Unmanned ultra-high-speed naval vessel power system mounting rack

By designing an installation platform for the unmanned ultra-high-speed ship power system, the problems of stable installation of aero engines on unmanned ships and rapid installation of testing platforms were solved, enabling stable operation and convenient replacement of engines and extending equipment life.

CN223604329UActive Publication Date: 2025-11-28HEBEI HANGUANG HEAVY IND
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Patent Information

Application Number
CN202422972292.7
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-12-03
Publication Date
2025-11-28
Estimated Expiration
2034-12-03

AI Technical Summary

Technical Problem

In the current technology, it is difficult to securely install aircraft engines on unmanned vessels, and the stable performance of the engines cannot be guaranteed during operation. At the same time, there is a lack of test platforms for rapid installation and convenient replacement.

Method used

An installation platform for the power system of an unmanned ultra-high-speed vessel was designed, including a fixed bracket, a support frame, and a shock-absorbing bracket. It adopts a modular design and uses high-strength bolts and shock absorbers to disperse impact forces, ensuring the stable installation and rapid replacement of the engine.

Benefits of technology

It has enabled the stable installation of aero engines on unmanned vessels, improved the stability and convenience of the testing process, extended the service life of the engine and the vessel, and enabled the rapid replacement and interchangeability of the installed components.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model belongs to the field of unmanned superspeed naval vessel power systems, and particularly relates to an unmanned superspeed naval vessel power system installation rack. The utility model provides an unmanned ultra-high-speed ship power system mounting rack which can stably mount an aero-engine on an ultra-high-speed unmanned ship and further test the application possibility of the aero-engine in the field of ultra-high-speed unmanned ship power systems. The unmanned ultra-high-speed naval vessel power system installation rack comprises a fixed support, a supporting framework and a damping support. The fixing support is of a hollow structure, and the power system is contained in the fixing support. The supporting framework is used for supporting the fixing support and the damping support. The damping support is coaxially connected to the front end face of the fixing support and used for installing a damper. The front end of the power system faces the damping support. According to the mounting rack, the impact force borne by the mounting rack can be effectively reduced, then impact damage of the mounting rack to a naval vessel is reduced, and the service life of the engine mounting rack and the service life of the naval vessel are prolonged.
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Description

TECHNICAL FIELD

[0001] The utility model belongs to the unmanned super -high -speed warship power system field, concretely relates to a kind of unmanned super -high -speed warship power system installation rack. BACKGROUND

[0002] In view of the urgent demand of super -high -speed unmanned warship in our country, carry out the application test research of retired aeroengine modified super -high -speed unmanned warship, focus on solving the problem of low speed, weak mobility, high cost of unmanned warship, overall achieve the goal of super -high -speed, high mobility, large range, long time of sailing to execute tactical task, with lower cost, quickly make up the deficiency of our army in asymmetric warfare (asymmetric warfare refers to the small party to make up for the disparity in strength and adopt a kind of irregular, asymmetric combat mode, it emphasizes the realization of strategic purpose by using non-military means and non-military targets), improve the combat capability on sea.

[0003] Because previous aeroengine in our country belongs to the control field, domestic scientific research institutes and enterprises are difficult to obtain aeroengine, therefore, our country only has unmanned warship of traditional propulsion mode, and there is no test platform, standard and entity of jet propulsion warship research. There is no relevant report in prior art document, the utility model is the preliminary attempt in the field.

[0004] Utilize the advantages (reserve engine main structure, oil, anti-icing, leak oil system, ensure that engine works normally) such as high thrust-to-weight ratio, high speed, large thrust of aeroengine, use unmanned warship as platform carrier, carry out intelligentization, automation transformation of retired aeroengine, and then carry out systematic integration with unmanned warship, so that ordinary low-speed unmanned warship becomes super -high -speed unmanned warship. But in the process of using aeroengine for super -high -speed unmanned warship test, there are many technical problems to be solved, for example, how to stably install aeroengine on super -high -speed unmanned warship, how to ensure that aeroengine has high stability during operation, how to ensure that the rack supporting engine can be quickly installed during test, and the installation parts can be conveniently replaced.

