CN211731836U

CN211731836U - Multifunctional steering instrument capable of automatically steering by 360 degrees

Info

Publication number: CN211731836U
Application number: CN201921150244.2U
Authority: CN
Inventors: 杜德华
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-07-22
Filing date: 2019-07-22
Publication date: 2020-10-23
Anticipated expiration: 2029-07-22

Abstract

The utility model relates to a multifunctional steering instrument capable of automatically steering by 360 degrees, which comprises a fixed bottom plate fixedly arranged on an outer component, and a columnar outer frame connected with the fixed bottom plate into a whole, wherein a columnar outer disc and an inner disc which is suspended in the columnar outer disc through a transmission assembly and can horizontally rotate by 360 degrees relative to the columnar outer disc are arranged in the columnar outer frame; the inner disc is fixedly provided with a mechanical gripper for gripping missiles for operation, has high flexibility, can be used for air, space and space operation equipment such as fighters, space shuttles, space vehicle satellites and the like, and can be used for 360-degree operation without dead angles in the air space and the space; the utility model has the performance of more stable operation and stronger supporting performance; and can be used for port carrying, capital construction, large, medium and small hoisting devices, excavators and other heavy hoisting equipment.

Description

Multifunctional steering instrument capable of automatically steering by 360 degrees

Technical Field

The utility model A relates to a full-automatic steering instrument, in particular to a 360-degree full-automatic steering instrument which is suitable for all combat equipment in air and space such as fighter planes, space shuttles, space vehicles, satellites and the like; the type B is large-scale hoisting and excavating equipment for port delivery and infrastructure construction.

Background

When the existing military fighter aircraft is in air battle, the aircraft nose of the aircraft must be directly opposite to a target to attack, so when the military fighter aircraft is in air battle, the two parties must occupy favorable positions and orientations, if one party is in a disadvantaged orientation, the other party cannot be attacked, so that the military fighter aircraft is in close attack and fails, conceivably, the result is that the man-out of the aircraft is small, the whole battle and even the whole war ending are influenced greatly, and the big affair !

Aiming at the current problem of the existing fighter, the steering instrument which can fight at multiple angles in the air and even 360 degrees without dead angles without adjusting the flight direction and the direction of the airplane, doing large roundabout and large turning is very urgent and necessary.

Of course, except for the military field, the existing equipment in the civil hoisting field has the advantages of complex structure, high cost and low bearing capacity, and the B-type hoisting device can also be suitable for the civil large-scale hoisting field.

SUMMERY OF THE UTILITY MODEL

The utility model aims to solve the technical problem that, overcome prior art's shortcoming, provide a simple structure is reasonable, control is convenient and with low costs can 360 auto-steering's multi-functional steering appearance.

In order to solve the technical problem, the utility model discloses a multifunctional steering instrument that can 360 degrees automatic steering, including the fixed baseplate that is fixedly installed on the external member, still include the column frame that is connected as an organic whole with the fixed baseplate, be equipped with the column outer disc in the column frame and through the inner disc that transmission assembly hangs and adorn in the column outer disc and can 360 degrees rotations horizontally relative to the column outer disc; and a mechanical gripper for gripping missiles for fighting or a hoisting mechanism for hoisting and hoisting equipment is fixedly arranged on the inner disc.

The utility model discloses further technical scheme is: the transmission assembly comprises an electric motor which is fixedly arranged at the bottom of the cylindrical outer disc; three annular grooves are formed in the columnar outer disc, a driven large gear is fixedly mounted on the outer wall of the inner disc at a position corresponding to the position of the middle annular groove, and pulleys are respectively mounted at positions corresponding to the positions of the upper annular groove and the lower annular groove; and a driving pinion meshed with the driven gearwheel is mounted at the end part of a power output shaft of the electric motor.

Furthermore, at least one channel is formed in the center of the inner disc along the axis direction; the bottom of the channel is provided with a first cylinder, the connecting rod is sleeved in a connecting pipe of the first cylinder, and the connecting pipe is fixedly connected with the first cylinder through a movable joint.

