[0015] The accompanying drawings, which are included to provide a further understanding of the embodiments of the application and are incorporated in and constitute a part of this specification, illustrate embodiments of the application and together with the description serve to explain the principles of the application. It is understood that the drawings are for purposes of illustrating the concepts of the application and are not intended to limit the scope of the application. It is further understood that the drawings can not be to scale and that, unless otherwise specifically mentioned, the drawings are merely intended to conceptually illustrate aspects of the application.
[0016] Figure 1 An exploded structural schematic diagram of a separate spring mounting structure on a tail cover body is shown according to a specific embodiment of the present application;
[0017] Figure 2 A structural schematic diagram of a first fixed mounting member is shown according to a specific embodiment of the present application;
[0018] Figure 3 A structural schematic diagram of a second fixed mounting member is shown according to a specific embodiment of the present application;
[0019] Figure 4 A longitudinal cross-sectional structural schematic diagram of a separate spring mounting structure on a tail cover body is shown according to a specific embodiment of the present application.
[0020] Figure 5 A first fixed mounting member and a spring end rotationally fixed welding point schematic diagram is shown according to a specific embodiment of the present application.
[0021] The above-mentioned drawings include the following reference signs:
[0022] 10, first fixed mounting member; 11, first fixed mounting base; 11a, first bevel; 11b, second bevel; 12, first buckle; 13, second buckle; 10a, first mounting hole; 20, second fixed mounting member; 20a, second mounting hole; 21, second fixed mounting base; 21a, third bevel; 21b, fourth bevel; 22, third buckle; 23, fourth buckle; 30, spring; 40, threaded connecting member; 100, separate spring mounting structure; 200, tail cover body; 200a, spring accommodating cavity; 200b, threaded connecting hole; 51, rotationally fixed point. DETAILED DESCRIPTION
[0023] It should be noted that the embodiments and features of the embodiments in the present application can be combined with each other in the case of no conflict. The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings of the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments of the present application. The description of the at least one exemplary embodiment is actually only illustrative, but not as any limitation to the present application and its application or use. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative work under the premise that there is no conflict, belong to the scope of protection of the present application.
[0024] It should be noted that the terms used herein are only intended to describe specific embodiments and are not intended to limit exemplary embodiments according to the present application. As used herein, the singular form is intended to include the plural form, unless the context clearly indicates otherwise, and it should be understood that, when the terms "comprise" and / or "include" are used in the specification, it indicates the presence of the features, steps, operations, devices, components and / or combinations thereof.
[0025] Unless specifically stated otherwise, the relative arrangements of the components and steps illustrated in these embodiments and the numerical expressions and values set forth herein are not limiting of the scope of the application. It should be understood that the various parts of the drawings are not necessarily drawn to scale, and that, for the purpose of convenience and clarity, not all components and steps can be shown in a given figure. Techniques, methods, and devices known to those of ordinary skill in the art can not be discussed in detail, but rather can be assumed to be known by those of ordinary skill in the art. In the examples shown and discussed herein, any specific values should be interpreted as merely illustrative of the examples, and not as a limitation of the scope of the exemplary embodiments. Other examples of the exemplary embodiments can have different values. It should be noted that like numbers and letters refer to like elements throughout the several views of the drawings and that, unless otherwise indicated, like elements in different views can not be discussed in detail in order to avoid obscuring the novelty in the present application.