[0005] New type of a device for the production of a beverage

[0006] The utility model provides a kind of unmanned super -high -speed warship power system installation rack, can stably install aeroengine on super -high -speed unmanned warship, and then test the possibility of application of aeroengine in super -high -speed unmanned warship power system field.

[0007] The unmanned super -high -speed warship power system installation rack includes: fixed support, support framework and shock-absorbing support;Wherein, the fixed support is hollow structure, and its inside contains power system;

[0008] The support framework is used to support fixed support and shock-absorbing support.

[0009] The damping support is coaxially connected to the front end surface of the fixed support, and is used for mounting the damper;

[0010] The front end of the power system faces the damping support.

[0011] Preferably, the damping support is a conical frustum frame structure; the conical frustum frame structure comprises a plurality of annular structures coaxially and spaced along the axial direction; the diameters of the annular structures decrease from the rear to the front.

[0012] The adjacent two layers of the annular structures are connected through a plurality of damping dampers uniformly distributed along the circumferential direction.

[0013] Preferably, the fixed support comprises a fixed support upper module and a fixed support lower module,

[0014] The fixed support upper module and the fixed support lower module are both frame structures with a semicircular cross section, and the fixed support upper module and the fixed support lower module are butt-jointed to form a complete cylindrical frame structure.

[0015] The semicircular frame structure comprises a plurality of sector structures spaced along the axial direction and a plurality of rectangular tubes used for connecting the sector structures.

[0016] Preferably, the upper end surface of the support framework is connected to the fixed support lower module through a connecting plate and a fastener.

[0017] Preferably, a plurality of hinged supports are arranged along the circumferential direction of the inner side of the fixed support.

[0018] Each of the hinged supports is provided with a hinge hole.

[0019] The hinge holes correspond to the hinge points on the circumferential wall of the power system in a one-to-one manner, and are fastened and connected.

[0020] Preferably, the fixed support, the support framework and the damping support are all welded with rectangular tubes.

[0021] Preferably, the power system is an aero-engine.

[0022] Preferably, a fixed mounting structure is arranged on the rear end surface of the fixed support.

[0023] The fixed mounting structure is machined with a conical surface matched with the rear end conical surface of the power system, so as to ensure that the mounting rack is firmly and reliably mounted with the power system.

[0024] Beneficial effects

[0025] (I) the installation rack includes shock-absorbing supports, provides a shock-absorbing structure for the installation rack, and is used for dispersing impact force generated by a power system to a support framework and a ship body, so that the impact force received by the installation rack can be effectively reduced, the impact damage of the installation rack to the ship is reduced, and the service life of the engine installation rack and the ship is prolonged.

[0026] (II) the installation rack adopts a modular design, includes a fixed support upper module and a fixed support lower module of a fixed support, a support framework and shock-absorbing supports; the modules are quickly assembled between each other, maintenance and replacement are simple and convenient, and the interchangeability of the installation rack is greatly improved. Moreover, the modular design is beneficial to realizing weight adjustment of the whole installation rack,

[0027] balance between strength and light weight is realized, and the reliability of overall connection is ensured.

[0028] (III) the support framework is a main supporting component of the installation rack, the support framework and the fixed support lower module are provided with a connecting plate, a fastener (including a high-strength connecting bolt) is used to make the fixed support and the support framework form an integral whole, and the stability of the whole installation rack is improved.

[0029] (IV) the whole installation rack is welded after being cut and bent from a standard rectangular pipe, so that the bearing capacity of the installation rack can be ensured; the support framework, the fixed support and the shock-absorbing supports are connected and fastened by high-strength bolts, so that the overall structural strength is ensured.

