Separating cabin for patrol aircraft and carrier

Abstract

The utility model provides a separation cabin for a patrol aircraft and a carrier, which comprises a shell, a plurality of explosive bolts are uniformly mounted on the shell, threaded ends of the explosive bolts extend out of the front end face of the shell, mounting notches are processed on the front end faces of two opposite sides of the shell, and a separation hinge is mounted in each mounting notch; a pressing ring is installed in the front end of the connecting ring, and a cutting rope is installed between the connecting ring and the pressing ring. The connecting ring is installed in the center of the shell through a plurality of connecting rib plates, and the detonating devices are installed on the connecting rib plates to detonate the explosive bolts. According to the fairing, it is guaranteed that the fairing is rapidly separated through the explosive bolts, and the separation hinge can enable the two fairing bodies to be synchronous in the separation process; and the attitude instability of the patrol aircraft caused by the fairing is avoided.

Description

Technical Field

[0001] The utility model relates to a separation cabin for a patrol vehicle and a carrier. Background Art

[0002] Stage separation is a link that multi-stage aircraft must go through during flight. In order to ensure that the aircraft can smoothly perform subsequent flight missions, it is necessary to ensure that the patrol vehicle can safely and reliably unlock and separate from the carrier that has completed the transportation work, so as to reduce the quality of the aircraft's subsequent missions, ensure the flight altitude and range of the patrol vehicle, and at the same time reduce the impact caused by differences in aerodynamic shapes, and avoid excessive ballistic disturbances and control divergence during the subsequent flight of the patrol vehicle.

[0003] The cruiser is a plane-symmetrical aircraft, and the carrier is an axisymmetric aircraft. First, during the ground assembly process, the two-stage aircraft need to be connected, and the cruiser needs to fold its wings and rudder surfaces before separation, and needs to be wrapped with a fairing to ensure the overall aerodynamic shape of the aircraft.

[0004] When the patrol vehicle and the carrier stage are separated, the patrol vehicle is a large cantilever connection structure, and is in a complex airflow disturbance and coupled vibration environment of the structure and airflow. The separation mechanism is subject to large loads and complex working conditions. The separation of the patrol vehicle and the carrier has a large overload impact, and because the patrol vehicle is in an uncontrolled state during separation, the separation posture is easily affected by the separation mechanism.

[0005] In addition, the separation of the fairing has high synchronization requirements. Asynchronous separation will cause the attitude instability of the projectile, collision and interference between the cruiser and the carrier, and lead to separation failure. Utility Model Content

[0006] In order to solve the above technical problems, the utility model provides a separation cabin for a patrol vehicle and a carrier.

[0007] The utility model is realized through the following technical solutions.

[0008] The utility model provides a separation cabin for a patrol vehicle and a carrier, comprising:

[0009] The shell is evenly equipped with a number of explosive bolts, the threaded ends of the explosive bolts extend out of the front end surface of the shell, and installation notches are processed on the front end surfaces of the two opposite sides of the shell, and a separation hinge is respectively installed in the installation notches;

[0010] A connecting ring, a pressure ring is installed in the front end of the connecting ring, and a cutting rope is installed between the connecting ring and the pressure ring;

[0011] The connecting ring is installed at the center of the shell through a plurality of connecting ribs, and a detonating device is installed on the connecting rib to detonate the explosive bolt.

[0012] The shell is annular, and an annular groove is processed on its inner ring. The explosive end of the explosive bolt is placed in the annular groove, and the threaded end extends out from the through hole on the front end surface of the shell.

[0013] The connecting ring and the pressing ring are both hollow cylinders, an annular groove is processed on the outer wall of the pressing ring, and the cutting rope is installed in the annular groove.

[0014] A plurality of flame extinguishing holes which are relatively connected to each other are processed on the side walls of the pressure ring and the connecting ring.

[0015] The separation hinge is square, a hinge cavity is processed in the middle of one side of the separation hinge, and ears are respectively installed at the edges of the two ends of the separation hinge adjacent to the opening of the hinge cavity, and the ears are fixed at the bottom of the ring groove.

[0016] One end of the hinge cavity relative to the installation notch is set as an opening, and a rotating shaft perpendicular to its inner wall is installed in the hinge cavity. A sliding groove is processed on the side wall between the rotating shaft and the opening of the hinge cavity. The sliding groove is perpendicular to the bottom of the hinge cavity and is processed with a flared opening.