[0026] As Figures 1 to 5As shown, the specific embodiment according to the present application provides a separation spring mounting structure for a boost vehicle, which comprises a first fixed mounting piece 10, a second fixed mounting piece 20, a spring 30 and a threaded connecting piece 40, the first fixed mounting piece 10 has a first mounting hole 10a, the second fixed mounting piece 20 has a second mounting hole 20a, one end of the spring 30 is connected with the first fixed mounting piece 10, the other end of the spring 30 is connected with the second fixed mounting piece 20, and the threaded connecting piece 40 is used to realize the fixed connection of the spring 30 with the tail cover body; the tail cover body has a threaded connecting hole, the threaded connecting piece 40 passes through the first mounting hole 10a, the spring 30 and the second mounting hole 20a in sequence and cooperates with the threaded connecting hole on the tail cover body to realize the fixed connection of the second fixed mounting piece 20 with the tail cover body; the first fixed mounting piece 10 has a first fixed mounting base body 11, a first buckle 12 and a second buckle 13, the first fixed mounting base body 11 has a first bevel 11a and a second bevel 11b, the first bevel 11a is oppositely arranged with the first buckle 12, and the second bevel 11b is oppositely arranged with the second buckle 13, the first buckle 12 is arranged on one side of the first fixed mounting base body 11, and the second buckle 13 is arranged on the other side of the first fixed mounting base body 11, when connected, the first buckle 12 and the second buckle 13 wrap one end of the spring 30 by one turn of the spring, the free end of the first buckle 12 is welded with the first fixed mounting base body 11 at the first bevel 11a, and the free end of the second buckle 13 is welded with the first fixed mounting base body 11 at the second bevel 11b, after the welding is completed, the first buckle 12 and the second buckle 13 which are too long are cut off, and the welding seam part is polished flat, so as to realize the fixed connection between the first fixed mounting piece 10 and one end of the spring; the second fixed mounting piece 20 has a second fixed mounting base body 21, a third buckle 22 and a fourth buckle 23, the second fixed mounting base body 21 has a third bevel 21a and a fourth bevel 21b, the third bevel 21a is oppositely arranged with the third buckle 22, and the fourth bevel 21b is oppositely arranged with the fourth buckle 23, the third buckle 22 is arranged on one side of the second fixed mounting base body 21, and the fourth buckle 23 is arranged on the other side of the second fixed mounting base body 21, the third buckle 22 cooperates with one side of the spring 30, and the fourth buckle 23 cooperates with the other side of the spring 30, when connected, the third buckle 22 and the fourth buckle 23 wrap the other end of the spring 30 by one turn of the spring, the free end of the third buckle 22 is welded with the second fixed mounting base body 21 at the third bevel 21a, and the free end of the fourth buckle 23 is welded with the second fixed mounting base body 21 at the fourth bevel 21b, after the welding is completed, the third buckle 22 and the fourth buckle 23 which are too long are cut off, and the welding seam part is polished flat, so as to realize the fixed connection between the second fixed mounting piece 20 and the other end of the spring.
[0027] With the configuration, the separation spring mounting structure for the boost vehicle is provided, the two ends of the spring are connected with the first fixing mounting member and the second fixing mounting member respectively by setting the first fixing mounting member and the second fixing mounting member, the spring is fixed with the mounting member through the buckle bending welding on the mounting member and the special welding of the tail end of the spring, the rotation of the spring can be effectively prevented, during the mounting, the threaded connecting member passes through the first mounting hole of the first fixing mounting member and enters the inside of the spring, and is connected with the tail cover body through the second mounting hole of the second fixing mounting member, the reliable mounting of the separation spring on the tail cover is realized, the synchronous movement of the spring and the tail cover under the compression and release actions of the spring is realized, the convenient disassembly and assembly of the tail cover and the spring are realized, and the separation action of the boost vehicle and the tail cover can be well realized. Meanwhile, since the structure shape of the present application is not limited, the adaptability is high, and the tail cover separation of various boost vehicles can be adapted. Therefore, compared with the prior art, the separation spring mounting structure for the boost vehicle can effectively solve the spring mounting problem, the spring and the connected member are fixed reliably, the disassembly and assembly are convenient, the connection effect is good, and the mounting demand in the field of high-speed vehicles can be met.