[0030] (V) the fixed installation structure of the installation rack is processed with a conical surface that is matched with a conical surface at the rear end of a power system, so as to ensure that the installation rack is firmly and reliably installed with the power system. BRIEF DESCRIPTION OF DRAWINGS

[0031] Figure 1 it is an overall installation schematic view of the installation rack;

[0032] Figure 2 it is an overall frame schematic view of the installation rack;

[0033] Figure 3 it is a support framework structure schematic view;

[0034] Figure 4 it is a fixed support lower module structure schematic view;

[0035] Figure 5 it is a fixed support upper module structure schematic view;

[0036] Figure 6 it is a shock-absorbing support overall structure schematic view;

[0037] Figure 7 it is an engine installation structure schematic view;

[0038] Figure 8 It is a fixed support rear end surface sector structure schematic diagram;

[0039] Figure 9 It is a fixed support front end surface sector structure schematic diagram;

[0040] Figure 10 It is a fixed support middle sector module structure schematic diagram;

[0041] Figure 11 It is a fixed support fixed installation structure schematic diagram;

[0042] Figure 12 It is a first stage damping structure corresponding annular structure schematic diagram;

[0043] Figure 13 It is a first stage damping structure corresponding annular structure schematic diagram;

[0044] Figure 14 It is a third stage damping structure corresponding annular structure schematic diagram;

[0045] Figure 15 It is a two kinds of connecting plate structure schematic diagram;

[0046] 1-fixed support, 2-support framework, 3-damping support, 4-power system, 5-fixed installation structure, 6-connecting plate, 7-hinged support, 8-hinge hole, 9-hinge point, 10-damper installation hinge hole, 1-1-fixed support upper module, 1-2-fixed support lower module, 1-3-sector structure, 1-4-rectangular pipe, 3-1-annular structure, 3-2-damping damper. DETAILED DESCRIPTION

[0047] The utility model will be further described below in combination with the drawings and specific embodiments. Figures 1-15

[0048] The embodiment provides a kind of unmanned super-speed warship power system installation rack, which includes support framework 2, fixed support 1, damping support 3.The fixed support 1 is hollow frame structure, and its inside contains power system 4 (including various aeroengines);The front end surface of fixed support 1 is connected with damping support 3, and support framework 2 is supported below fixed support 1 and damping support 3, and plays the role of supporting stability.The damping support 3 is the frame structure of cone frustum, and fixed support 1 is cylindrical structure (can be adjusted according to aeroengine appearance, for example, form cone structure), and the rear end surface of damping support 3 is coaxially connected with the front end surface of fixed support 1 (i.e. damping support 3 is installed at the forefront of overall structure).

[0049] ​The front end of the power system 4 is close to the damping support 3, and the damping support 3 is used to reduce the impact force at the starting moment and the acceleration moment of the power system 4, so that the impact force received by the mounting rack can be effectively reduced, the impact damage of the mounting rack to the warship is further reduced, and the service life of the mounting rack and the warship is further prolonged.

[0050] As an example, the support angle of the fixed support 1 on the support framework 2 (that is, the angle between the axis of the fixed support 1 and the horizontal direction) needs to be determined according to the internal structure and space of the unmanned warship.

[0051] The mounting rack as a whole is welded after being cut and bent from standard rectangular pipes 1-4, so that the bearing capacity of the mounting rack can be ensured, and the support framework 2, the fixed support 1 and the damping support 3 are connected and fastened by high-strength bolts, so that the overall structural strength is ensured.

[0052] The damping support 3 is the main damping structure in the mounting rack, and the damping support 3 includes a plurality of coaxial and axially spaced annular structures 3-1, the diameters of the annular structures 3-1 gradually decrease from back to front (the sizes of the annular structures 3-1 gradually decrease step by step); the adjacent two layers of annular structures 3-1 are connected by a plurality of circumferentially uniformly spaced damping shock absorbers 3-2, thereby forming a frustoconical frame structure; specifically, the annular structure 3-1 is provided with a damper mounting hinge hole 10, and the two ends of the damping shock absorber 3-2 are respectively connected to the corresponding damper mounting hinge hole 10. The damping shock absorber 3-2 is an important damping component in the damping support 3, which is used to ensure the stable state between the power system 4 and the unmanned warship.

