JPH073198Y2 - Missile storage rack device - Google Patents

Description

DETAILED DESCRIPTION OF THE INVENTION (Industrial field of application) The present invention relates to a missile storage rack device applied to an armored vehicle or the like.

(Prior Art) Armored vehicles for protecting troops from enemy attacks have traditionally been
The main purpose is to transport troops, but it is not designed to carry missiles, etc., and there is a demand for diversified transportation that enables the mounting of missiles.

(Problems to be solved by the invention) Since the armored vehicle is operated and steered in a mountainous area with severe irregularities, when a missile or the like is stored together with troops and traveled, the missile or the like may fly out and be damaged due to the traveling disturbance of the vehicle. However, in order to fix the missile accommodated so as to cope with the traveling disturbance, there are problems that many members and labor are required and it takes time to take out the missile.

The present invention was developed in order to address the above-mentioned problems, and its object is to provide a missile storage rack device having improved storage and removal performance as well as storage and fixing performance of the missile. is there.

(Means for Solving the Problem) The present invention is directed to a missile accommodating rack (2) in the front-rear direction of the vehicle body (1a) by tilting the missile outlet side of the rear portion of the vehicle body (1a) upward.
And a cushion (6) that presses the missile downward is provided on the bottom of the missile storage rack (2) with a missile support that cushions and supports the lower part of the missile that is laid down in the longitudinal direction of the vehicle body (1a). The upper cover (3) that can be opened and closed is provided on the upper part of the missile storage rack (2), and the openable cover (3a) that is rotatable about the left-right direction of the vehicle body (1a) is used as the missile of the upper cover (3). A shaft (13), which is provided at the exit end and is rotatable about the left-right direction of the vehicle body (1a), is provided below the missile exit of the missile storage rack (2), and one end of which is fixed to the shaft (13). An operation lever (12) for rotating the shaft (13) is provided on the outside of the missile storage rack (2) so that one end is fixed to the shaft (13) and a roller (15) is attached between the other ends. Install a pair of levers (14) A lever (16) provided on the lower rear end of the body (1a) of the missile to be placed, one end of which is fixed to the shaft (13) and one end of which is the opening / closing cover (3a).
Characterized by a link mechanism that connects the other end of the rod (17) connected to the missile, by storing the missile by opening and closing the upper cover and lifting the rear part of the missile by the missile take-out mechanism with operating lever. In addition to facilitating storage and removal of missiles on the rack, the missile support and cushions have improved the ability to store and fix missiles.

(Operation) By opening and closing the upper cover by the missile take-out mechanism with operating lever, the missile is easily stored in the missile storage rack, and the missile is elastically supported by the missile support and supported by the cushion, which makes the car body violent. The missile is easily taken out by being buffered and stabilized against traveling disturbance and the like, and the upper cover is opened upward and the rear part of the missile is lifted by the missile takeout mechanism with the operating lever.

(Embodiment) FIGS. 1 to 4 show an embodiment of the present invention, in which (1) is an armored vehicle, (2) is a vehicle body (1) of an armored vehicle (1).
a) Missile storage rack arranged in the rear portion, (3) is an upper cover that is openably opened above the missile storage rack (2), and (5) is inside the missile storage rack (2). A missile support which is arranged and supported by a bullet (4a), (6) is a cushion arranged in the upper cover (3), and (10) is an operation lever (at the rear of the missile storage rack (2) ( 1
2) An attached missile take-out mechanism, wherein the missile take-out mechanism (10) includes a shaft (13) axially supported on both left and right sides of the missile storage rack (2) and both ends of the shaft (13). One end is fixed and a pair of operating levers (12) for rotating the shaft and the other end boss portion of the operating lever (12) are retractably fitted and inserted through a compression spring (18) into a missile storage rack ( Knob pin (11a) that engages and disengages with the boss (19) on the 2) side
And a missile (a) supported between a pair of lifting levers (14), one end of which is fixed to an intermediate portion of the shaft (13).
The roller (15) that lifts the lower rear side of the rear shaft and the shaft (1
One end is fixed to both sides of 3) and the other end is composed of a cover opening / closing lever (16) connected to a rod (17) provided at the rear part of the opening / closing covers (3a) (3a).

The missile accommodating rack (2) is arranged in the rear part of the vehicle body (1) in a slightly downward arrangement by brackets (7), (7), etc., and fixed to the rear (right side in the figure) of the missile (a). Movement is prevented, the rear part (right part in the drawing) of the missile storage rack (2) is opened, and an opening / closing door (not shown) is provided on the vehicle body (1a) side.

The upper cover (3) is preferably provided on the upper side of the missile accommodating rack (2) over substantially the entire length, and the rear side can be opened upward around a pivotal attachment portion (not shown) on the front side (the left side in the drawing). And the rear part (3a) of the top cover (3)
Covers the upper and rear upper half of the stored missile (a) in an openable and closable manner, and the lower side of the upper cover (3) is
The cushion (6) is provided so as to project downward in the entire lengthwise direction or locally, and presses the upper side of the stored missile (a).