[0028] Specifically, in the present application, the base bodies of the first fixing mounting member 10 and the second fixing mounting member 20 are welded with the end of the spring, the welding point area is adjusted according to the spring parameters, and the welding current and the welding time are controlled according to the thermal conductivity of the spring. The welding point is used to prevent the rotation of the spring; in this configuration, the first buckle and the second buckle are arranged on the first fixing mounting base body 11, when it is needed to be fixedly connected with one end of the spring, a certain external force is applied to make the first buckle and the second buckle tightly wrap the last circle of the spring, then the free end of the buckle and the base body are welded at the bevel reserved on the base body, the excess buckle is cut off, and the welding seam part is polished flat. The first buckle and the second buckle can clamp the spring, so that the fixed connection between the first fixing mounting member and one end of the spring is realized; similarly, the third buckle and the fourth buckle are arranged on the second fixing mounting base body 21, when it is needed to be fixedly connected with the other end of the spring, a certain external force is applied to make the third buckle and the fourth buckle tightly wrap the last circle of the spring, then the free end of the buckle and the base body are welded at the bevel reserved on the base body, the excess buckle is cut off, and the welding seam part is polished flat. So that the fixed connection between the second fixing mounting member and the other end of the spring is realized.
[0029] As a specific embodiment of the present application, as Figure 1As shown, the separation spring mounting structure for the boost vehicle includes a first fixed mounting member 10, a second fixed mounting member 20, a spring 30, and a threaded connecting member 40, in this embodiment, a screw is used as the threaded connecting member 40, the tail cover body 200 has a spring accommodating cavity 200a, threaded connecting holes 200b are arranged on the cavity bottom surface of the spring accommodating cavity 200a, and the separation spring mounting structure is arranged in the spring accommodating cavity 200a. When the spring is mounted, the screw passes through the first mounting hole 10a, the spring 30, and the second mounting hole 20a in sequence and is matched with the threaded connecting hole on the tail cover body to realize the fixed connection of the spring 30 and the tail cover body.
[0030] Further, in order to improve the connection reliability between the spring and the tail cover body, the separation spring mounting structure can be configured to include a plurality of threaded connecting members 40, the second fixed mounting member 20 has a plurality of second mounting holes 20a, the tail cover body has a plurality of threaded connecting holes, and the plurality of threaded connecting members 40, the plurality of second mounting holes 20a, and the plurality of threaded connecting holes are arranged one-to-one.
[0031] In this configuration, the first threaded connecting member passes through the first mounting hole 10a, the spring 30, and the second mounting hole 20a in sequence and is matched with the first threaded connecting hole on the tail cover body, the second threaded connecting member passes through the first mounting hole 10a, the spring 30, and the second mounting hole 20a in sequence and is matched with the second threaded connecting hole on the tail cover body, and so on, until the Nth threaded connecting member passes through the first mounting hole 10a, the spring 30, and the second mounting hole 20a in sequence and is matched with the Nth threaded connecting hole on the tail cover body, which can greatly improve the connection reliability between the spring and the tail cover body.
[0032] Further, in the present application, the tail cover body 200 can be made of aluminum alloy, titanium alloy, steel, high-temperature alloy, etc. The structural surface is spherical, ellipsoidal, parabolic, or other required surface.
[0033] In addition, considering the structural strength and use reliability, the spring 30 is a spiral compression spring, and the material of the spring 30 includes spring steel. The spring parameters can be selected according to the spring manual and use conditions.
[0034] Further, in the present application, considering the structural strength and use reliability of the fixed mounting member, the material of the first fixed mounting member 10 and the second fixed mounting member 20 can be configured to include aluminum alloy, titanium alloy, steel, or high-temperature alloy. The thickness of the first fixed mounting member 10 and the second fixed mounting member 20 is 0.2mm to 5mm. The outer diameter of the first fixed mounting member 10 and the second fixed mounting member 20 is adapted to the size of the spring, that is, the outer diameter of the first fixed mounting member 10 and the second fixed mounting member 20 is the same as or slightly larger than the outer diameter of the spring.
