CN220974548U - Multi-machine type universal test-run mooring mechanism with quick-release function - Google Patents

Abstract

The application belongs to the field of mooring lock design, and discloses a multi-machine type universal test-run mooring mechanism with a quick-release function, which comprises a double-head mooring lock and a quick-release fixing pin, wherein the double-head mooring lock comprises a lock body, a fixing double ear, a roadbed double ear and a ship base double ear; when the double-head mooring lock is required to be connected with the ship-based aircraft, the ship-based double ears are matched with the mooring interfaces of the ship-based aircraft, and then the quick-release fixing pins are inserted into the double-head mooring lock to fix the ship-based aircraft, so that the multi-machine type general requirement of the double-head mooring lock can be realized by arranging two groups of different double-ear structures; the quick-release fixing pin can realize quick assembly and disassembly between the double-head mooring lock and the corresponding airplane.

Description

Multi-machine type universal test-run mooring mechanism with quick-release function

Technical Field

The application belongs to the field of tethered lock design, and particularly relates to a multi-machine type universal test run tethered mechanism with a quick-release function.

Background

The ground test force mooring device for the aircraft has various structural forms of test vehicle mooring locks matched with aircraft mooring interfaces, but the problem that the test vehicle mooring locks cannot be commonly used among different aircraft types exists.

For example, the sizes of the mooring interfaces on the roadbed aircraft and the ship-based aircraft are different from those of the ground test force mooring devices, so that the two aircraft cannot be assembled simultaneously on the premise of ensuring the assembly precision, and the ground test force mooring devices can be assembled only by replacing different mooring locks back and forth when assembling different aircraft, so that the assembly is inconvenient.

How to achieve a universal assembly of a multi-machine mooring mechanism is a problem to be solved.

Disclosure of Invention

The application aims to provide a multi-machine type universal test run mooring mechanism with a quick-release function, so as to solve the problem that the existing mooring mechanism cannot be universally used among different machine types.

The technical scheme of the application is as follows: the utility model provides a general test-run mooring mechanism of multimachine with quick-release function, includes double-end mooring lock and quick-release fixed pin, double-end mooring lock includes lock body, fixed ears, road bed ears and warship base ears all are connected with the lock body is integrative, fixed ears can be connected with ground test-run mooring device, the opening interval between the road bed ears is greater than the opening interval between warship base ears to road bed ears and warship base ears set up side by side, road bed ears can link to each other with the road bed aircraft, warship base ears can link to each other with warship base aircraft; the quick-release fixing pins are two groups in total and are respectively in splicing fit with the roadbed double ears and the ship foundation double ears, and one end of each quick-release fixing pin is provided with a pin hole which can be connected with the installation lock.

Preferably, the quick-release fixing pin comprises a handle section and a connecting section, the diameter of the handle section is larger than that of the connecting section, the pin hole is formed in the handle section, a baffle ring is arranged at one end, close to the connecting section, of the handle section, and the baffle ring is of an irregular annular structure.

Preferably, the quick-release fixing pin is in clearance fit with the roadbed double ears or the ship foundation double ears, and the middle part of the fixing double ears is of a pulley structure with arc-shaped concave parts from two sides to the middle part.

Preferably, the lock body is in a fan-shaped structure, and the two sides of the middle part of the lock body are provided with lightening holes.

The application relates to a multi-machine type universal test-run mooring mechanism with a quick-release function, which comprises a double-head mooring lock and a quick-release fixing pin, wherein the double-head mooring lock comprises a lock body, a fixing double ear, a roadbed double ear and a ship base double ear; when the double-head mooring lock is required to be connected with the ship-based aircraft, the ship-based double ears are matched with the mooring interfaces of the ship-based aircraft, and then the quick-release fixing pins are inserted into the double-head mooring lock to fix the ship-based aircraft, so that the multi-machine type general requirement of the double-head mooring lock can be realized by arranging two groups of different double-ear structures; the quick-release fixing pin can realize quick assembly and disassembly between the double-head mooring lock and the corresponding airplane.

Drawings

In order to more clearly illustrate the technical solution provided by the present application, the following description will briefly refer to the accompanying drawings. It will be apparent that the figures described below are merely some embodiments of the application.

FIG. 1 is a schematic diagram of the overall structure of the present application;

FIG. 2 is a schematic view of a double-headed mooring lock according to the present application;

fig. 3 is a schematic view of the structure of the quick release fixing pin of the present application.

1. A double-headed mooring lock; 2. a quick release fixing pin; 3. a lock body; 4. fixing the ears; 5. roadbed double ears; 6. double ears of warship base; 7. a handle section; 8. a connection section; 9. a baffle ring.

Detailed Description

The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.

The utility model provides a general test-run mooring mechanism of multi-machine type with quick-release function, including double-end mooring lock 1 and quick-release fixed pin 2, double-end mooring lock 1 includes lock body 3, fixed ears 4, road bed ears 5 and warship base ears 6 are all connected with lock body 3 an organic whole, fixed ears 4 can link to each other with ground test-force mooring device, the opening interval between road bed ears 5 is greater than the opening interval between warship base ears 6, and road bed ears 5 and warship base ears 6 set up side by side, road bed ears 5 can link to each other with the road bed aircraft, warship base ears 6 can link to each other with warship base aircraft; the quick-release fixing pins 2 are two groups in total, the two groups of quick-release fixing pins 2 are respectively in plug-in connection with the roadbed double lugs 5 and the ship base double lugs 6, and one end of each quick-release fixing pin 2 is provided with a pin hole which can be connected with the installation lock.