Further, the mechanical gripper comprises a left gripper, a right gripper, a left support, a right support and an arm, wherein the left gripper and the right gripper are hinged to the arm through hinges, the left gripper and the right gripper are hinged to the left support and the right support through hinge points on the outer wall, the left support and the right support are hinged to a connecting rod, and the connecting rod controls the left support and the right support to lift and grips and release the left gripper and the right gripper.

Furthermore, the arm of the mechanical gripper is fixedly connected with a channel opening at the top of the inner disc, the left support and the right support enter the channel of the inner disc from wedge-shaped channel openings at two sides of the inner disc and are hinged with a connecting rod, and the connecting rod is sleeved with a connecting pipe of the first air cylinder.

And the push rod of the second cylinder is fixedly connected with the bottom of the columnar outer disc and used for controlling the lifting of the steering instrument. The first cylinder and the second cylinder are both controlled by the airplane fire control radar.

Furthermore, the top of the cylindrical outer disc is higher than that of the inner disc, and a compass is arranged at the top of the outer disc.

Furthermore, the inner disc is higher than the columnar outer disc, and a reinforcing support structure is additionally arranged at the lower part of the suspension arm, so that the lifting device is more suitable for port carrying and infrastructure construction equipment of the existing large-scale hoisting.

Furthermore, the steering instrument is suitable for manufacturing and modifying weaponry such as combat airplanes, bombers, unmanned planes and armed helicopters, and conceptual weapons such as laser guns and laser cannons.

The utility model has the advantages that: the mechanical gripper for gripping missiles for fighting is fixedly arranged on the inner disc of the A-shaped structure, has high flexibility, can be used for air, space and space fighting equipment such as fighters, space shuttles, space aircraft satellites and the like, and can fight in the air space without dead angles of 360 degrees in the space; the B-shaped structure of the utility model has the performance of more stable operation and stronger supporting performance; and can be used for port carrying, capital construction, large, medium and small hoisting devices, excavators and other heavy hoisting equipment.

Drawings

Fig. 1 is a schematic view of the overall structure of embodiment 1 of the present invention.

Fig. 2 is a schematic diagram of a second position state of the structure of fig. 1.

Fig. 3 is a schematic structural diagram of a first mechanical gripper according to embodiment 1 of the present invention.

Fig. 4 is a schematic structural view of a second mechanical gripper according to embodiment 1 of the present invention.

Fig. 5 is a perspective view of 1/4 of the outer tray according to embodiment 1 of the present invention.

Fig. 6 is a perspective view of 1/4 of the inner tray according to embodiment 1 of the present invention.

Fig. 7 is a single-channel top plan view of embodiment 1 of the present invention.

Fig. 8 is a top plan view of the dual channel of embodiment 1 of the present invention.

Fig. 9 is a schematic diagram of the first mechanical gripper used for the guided missile in embodiment 1 of the present invention.

Fig. 10 is a schematic diagram of a second mechanical gripper used for the guided missile in embodiment 1 of the present invention.

Fig. 11 is a schematic view of the installation position and the fighting orientation of the fighter plane in pitching flight according to embodiment 1 of the present invention.

Fig. 12 is a schematic view of the installation position and the combat orientation of the aircraft on the side of the fighter plane according to embodiment 1 of the present invention.

Fig. 13 is a schematic view of the overall structure in embodiment 2 of the present invention.

Fig. 14 is a schematic view of the overall structure of embodiment 3 of the present invention.

Detailed Description

The present invention will be further described with reference to the accompanying drawings and the detailed description.

Example 1

The embodiment provides a multifunctional steering instrument capable of automatically steering 360 degrees, which is shown in fig. 1-12:

the mechanical gripper comprises a mechanical gripper 1, a left support 2, a right support 2, a hinge point 3, an inner disc 4, a columnar outer disc 5, a first pulley 6, a second pulley 6', a channel 7, a connecting rod 8, a driven large gear 9, a driving small gear 10, an electric motor 11, a cylinder connecting pipe 12, a movable joint 13, a first cylinder 14, a fixed bottom plate 15, a columnar outer frame 16, a lifter connecting sleeve 17, a second cylinder 18(1), a push rod 18(2), an annular groove 5-2, an upper annular groove 5-1, a lower annular groove 5-1, a channel opening 4-1 and a compass 19.