[0035] In addition, in the present application, in order to ensure the reliability of the connection, the material of the threaded connection 40 can be configured to include aluminum alloy, titanium alloy, steel or high-temperature alloy.
[0036] As a specific embodiment of the present application, one or more separation spring mounting structures can be mounted on the tail cover body 200 as needed, and a cylindrical groove is designed at the position of each separation spring mounting structure, the groove diameter gap is 0.5mm to 20mm with the outer diameter of the cylindrical spring, and a threaded connection hole 200b is arranged on the bottom platform of the groove, the size of the threaded connection hole 200b is M3 to M10. A first mounting hole 10a is arranged on the first fixed mounting part 10, the hole diameter of the first mounting hole 10a is 5mm to 30mm, and the first fixed mounting part 10 is provided with a first buckle and a second buckle, which are used to realize the fixed connection between the first fixed mounting part and the spring.
[0037] One or more second mounting holes 20a are arranged on the second fixed mounting part 20, the hole diameter of the second mounting hole 20a is 3mm to 10mm, and the second fixed mounting part 20 is provided with a third buckle and a fourth buckle, which are used to realize the fixed connection between the second fixed mounting part and the spring. The threaded connection part 40 is a screw, and the thread size of the screw is selected to be M3 to M10. The corresponding first fixed mounting part 10 and the second fixed mounting part 20 are selected to have a hole diameter size corresponding to the screw. The screw can be a slot screw, an internal hexagonal screw, etc.
[0038] The first fixed mounting part 10 and the second fixed mounting part 20 are first mounted together with the spring, one end of the second fixed mounting part 20 enters the cylindrical spring accommodating cavity 200a of the tail cover body 200, the screw enters the inside of the spring through the first mounting hole of the first fixed mounting part 10, and the second fixed mounting part 20 is connected with the tail cover body 200 by screwing through the second mounting hole on the second fixed mounting part 20, and the installation tool enters the first mounting hole of the first fixed mounting part 10 to tighten the screw, thereby realizing the fixed connection between the spring and the tail cover body.
[0039] According to another aspect of the present application, a kind of aircraft is provided, which includes separation spring mounting structure 100 and tail cover body 200, separation spring mounting structure 100 is as shown in the above separation spring mounting structure 100, separation spring mounting structure 100 is arranged on tail cover body 200.
[0040] With the configuration, the aircraft is provided. The separation spring mounting structure provided by the application is configured by the first fixing mounting member and the second fixing mounting member, the two ends of the spring are connected with the first fixing mounting member and the second fixing mounting member respectively, during installation, the threaded connecting member passes through the first mounting hole of the first fixing mounting member and enters the inside of the spring, and is connected with the tail cover body through the second mounting hole of the second fixing mounting member. The reliable installation of the separation spring on the tail cover is realized, the synchronous movement of the spring and the tail cover under the compression and release of the spring is realized, the convenient disassembly and assembly of the tail cover and the spring are realized, and the separation of the boost aircraft and the tail cover is realized. In addition, the structure of the application is not limited, and is suitable for the tail cover separation of various boost aircrafts. Therefore, the separation spring mounting structure provided by the application is applied to the boost aircraft, and the working performance of the boost aircraft is greatly improved.
[0041] Further, in the application, in order to realize the reliable installation of the separation spring mounting structure on the tail cover body and improve the stability of the connection between the separation spring mounting structure and the tail cover body, the tail cover body 200 has a spring accommodating cavity 200a, the threaded connecting hole 200b is arranged on the cavity bottom surface of the spring accommodating cavity 200a, and the separation spring mounting structure is arranged in the spring accommodating cavity 200a.
[0042] In order to further improve the reliability of the connection between the separation spring mounting structure and the tail cover body, the aircraft can be configured to include a plurality of separation spring mounting structures 100, the tail cover body has a plurality of spring accommodating cavities 200a, and the plurality of separation spring mounting structures 100 are arranged in the plurality of spring accommodating cavities 200a one by one.