When the aircraft is fixed, the fixed double lugs 4 of the double-head mooring lock 1 are connected with a ground test force mooring device, when the double-head mooring lock 1 needs to be connected with a roadbed aircraft, the roadbed double lugs 5 are matched with a mooring interface of the roadbed aircraft, and then the roadbed aircraft can be fixed by inserting the quick release fixing pin 2; when the double-head mooring lock 1 is required to be connected with a ship-based aircraft, the ship-based double ears 6 are matched with a mooring interface of the ship-based aircraft, and then the quick-release fixing pins 2 are inserted to fix the ship-based aircraft, so that the multi-machine type general requirement of the double-head mooring lock 1 can be realized by arranging two groups of different double-ear structures; quick assembly and disassembly between the double-head mooring lock 1 and the corresponding aircraft can be realized through the quick-release fixing pin 2.

After the fixing is completed, the safety lock is connected through the pin hole to realize the stable fixing of the quick-release fixing pin 2. The double-head mooring lock 1 and the quick-release fixing pin 2 are made of metal with good salt spray prevention effect, light weight and wear resistance, such as stainless steel. The structural form of the whole set of test-run mooring lock meets the general design requirement of the ground test-force mooring device among multiple models on the premise of unchanged safety and stability.

Preferably, the quick-release fixing pin 2 comprises a handle section 7 and a connecting section 8, the diameter of the handle section 7 is larger than that of the connecting section 8, the pin hole is formed in the handle section 7, one end, close to the connecting section 8, of the handle section 7 is provided with a baffle ring 9, and the baffle ring 9 is of an irregular annular structure. When the quick-release fixing pin 2 is assembled and disassembled, the connecting section 8 is inserted into the roadbed double ears 5 or the ship base double ears 6 by holding the handle section 7 until the baffle ring 9 abuts against the side wall of the roadbed double ears 5 or the ship base double ears 6, so that the quick-release fixing pin is convenient.

Preferably, the quick-release fixing pin 2 is in clearance fit with the roadbed double ears 5 or the ship foundation double ears 6 so as to prevent the quick-release fixing pin 2 from deflecting, the middle part of the fixed double ears 4 is of a pulley structure with arc-shaped concave parts from two sides to the middle part, and therefore, when the steel cable is connected with the fixed double ears 4, the steel cable can be connected to the middle position of the fixed double ears 4, and accordingly, 180-degree fit is formed between an aircraft mooring interface connected with the roadbed double ears 5 or the ship foundation double ears 6 and the steel cable, and accordingly, the installation stability of the mooring mechanism is effectively improved.

Preferably, the lock body 3 has a fan-shaped structure, and weight reducing holes are formed at both sides of the middle part of the lock body 3, so that the weight of the structure is reduced under the condition of ensuring the structural strength.

The last points to be described are: first, in the description of the present application, it should be noted that, unless otherwise specified and defined, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be mechanical or electrical, or may be a direct connection between two elements, and "upper," "lower," "left," "right," etc. are merely used to indicate relative positional relationships, which may be changed when the absolute position of the object being described is changed;

Secondly: in the drawings of the disclosed embodiments, only the structures related to the embodiments of the present disclosure are referred to, and other structures can refer to the common design, so that the same embodiment and different embodiments of the present disclosure can be combined with each other under the condition of no conflict;

Finally: the foregoing description of the preferred embodiments of the invention is not intended to limit the invention to the precise form disclosed, and any such modifications, equivalents, and alternatives falling within the spirit and principles of the invention are intended to be included within the scope of the invention.

Claims (4)

1. The utility model provides a general test of multimachine formula mooring mechanism with quick-release function which characterized in that: the double-head mooring lock comprises a lock body (3), fixed double ears (4), roadbed double ears (5) and ship base double ears (6), wherein the fixed double ears (4), the roadbed double ears (5) and the ship base double ears (6) are integrally connected with the lock body (3), the fixed double ears (4) can be connected with a ground test force mooring device, the opening spacing between the roadbed double ears (5) is larger than the opening spacing between the ship base double ears (6), the roadbed double ears (5) and the ship base double ears (6) are arranged side by side, the roadbed double ears (5) can be connected with a roadbed airplane, and the ship base double ears (6) can be connected with the ship base airplane; the quick-release fixing pins (2) are two groups in total, the two groups of quick-release fixing pins (2) are respectively in plug-in connection with the roadbed double ears (5) and the ship base double ears (6), and pin holes which can be connected with the installation lock are formed in one end of the quick-release fixing pins (2).

2. The multi-machine type universal test run mooring mechanism with quick release function as defined in claim 1, wherein: quick-release fixed pin (2) are including handle section (7) and linkage segment (8), the diameter of handle section (7) is greater than the diameter of linkage segment (8), the pinhole is seted up on handle section (7), one end that handle section (7) are close to linkage segment (8) is equipped with keeps off ring (9), keep off ring (9) are irregular annular structure.

3. The multi-machine type universal test run mooring mechanism with quick release function as defined in claim 1, wherein: the quick-release fixing pin (2) is in clearance fit with the roadbed double ears (5) or the ship foundation double ears (6), and the middle part of the fixing double ears (4) is of a pulley structure which is concave in an arc shape from two sides to the middle part.

4. The multi-machine type universal test run mooring mechanism with quick release function as defined in claim 1, wherein: the lock body (3) is of a fan-shaped structure, and lightening holes are formed in two sides of the middle of the lock body (3).