Wherein: the mechanical hand grip 1 comprises a left hand grip and a right hand grip, and the outer walls of the left hand grip and the right hand grip are hinged with the left support 2 and the right support 2; the groove is respectively arranged on two sides of the outer arm of the mechanical gripper in the embodiment, and the left support and the right support are hinged with the corresponding mechanical gripper and then enter the channel through the groove to be hinged with the connecting rod 8 at the hinge joint 3. Preferably, the grip in this embodiment may be in the shape of two palms or in the shape of two arcs.

In the embodiment, the center of the inner disc 4 is provided with a channel 7 along the axis direction; the bottom of the channel is provided with a first cylinder 14, and the left support 2 and the right support 2 at the top of the connecting rod control the grabbing of the manipulator.

Preferably, in this embodiment, the connecting rod 8 is sleeved in a cylinder connecting pipe 12 of the first cylinder, the cylinder connecting pipe 12 is fixedly connected with the first cylinder through a movable joint 13, and the first cylinder controls the lifting of the connecting rod and the gripping of the manipulator.

Preferably, the channel top channel opening 4-1 in the embodiment is

The upper part of the channel is of a wedge-shaped structure, and the middle part and the lower part of the channel are cylindrical round hole channels.

The cylindrical outer disk 5 is arranged in the cylindrical outer frame 16, and the inner disk 4 is suspended in the cylindrical outer disk 5 through a transmission assembly and can horizontally rotate for 360 degrees relative to the cylindrical outer disk; and a push rod 18(2) of the second air cylinder is connected with the bottom of the columnar outer disc in a sleeved mode through a lifter connecting sleeve 17, so that the lifting of the steering instrument can be controlled.

As shown in fig. 5 and 6: in the embodiment, the transmission assembly comprises an electric motor 11, the electric motor 11 is fixedly arranged at the bottom of the columnar outer disc, three annular grooves are formed in the inner wall of the columnar outer disc along the circumferential direction, a driven large gear 9 is fixedly arranged on the outer wall of the inner disc at a position corresponding to the position of a middle annular groove 5-2, and a first pulley 6 and a second pulley 6' are respectively arranged at positions corresponding to the positions of an upper annular groove 5-1 and a lower annular groove 5-1; and a driving pinion 10 meshed with the driven gearwheel is mounted at the end part of a power output shaft of the electric motor. A driving pinion 10 of an electric motor 11 drives an outer ring-shaped driven bull gear 9 of the inner disc to rotate for 360 degrees, and a mechanical gripper on the inner disc and the missile fight at any direction of 360 degrees.

Preferably, the top of the cylindrical outer disc 5 is higher than the inner disc, said outer disc being provided with a compass 19 at the top, as shown in fig. 7-8. Two channels may be opened in the inner disc 4 in this embodiment.

The fixed bottom plate 15 and the columnar outer frame 16 are connected into an integral structure; the second cylinder 18(1) is mounted on the fixed base plate.

The first cylinder controls the gripping of the manipulator, the second cylinder controls the lifting of the steering gear, the two cylinders are controlled by the airplane fire control radar, and a pilot can electrically or remotely control the cylinders and the manipulator.

Preferably, the fixed bottom plate in this embodiment is linear, arc or other suitable installation shape, and is provided with bolt holes meeting composite installation requirements, so that the fixed bottom plate can be installed under the wing, and the fixed bottom plate is inversely fixed on the wing; or the missile hanging point can be arranged in the cabin, or arranged above the wings or other parts beneficial to operation, or can be arbitrarily set for operation missile hanging points for the operation requirements of airplanes and various operation equipment.