[0043] In order to further understand the application, the following will be combined with Figures 1 to 5 The separation spring mounting structure for the boost aircraft provided by the application is described in detail.
[0044] As Figures 1 to 5 shown, according to the specific embodiment of the application, a separation spring mounting structure for a boost aircraft is provided, which includes a first fixing mounting member 10, a second fixing mounting member 20, a spring 30 and a threaded connecting member 40. In the embodiment, the first fixing mounting member 10 and the second fixing mounting member 20 are both in a round plate structure, the threaded connecting member 40 is a screw, and the first mounting hole 10a and the second mounting hole 20a are both circular holes.
[0045] The tail cover body 200 and the second fixed mounting member 20 are mounted together, the two ends of the spring 30 are respectively mounted with the second fixed mounting member 20 and the first fixed mounting member 10, and the screw is connected together the second fixed mounting member 20 and the tail cover body 200 through the round hole on the second fixed mounting member 20; the separation spring mounting structure is located inside the spring containing cavity 200a of the tail cover body.
[0046] The tail cover body 200 is made of aluminum alloy material, and the structure surface of the tail cover body 200 is a spherical surface. The spring 30 is made of spring steel material. The second fixed mounting member 20 can be made of aluminum alloy material, with a thickness of 1 mm and an outer diameter of 40 mm. The first fixed mounting member 10 can be made of aluminum alloy material, with a thickness of 1 mm and an outer diameter of 50 mm. The screw can be made of steel material.
[0047] The spring 30 is a spiral compression spring. The effective number of turns is 6.5, the total number of turns is 8.5, the material diameter is 3.5 mm, the spring diameter is 35 mm, the free length is 90 mm, the working stroke is 57 mm, and the stiffness is 5.3 N / mm.
[0048] Two springs 30 are mounted on the tail cover body 200, and a cylindrical groove is designed as a spring containing cavity at the position of each spring 30. The gap between the groove diameter and the outer diameter of the cylindrical spring is 3 mm, and two threaded holes are provided on the bottom platform of the groove, with a size of M5.
[0049] The second fixed mounting member 20 is provided with two round holes with a diameter of 5 mm. The second fixed mounting member 20 has two flange ears for fixing the spring. The first fixed mounting member 10 is provided with one round hole with a diameter of 10 mm. The first fixed mounting member 10 has two buckles for fixing the spring.
[0050] The size of the screw is selected as M5. The screw is a one-way slot screw.
[0051] The second fixed mounting member 20 and the first fixed mounting member 10 are first mounted together with the spring 30. One end of the second fixed mounting member 20 enters the cylindrical groove of the tail cover body 200, the screw enters the inside of the spring through the round hole of the first fixed mounting member 10, and the screw connection between the second fixed mounting member 20 and the tail cover body 200 is realized through the two round holes on the second fixed mounting member 20. The installation tool enters the round hole of the first fixed mounting member 10 to tighten the screw, realizing the fixed connection between the spring and the tail cover body.
[0052] In this configuration, the first fixed mounting base 11 is provided with a first buckle 12 and a second buckle 13, when it is necessary to be fixedly connected with one end of the spring, a certain external force is applied to tightly wrap the last coil of the spring with the first buckle and the second buckle, then the free end of the buckle is welded with the base at the bevel reserved on the base, the excess buckle is cut off, and the welding seam is polished flat. The first buckle 12 and the second buckle 13 can clamp the spring, so as to realize the fixed connection between the first fixed mounting part and one end of the spring; similarly, the second fixed mounting base 21 is provided with a third buckle 22 and a fourth buckle 23, when it is necessary to be fixedly connected with the other end of the spring, a certain external force is applied to tightly wrap the last coil of the spring with the third buckle 22 and the fourth buckle 23, then the free end of the buckle is welded with the base at the bevel reserved on the base, the excess buckle is cut off, and the welding seam is polished flat. Thus, the fixed connection between the second fixed mounting part and the other end of the spring is realized.