[0017] The two ends of the connecting rib plate are respectively connected to the rear end faces of the shell and the connecting ring. Vertical reinforcing ribs are also provided between the connecting rib plate and the connecting ring. The vertical reinforcing ribs are parallel to the axial direction of the connecting ring.

[0018] The beneficial effects of the utility model are as follows: the explosion bolts are used to ensure the rapid separation of the fairing, and the separation hinges can synchronize the two petals of the fairing during the separation process, thereby preventing the fairing from causing the attitude instability of the cruiser. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a schematic diagram of the structure of the utility model;

[0020] Figure 2 This is a schematic diagram of the separation hinge structure of the utility model;

[0021] Figure 3 This is a schematic diagram of the compression ring structure of the utility model;

[0022] Figure 4 This is a schematic diagram of the structure of the utility model after the cabin is unlocked and separated;

[0023] Figure 5 This is a schematic diagram of the explosive bolt structure of the utility model;

[0024] Figure 6 This is a schematic diagram of the structure of the detonator of the utility model;

[0025] In the figure: 1-shell, 2-separation hinge, 3-cutting rope, 4-connecting ring, 5-detonating device, 6-explosive bolt, 7-rotating shaft, 8-sliding groove, 9-pressure ring, 10-connecting rib plate, 11-vertical reinforcement rib, 12-flame extinguishing hole, 13-ear piece, 14-hinge cavity. DETAILED DESCRIPTION

[0026] The technical solution of the utility model is further described below, but the scope of protection required is not limited to the description.

[0027] A separation cabin for a patrol vehicle and a carrier, wherein a first set of separation mechanisms connects and unlocks a fairing and a connection cabin through an explosive bolt separation mechanism, and a separation hinge limits the separation direction of the fairing to complete the separation of the fairing. A second set of separation mechanisms completes the unlocking and separation of the patrol vehicle and the carrier through an energy-gathering cutting cable assembly. After the separation of the fairing is completed, the cutting cable explodes in a direction corresponding to the separation area of ​​the pressure ring, so that the patrol vehicle and the carrier are unlocked and separated.

[0028] include:

[0029] The shell 1 is evenly equipped with a plurality of explosive bolts 6, the threaded ends of the explosive bolts 6 extend out of the front end surface of the shell 1 and are connected to the fairing. When separation is required, the bolts are detonated by the detonator to unlock and separate the fairing. The front end surfaces on opposite sides of the shell 1 are processed with installation notches, and a separation hinge 2 is respectively installed in the installation notches;

[0030] A connecting ring 4, a pressing ring 9 is installed in the front end of the connecting ring 4, and a cutting rope 3 is installed between the connecting ring 4 and the pressing ring 9;

[0031] The connecting ring 4 is installed at the center of the housing 1 through a plurality of connecting ribs 10 , and a detonating device 5 is installed on the connecting ribs 10 to detonate the explosive bolts 6 .

[0032] The housing 1 is annular, and an annular groove is processed on its inner ring. The explosive end of the explosive bolt 6 is placed in the annular groove, and the threaded end extends out from the through hole on the front end surface of the housing 1.

[0033] The fairing is connected and unlocked and separated from the connection cabin through the explosive bolt separation mechanism. The separation hinge is installed on the cabin body. The separation hinge is provided with a rotating shaft and a sliding groove. After the explosive bolt is detonated, the fairing can only rotate along the sliding groove. After the fairing rotates to a certain angle, the fairing is unhooked from the separation hinge and moves outward to complete the separation from the carrier to avoid collision. After the fairing is separated, the patrol vehicle is unlocked and separated from the carrier through the cutting rope separation mechanism.

[0034] The connecting ring 4 and the pressure ring 9 are both hollow cylinders, and an annular groove is processed on the outer wall of the pressure ring 9, and the cutting rope 3 is installed in the annular groove. The connecting ring and the separation cabin are connected by radial screws, and a detonating cord is placed on the connecting ring and the missile connecting cabin. When the separation signal is received, the detonating cord is ignited and detonated, cutting the cabin into two parts, unlocking the UAV and the carrier missile, and after the fairing is opened, the aerodynamic resistance difference between the patrol vehicle and the carrier is used to achieve separation.