The missile redirector comprises the following components: 1. the hanging type missile is generally hung below a wing, the missile faces downwards, a base plate is inversely fixed on the wing, according to the level of scientific and technological manufacture, if the hanging type missile can be installed above the wing, the missile faces upwards, and the base plate is installed above the wing; 2. the missile launcher is semi-concealed, has excellent performance, is provided with a cover cap, can be arranged below or above the wings of an airplane, in a cabin and the like, can automatically position a missile and then open the cover cap to directly and suddenly launch the missile, and can also launch the missile after opening the cover cap, wherein a drawer-type cover cap is generally preferred; 3. the hidden type is mainly arranged in the cabin, a lifter is needed, the lifter can be delivered out of the cabin for battle by a cylinder or other suitable lifting technologies, and the existing lifting technologies are advanced, various in types, preferred and not introduced.

The utility model discloses an it is whole to rely on two upper and lower pulleys to link into on between inner disc and the column outer disc, the inner disc hangs the dress and can play upper and lower positioning action in the column outer disc, can make inside and outside linking into an organic whole, and the inner disc can use external force kinetic energy to rotate in a flexible way in the outer disc, the outside gear wheel of inner disc can with the pinion toothing on the electric motor, electric motor and the fire control radar looks UNICOM of aircraft, pilot's electronic or remote control motor, it is rotatory to drive the inner disc by the pinion on the motor, and the top manipulator of inner disc is used for fixed operation guided missile, pivoted inner disc drives manipulator and guided missile rotation, the guided missile can do multi-angle or 360 rotation operations according to pilot's instruction like this, according to the accurate and arbitrary target of doing the dead angle of location compass reading and fight.

As shown in fig. 11 and 12: the circle in the figure represents the installation position schematic of the direction finder in the embodiment and the effect graph of the operation direction thereof, and the dotted line and the arrow in the figure represent the operation flight path of the missile.

The utility model discloses the structure is applicable to various aircraft such as combat aircraft, bomber, unmanned aerial vehicle, armed helicopter, space plane, and the manufacturing and the repacking of weapon equipment such as satellite still are applicable to conceptual weapons such as laser gun, laser big gun in addition. The battle can be carried out at 360 degrees without dead angles, the existing old mode of battle operation without large roundabout and large turning and occupying attack directions and positions can freely, easily and quickly orient the target at any time, accurately attack and defend oneself, and greatly enhance the operation capacity of the fighter.

During combat, this structure is under pilot control:

1. the missile normally points to the right front, namely 0;

2. when coming from the left enemy, the user can strike the golf club in 180 degrees on the left;

3. when coming to the right, striking in 180 degrees on the right;

4. when the rear coming enemy attacks, the attack is performed in 180 degrees in an oriented mode.

Besides, the airplane can freely attack the other side and defend themselves at 360 degrees, the unfavorable factors such as flight path adjustment, great roundabout, great turning, favorable direction occupation and the like are not needed, particularly, when the airplane is attacked or attacked suddenly by enemies, the strange energy can be more highlighted, and the airplane can be started by the enemy first, combat leisurely and fight against the enemy in the air.

The structure in the embodiment is a more advanced, more convenient, flexible and quick battle mode which appears in long air and space. The battle force is remarkable, the fighting force is doubled, and the enemy can smell wind and can fun the gallbladder.

Example 2

The embodiment provides a multifunctional steering instrument capable of automatically steering 360 degrees, as shown in fig. 13: the basic structure and the principle are the same as those of the embodiment 1, the difference is only that the second cylinder equipment which is lifted by the whole structure can not be used below the fixed bottom of the embodiment, and the structure is suitable for the exposed hanging type and the semi-hidden type.

Example 3

The multifunctional steering instrument capable of automatically steering 360 degrees provided by the embodiment is as shown in fig. 14: the basic structure and principle of the lifting mechanism are the same as those of the embodiment 1, except that the mechanical gripper is changed into a lifting mechanism, and the lifting mechanism in the embodiment comprises a lifting arm 20 fixedly connected with the top of an inner disc, a lifting hook 23 arranged at the end of the lifting arm and other auxiliary equipment.