[0053] In this configuration, the base of the first fixed mounting part 10 and the base of the second fixed mounting part 20 are welded with the end of the spring to form a rotary fixed point 51, the diameter of the welding point is 3mm, the welding current is 20A, and the welding time is 2 seconds. The welding point is used to prevent the spring from rotating.
[0054] In summary, the present application provides a separation spring mounting structure of an aircraft, which can realize reliable installation of the separation spring on the tail cover, and well realizes the separation action of the boost aircraft and the tail cover. At the same time, since the structure shape of the present application is not limited, it has strong adaptability and can be suitable for the tail cover separation of various boost aircrafts. Compared with the prior art, the present application has the following beneficial effects.
[0055] (1) The present application realizes the effective connection of the tail cover and the separation spring, realizes the synchronous movement of the spring and the tail cover under the condition of meeting the spring compression and release action, and realizes the convenient disassembly and assembly of the tail cover and the spring.
[0056] (2) The welding buckle of the present application bears the tension and the tail end welding of the spring prevents rotation, which is the first in the industry and can solve the related spring connection and release problems.
[0057] (3) The tail cover and the separation spring mounting scheme of the present application have wide application range and can be popularized to other aircrafts.
[0058] For purposes of the description hereinafter, spatial or directional terms, for example, "above", "below", "upper", "lower", and the like, can be used, and relate to the device as illustrated in the figures. However, it is to be understood that no absolute or relative orientation of the device is intended or implied, unless specifically described as such. Terms concerning attachments, coupling and the like, such as "connected" and "coupled" and the like, are to be construed in accordance with their normal meanings, that is, as referring to an indirect or direct connection or coupling. Any reference to "comprising" or "containing" is to be construed as meaning "comprising or containing, but not limited to". Any reference to "comprising" or "containing" is to be construed as meaning "comprising or containing, but not limited to".
[0059] In addition, it should be pointed out that the use of the terms "first", "second" and the like, to describe various elements, is merely intended to differentiate the elements from one another, and does not connote any special order or order of precedence, unless otherwise specifically indicated. Thus, the use of the terms "first", "second" and the like, is not intended to limit the scope of the present application, and is not intended to connote any special order or order of precedence.
[0060] The preferred embodiments herein disclosed are not intended to limit or restrict the scope of the application, but merely convey the best mode contemplated by the inventors of carrying out the claimed application. Modifications can be made by those skilled in the art, which yet fall within the scope of the present application. Therefore, it is, therefore, to be understood that any variations made to the application are to be considered as being within the scope of the present application as defined by the appended claims, if any, and their equivalents.