[0035] A plurality of flame extinguishing holes 12 are processed on the side walls of the pressure ring 9 and the connecting ring 4. The flame extinguishing holes 12 release the heat of the cutting rope 3 during the combustion process to prevent the heat from directly impacting the patrol aircraft.

[0036] The separation hinge 2 is square, and a hinge cavity 14 is processed in the middle of one side of the separation hinge 2. Ear pieces 13 are respectively installed at the edges of the opening of the hinge cavity 14 at both ends of the separation hinge 2, and the ear pieces 13 are fixed to the bottom of the annular groove.

[0037] The hinge cavity 14 is set to be open at one end relative to the installation notch, and the hinge seat at the end of the fairing extends into the hinge cavity and is hinged to the rotating shaft 7. A sliding groove 8 is processed on the side wall between the rotating shaft 7 and the opening of the hinge cavity 14 as a limiting structure for the fairing to expand to both ends after the explosion of the explosive bolt. The sliding groove 8 is perpendicular to the bottom of the hinge cavity 14 and is processed with a flared mouth to prevent the fairing from being stuck.

[0038] The two ends of the connecting rib plate 10 are respectively connected to the rear end faces of the shell 1 and the connecting ring 4, and a vertical reinforcing rib 11 is provided between the connecting rib plate 10 and the connecting ring 4, and the vertical reinforcing rib 11 is parallel to the axial direction of the connecting ring 4. The connecting rib plate allows air permeability between the shell and the connecting ring, and the vertical reinforcing rib 11 ensures that the connecting ring 4 can withstand the impact force of the explosion process.

Claims

1. A separation cabin for a patrol vehicle and a carrier, characterized in that: include: A shell (1), wherein a plurality of explosive bolts (6) are evenly mounted on the shell (1), wherein the threaded ends of the explosive bolts (6) extend out of the front end surface of the shell (1), and mounting notches are machined on the front end surfaces of opposite sides of the shell (1), and a separation hinge (2) is respectively mounted in the mounting notches; A connecting ring (4), a pressure ring (9) is installed in the front end of the connecting ring (4), and a cutting rope (3) is installed between the connecting ring (4) and the pressure ring (9); The connecting ring (4) is installed at the center of the housing (1) via a plurality of connecting ribs (10), and a detonating device (5) is installed on the connecting ribs (10) to detonate the explosive bolts (6).

2. The separation cabin for a patrol vehicle and a carrier as claimed in claim 1, characterized in that: The shell (1) is annular, and an annular groove is processed on its inner ring. The explosive end of the explosive bolt (6) is placed in the annular groove, and the threaded end extends out from the through hole on the front end surface of the shell (1).

3. The separation cabin for a patrol vehicle and a carrier as claimed in claim 1, characterized in that: The connecting ring (4) and the pressing ring (9) are both hollow cylinders. An annular groove is processed on the outer wall of the pressing ring (9), and the cutting rope (3) is installed in the annular groove.

4. The separation cabin for a patrol vehicle and a carrier as claimed in claim 3, characterized in that: A plurality of flame extinguishing holes (12) which are relatively connected to each other are processed on the side walls of the pressure ring (9) and the connecting ring (4).

5. The separation cabin for a patrol vehicle and a carrier as claimed in claim 1, characterized in that: The separation hinge (2) is square-shaped, a hinge cavity (14) is processed in the middle of one side of the separation hinge (2), and ears (13) are respectively installed at the edges of the opening of the hinge cavity (14) at both ends of the separation hinge (2), and the ears (13) are fixed to the bottom of the ring groove.

6. The separation cabin for a patrol vehicle and a carrier as claimed in claim 5, characterized in that: One end of the hinge cavity (14) relative to the installation notch is arranged to be open, and a rotating shaft (7) perpendicular to the inner wall of the hinge cavity (14) is installed in the hinge cavity (14), and a sliding groove (8) is processed on the side wall between the rotating shaft (7) and the opening of the hinge cavity (14), and the sliding groove (8) is perpendicular to the bottom of the hinge cavity (14) and is processed to have a flared opening.

7. The separation cabin for a patrol vehicle and a carrier as claimed in claim 1, characterized in that: The two ends of the connecting rib plate (10) are respectively connected to the rear end faces of the shell (1) and the connecting ring (4); vertical reinforcing ribs (11) are also provided between the connecting rib plate (10) and the connecting ring (4); the vertical reinforcing ribs (11) are parallel to the axial direction of the connecting ring (4).

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