[0053] As an example, the mounting rack adopts a two-stage damping structure (that is, the damping support 3 includes three coaxial and spaced annular structures 3-1, thereby spacing and clamping two layers of damping shock absorbers 3-2), the first annular structure has the largest diameter size, which is consistent with the size of the front end face of the fixed support 1, and a plurality of mounting fixing holes are processed on the first annular structure in the circumferential direction, which are used to connect the damping support 3 and the support framework 2 firmly. The diameter of the second annular structure is smaller than that of the first annular structure. For the third annular structure, high-strength bolt connection is adopted between the third annular structure and the support framework 2, and the bolt mounting hole needs to be made on site during actual installation.

[0054] The damping support 3 is used to disperse the forward or backward impact force generated by the engine at the starting, accelerating and decelerating moments of the power system 4 to the support framework 2 and the warship body, so that the service life of the engine mounting rack and the warship is prolonged to a certain extent.

[0055] The installation rack is designed in a modular manner. For example, the fixed support 1 comprises a fixed support upper module 1-1 and a fixed support lower module 1-2. Both the fixed support upper module 1-1 and the fixed support lower module 1-2 are frame structures with a semicircular cross section (the semicircular frame structure comprises a plurality of sector structures 1-3 arranged at intervals along the axial direction and a plurality of rectangular tubes 1-4 used for connecting the sector structures 1-3, which are welded to ensure the structural strength of the fixed support 1). The fixed support upper module 1-1 and the fixed support lower module 1-2 are oppositely open to form a complete cylindrical frame structure. The fixed support upper module 1-1 and the fixed support lower module 1-2 are connected by fasteners (including high-strength bolts) to facilitate the installation of the power system 4.

[0056] The modular design can quickly complete the overall assembly of the installation rack, improve production efficiency, and facilitate the assembly and maintenance of the modules. The modular design advantage also includes that, under the premise of ensuring the load bearing capacity and structural strength of the installation rack, the overall structure of the installation rack and the weight distribution of the parts of each module are reasonably designed through design verification and optimization design, the balance between strength and lightness is achieved, and the reliability of the overall structure connection is ensured.

[0057] The fixed mounting structure 5 is arranged on the rear end surface of the fixed support 1 to ensure the size matching, structure fitting, and fastening connection with the power system 4. The fixed mounting structure 5 is formed by the butt joint of two semicircular ring structures, which are fitted with the rear end frame of the upper and lower modules of the fixed support 1 and welded with the fixed support 1 to increase the firmness of the fixed support 1.

[0058] Because the rear end of the existing power system 4 is a cone, the contact with the installation rack is a line contact, and the local pressure is relatively large. The fixed mounting structure 5 is processed with a conical surface that fits the conical surface of the rear end of the power system 4, which can ensure the firmness and reliability of the installation of the installation rack and the power system 4. In addition, the fixed mounting structure 5 is completely matched with the conical structure of the tail of the power system 4 in size, and the rear end of the engine is firmly fixed on the fixed support 1 by welding.

[0059] The front end of the fixed support 1 is completely matched with the front end of the engine. The front end of the fixed support 1 is processed with mounting threaded holes, and the front end of the power system 4 is fastened and connected by high-strength bolts (the front end of the power system 4 itself has a certain structure, and the installation rack can be installed through the structure of the power system 4).

[0060] Between the front end and the rear end of the fixed support 1, a plurality of hinged supports 7 are arranged on the inner side in the circumferential direction, and a hinged hole 8 is arranged on each hinged support 7; a plurality of hinged points 9 are welded on the outer side wall of the power system 4 (on the premise of not affecting the function of each system reserved in the engine itself), the hinged points 9 correspond to the hinged holes 8 one by one, and the connection strength between the power system 4 and the fixed support is ensured.