Claims
1. A separation spring mounting structure for a boost vehicle, characterized by, The separation spring mounting structure comprises: a first fixed mounting member (10) having a first mounting hole (10a); a second fixed mounting member (20) having a second mounting hole (20a); a spring (30) having one end connected to the first fixed mounting member (10) and the other end connected to the second fixed mounting member (20); a threaded connecting member (40) for fixedly connecting the spring (30) to the tail cover body; the tail cover body has a threaded connecting hole, the threaded connecting member (40) passes through the first mounting hole (10a), the spring (30) and the second mounting hole (20a) in sequence and is matched with the threaded connecting hole on the tail cover body to achieve the fixed connection of the second fixed mounting member (20) to the tail cover body; the first fixed mounting member (10) has a first fixed mounting base (11), a first clasp (12) and a second clasp (13), the first fixed mounting base (11) has a first bevel (11a) and a second bevel (11b), the first bevel (11a) is arranged opposite to the first clasp (12), the second bevel (11b) is arranged opposite to the second clasp (13), the first clasp (12) is arranged on one side of the first fixed mounting base (11), the second clasp (13) is arranged on the other side of the first fixed mounting base (11), when connected, the first clasp (12) and the second clasp (13) wrap one end of the spring (30) by one turn of the spring, the free end of the first clasp (12) is welded to the first fixed mounting base (11) at the first bevel (11a), the free end of the second clasp (13) is welded to the first fixed mounting base (11) at the second bevel (11b), after the welding is completed, the first clasp (12) and the second clasp (13) that are too long are cut off, the weld joint is polished flat, thereby achieving the fixed connection between the first fixed mounting member (10) and one end of the spring. The second fixed mounting member (20) has a second fixed mounting base (21), a third buckle (22) and a fourth buckle (23), the second fixed mounting base (21) has a third bevel (21a) and a fourth bevel (21b), the third bevel (21a) is arranged opposite to the third buckle (22), the fourth bevel (21b) is arranged opposite to the fourth buckle (23), the third buckle (22) is arranged on one side of the second fixed mounting base (21), the fourth buckle (23) is arranged on the other side of the second fixed mounting base (21), the third buckle (22) cooperates with one side of the spring (30), the fourth buckle (23) cooperates with the other side of the spring (30), when connected, the third buckle (22) and the fourth buckle (23) wrap one circle of the spring at the other end of the spring (30), the free end of the third buckle (22) is welded with the second fixed mounting base (21) at the third bevel (21a), the free end of the fourth buckle (23) is welded with the second fixed mounting base (21) at the fourth bevel (21b), after welding, the third buckle (22) and the fourth buckle (23) that are too long are cut off, and the welding position is polished flat, so that the fixed connection between the second fixed mounting member (20) and the other end of the spring is realized.
2. The separation spring mounting structure for a boost vehicle according to claim 1, characterized by, The separation spring mounting structure comprises a plurality of threaded connecting members (40), the second fixed mounting member (20) has a plurality of second mounting holes (20a), and the tail cover body has a plurality of threaded connecting holes, and the plurality of threaded connecting members (40), the plurality of second mounting holes (20a) and the plurality of threaded connecting holes are arranged in one-to-one correspondence.
3. The separation spring mounting structure for a boost vehicle according to claim 2, characterized by, The threaded connecting member (40) comprises a screw.
4. The separation spring mounting structure for a boost vehicle according to claim 3, characterized by The spring (30) is a spiral compression spring, and the material of the spring (30) comprises spring steel.
5. The separation spring mounting structure for a boost vehicle according to claim 4, characterized by The materials of the first fixed mounting member (10) and the second fixed mounting member (20) comprise aluminum alloy, titanium alloy, steel or high-temperature alloy.
6. The separation spring mounting structure for a boost vehicle according to any one of claims 1 to 5, characterized by, The material of the threaded connecting member (40) comprises aluminum alloy, titanium alloy, steel or high-temperature alloy.
7. The separation spring mounting structure for a boost vehicle according to claim 6, characterized by The thicknesses of the first fixed mounting member (10) and the second fixed mounting member (20) are both 0.2mm to 5mm.
8. A boost-glider characterized by, The boost aircraft comprises a separation spring mounting structure (100) and a tail cover body (200), the separation spring mounting structure (100) is the separation spring mounting structure (100) as claimed in claims 1 to 7, and the separation spring mounting structure (100) is arranged on the tail cover body (200).
9. The boost vehicle of claim 8, wherein, The tail cover body (200) has a spring accommodating cavity (200a), the threaded connecting hole (200b) is arranged on the cavity bottom surface of the spring accommodating cavity (200a), and the separation spring mounting structure is arranged in the spring accommodating cavity (200a).
10. The boost vehicle of claim 9, wherein, The boost vehicle includes a plurality of the separation spring mounting structures (100), and the tail cover body has a plurality of spring accommodating cavities (200a), and the plurality of separation spring mounting structures (100) are arranged one by one in the plurality of spring accommodating cavities (200a).