The missile support (5) is a missile storage rack (2).
Are arranged at appropriate intervals in the bottom of the missile (a) and are elastically supported (4a) upward by a spring (4) to buffer and support the lower side of the missile (a).

When the knob pin (11a) of the operation lever-equipped missile take-out mechanism (10) is fitted to the boss (19) as shown in FIG. 2,
The operating lever (12) is fixed, the roller (15) is in the position shown by the solid lines in FIGS. 3 and 4, and the rear portion of the upper cover (3) is in the position shown in FIGS. 1 (B) and (C). Is stored in the missile storage rack (2) and the missile support (5)
The lower side is elastically supported and the upper side is supported by the cushion (6),
When the knob (11) is pulled from the boss (19) and the operating lever (12) is swung in the direction of the arrow (Fig. 1B), the lever (14) and the roller (15) move in the direction of the arrow (the third direction). (Fig.) Swinging and ascending to lift the rear part of the missile (a) and pull it out rearward, and the rear (3a) side of the upper cover (3) is greatly raised by the link mechanism of the lever (16) and the rod (17). To the rear part of the missile (a), allowing the withdrawal. In the figure, reference numeral (21) is a bracket which is projected on the vehicle body (1a) and bears a shaft (13).

The embodiment of the present invention is configured as described above, and the operation will be described in detail. When the knob (11) is pulled from the boss (19) and the operation lever (12) is swung rearward, Open the rear part (3a) of the cover (3) upward and open the missile (a).
Is inserted and stored from the rear of the missile storage rack (2), the operation lever (12) is swung forward, the rear part (3a) is closed downward, and the lower side of the missile (a) is the missile support (5).
The missile (a) is supported by the spring (4), the upper side of the missile (a) is pressed by the cushion (6), and the upper and rear parts of the missile (a) are supported so that the vehicle body (1a) travels violently. Even under disturbance, the missile (a) is buffered and supported, is stabilized, and pops out to prevent damage.

When the knob (11) is pulled from the boss (19) and the operation lever (12) is swung rearward of the vehicle body, the lever (14) and the roller (15) move through the shaft (13) to the third and fourth positions. As shown in the figure, the missile (a) is swung backward and upward, the rear side of the missile (a) is lifted and pulled out rearward, and at the same time, the link mechanism between the lever (16) and rod (17) through the shaft (13) causes the upper part to rise. The rear part (3a) side of the cover (3) is largely moved upward to open the rear part of the missile (a), and the missile (a) is opened.
Can be easily removed to the rear of the vehicle body.

(Effect of the Invention) The present invention is configured as described above, and the upper cover is opened and closed by the missile take-out mechanism with an operation lever arranged at the rear of the missile storage rack arranged in the vehicle body.
The missile can be easily stored in the missile storage rack, the missile is elastically supported by the missile support and supported by the cushion to improve stability, and the missile withdrawal mechanism with the operating lever lifts the upper cover as the upper cover is opened. It can be easily taken out, and the storage and removal performance of the missile has been significantly improved along with the storage and fixing performance of the missile, and it can be stored even in armored vehicles and the like where traveling disturbance is severe.

[Brief description of drawings]

FIG. 1 (A) is a side view of an armored vehicle with a missile storage rack arrangement showing an embodiment of the present invention, FIG. 1 (B) is an enlarged vertical cross-sectional view of the missile storage rack portion of FIG. 1 (A), FIG. 1 (C) is a right side view of FIG. 1 (B), and FIG. 2 is II- of FIG. 1 (C).
FIG. 3 is an enlarged vertical sectional view of the II portion, FIG. 3 is an enlarged vertical side view of the rear portion of the missile of FIG. 1 (C), and FIG. 4 is a right view of FIG. 1a: vehicle body, 2: missile storage rack 3: upper cover, 4a: bullet support 5: missile support, 6: cushion 10: missile ejection mechanism with operating lever

Claims (1)

[Scope of utility model registration request] A missile storage rack (2) is arranged in the front-rear direction of the vehicle body (1a) by tilting the missile outlet side of the rear part of the vehicle body (1a) upward, and is laid down in the front-rear direction of the vehicle body (1a). A missile support for cushioning and supporting the lower part of the missile is provided at the bottom of the missile storage rack (2), and an openable and closable upper cover (3) having a cushion (6) for pressing the missile downward is provided on the missile storage rack ( A cover (3a) which is provided on the upper part of 2) and rotatable about the left-right direction of the vehicle body (1a) is installed on the end of the missile outlet of the upper cover (3). Rotatable shaft (1
3) is provided below the missile outlet of the missile storage rack (2), and one end of the shaft (13) is fixed to the shaft (13).
A pair of levers (14) having an operating lever (12) for rotating the projection projecting from the outside of the missile storage rack (2), one end of which is fixed to the shaft (13) and a roller (15) being attached between the other ends. ) Is installed at the lower rear end of the body (1a) of the missile to be installed, one end of which is fixed to the shaft (13) and a rod (17) of which one end is connected to the opening / closing cover (3a).
A missile accommodating rack device comprising a link mechanism that connects the other ends of the.