[0061] The support framework 2 is the main support component of the mounting rack, a plurality of sets of connecting plates 6 are mounted on the upper end of the support framework 2 and the part where the lower module 1-2 of the fixed support contacts, the fixed support 1 and the support framework 2 are connected into a whole through fasteners (including high-strength connecting bolts) between each corresponding connecting plate 6, so that the stability of the whole mounting rack is improved. The support framework 2 is also one of the important components for connecting the power system 4 and the ship into a whole. The specific connection structure and fixing mode between the support framework 2 and the ship is determined according to the actual structure of the ship, so that the overall connection strength of the two is ensured.

[0062] In summary, the above is an embodiment of the present application, and is not used to limit the protection scope of the present application. Any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the present application shall be included in the protection scope of the present application.

Claims

1. A mounting platform for an unmanned ultra-high-speed ship propulsion system, characterized in that, It includes a fixed bracket (1), a support frame (2), and a shock-absorbing bracket (3); wherein the fixed bracket (1) is a hollow structure, and its interior houses the power system (4); The supporting frame (2) is used to support the fixed bracket (1) and the shock-absorbing bracket (3); The shock absorber bracket (3) is coaxially connected to the front end face of the fixed bracket (1) for installing the shock absorber; The front end of the power system (4) faces the shock absorber bracket (3).

2. The mounting platform for an unmanned ultra-high-speed ship propulsion system as described in claim 1, characterized in that, The shock absorber bracket (3) is a frustum-shaped frame structure; it includes several coaxial and axially spaced annular structures (3-1); the diameter of the annular structures (3-1) decreases from back to front. The two adjacent ring structures (3-1) are connected by a number of damping shock absorbers (3-2) evenly spaced along the circumference.

3. The mounting platform for an unmanned ultra-high-speed ship propulsion system as described in any one of claims 1-2, characterized in that, The fixed bracket (1) includes an upper fixed bracket module (1-1) and a lower fixed bracket module (1-2). The upper module (1-1) and lower module (1-2) of the fixed bracket are both frame structures with a semi-circular cross-section. The upper module (1-1) and lower module (1-2) of the fixed bracket are connected to form a complete columnar frame structure. The semi-circular frame structure includes several fan-shaped structures (1-3) spaced apart along the axial direction and several rectangular tubes (1-4) for connecting each fan-shaped structure (1-3).

4. The mounting platform for an unmanned ultra-high-speed ship propulsion system as described in claim 3, characterized in that, The upper end face of the support frame (2) is connected to the lower module (1-2) of the fixed bracket through a connecting plate (6) and fasteners.

5. A mounting platform for an unmanned ultra-high-speed ship propulsion system as described in any one of claims 1-2, characterized in that, Several hinged brackets (7) are provided along the inner circumferential direction of the fixed bracket (1); Each of the hinge brackets (7) is provided with a hinge hole (8); The hinge hole (8) corresponds one-to-one with the hinge point (9) on the peripheral wall of the power system (4) and is fastened together.

6. A mounting platform for an unmanned ultra-high-speed ship propulsion system as described in any one of claims 1-2, characterized in that, The fixed bracket (1), the support frame (2), and the shock absorber bracket (3) are all made of rectangular tubing welded together.

7. A mounting platform for an unmanned ultra-high-speed ship propulsion system as described in any one of claims 1-2, characterized in that, The power system (4) is an aircraft engine.

8. A mounting platform for an unmanned ultra-high-speed ship propulsion system as described in any one of claims 1-2, characterized in that, A fixed mounting structure (5) is provided on the rear end face of the fixed bracket (1); The fixed installation structure (5) is machined with a conical surface that fits against the rear conical surface of the power system (4) to ensure that the installation platform is firmly and reliably installed with the power system (4).