Preferably, the inner disc in this embodiment is higher than the cylindrical outer disc, and a set of reinforced support structures 21 are fixedly connected between the suspension arm and the outer wall of the inner disc higher than the cylindrical outer disc at equal intervals.

Preferably, the fixed baseplate in this embodiment is disposed on a tower 22.

This embodiment structure can be used to each big, medium and small type jack-up hoist and mount and excavator equipment, because the utility model discloses have two swivels, so more have flexibility, stationarity and stronger support type ability, be applicable to large-scale hoist and mount fields such as building trade, harbour container transportation.

In addition to the above-described

embodiments

1, 2 and 3, the present invention may have other embodiments. All the technical solutions formed by adopting equivalent substitutions or equivalent transformations fall within the protection scope claimed by the present invention.

Claims

1. The utility model provides a can 360 multi-functional steering appearance of automatic steering, includes the PMKD of fixed mounting on outer member, its characterized in that: the inner disc is suspended in the columnar outer disc through a transmission assembly and can horizontally rotate for 360 degrees relative to the columnar outer disc; and a mechanical gripper for gripping missiles for fighting or a hoisting mechanism for hoisting and hoisting equipment is fixedly arranged on the inner disc.

2. A multi-purpose steering instrument capable of 360 ° automatic steering according to claim 1, characterized in that: the transmission assembly comprises an electric motor which is fixedly arranged at the bottom of the cylindrical outer disc; three annular grooves are formed in the columnar outer disc, a driven large gear is fixedly arranged on the outer wall of the inner disc corresponding to the position of the middle annular groove, and two pulleys are arranged at the positions corresponding to the positions of the upper annular groove and the lower annular groove; and a driving pinion meshed with the driven gearwheel is mounted at the end part of a power output shaft of the electric motor.

3. A multi-purpose steering instrument capable of 360 ° automatic steering according to claim 2, characterized in that: the mechanical gripper comprises a left gripper, a right gripper, a left support, a right support and an arm, wherein the left gripper and the right gripper are hinged to the arm through hinges, the left gripper and the right gripper are hinged to the left support and the right support through hinge points on the outer wall, the left support and the right support are hinged to a connecting rod, and the connecting rod controls the left support and the right support to lift and grips and release the left gripper and the right gripper.

4. A multi-purpose steering gauge capable of 360 ° automatic steering according to claim 3, characterized in that: the center of the inner disc is provided with at least one channel along the axis direction; the bottom of the channel is provided with a first cylinder, the connecting rod is sleeved in a connecting pipe of the first cylinder, and the connecting pipe is fixedly connected with the first cylinder through a movable joint.

5. The multi-purpose steering instrument capable of 360 ° automatic steering according to claim 4, characterized in that: the arms of the mechanical gripper are fixedly connected with a channel opening at the top of the inner disc, the left support and the right support enter the channel of the inner disc from wedge-shaped channel openings at two sides of the inner disc and are hinged with a connecting rod, and the connecting rod is sleeved with a connecting pipe of the first air cylinder.

6. The multi-purpose steering instrument capable of 360 ° automatic steering according to claim 5, characterized in that: the fire control system is characterized by further comprising a second cylinder fixedly mounted on the fixed base plate, a push rod of the second cylinder is fixedly connected with the bottom of the columnar outer disc, and the first cylinder and the second cylinder are controlled by the aircraft fire control radar.

7. The multi-purpose steering instrument capable of 360 ° automatic steering according to claim 6, characterized in that: the top of the cylindrical outer disc is higher than that of the inner disc, and a compass is arranged at the top of the outer disc.

8. A multi-purpose steering instrument capable of 360 ° automatic steering according to claim 7, characterized in that: the steering instrument is suitable for manufacturing and modifying combat aircrafts, bombers, unmanned planes and armed helicopters, and is also suitable for laser guns and laser cannons.

9. A multi-purpose steering instrument capable of 360 ° automatic steering according to claim 2, characterized in that: the hoisting mechanism comprises a hoisting arm fixedly connected with the top of the inner disc, and a reinforcing support structure is additionally arranged on the lower portion of the hoisting arm.