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CN-122008748-A - Military amphibious aircraft carrier-based aircraft land spacecraft

CN122008748ACN 122008748 ACN122008748 ACN 122008748ACN-122008748-A

Abstract

The invention relates to a military water, land and air carrier-based reconnaissance attack plane land spacecraft. The military vertical take-off and landing fighter plane is designed by integrating an airplane, an automobile and a ship and is driven by oil and electricity. The unmanned ship is formed by a ship bottom shell of a vehicle body, a laser weapon, a radar, a camera, a bypass rotor tire, a landing gear and a water wheel propeller which are arranged on the shell, an automobile assembly and a navigation control system. The mechanical transmission system is formed by driving a double-ball cage universal folding transmission shaft, a landing gear, a bidirectional double-control electromagnetic valve to control forward and backward rotation of a rotor tire of a culvert to finish vertical take-off and landing and highway driving through an automobile assembly and an electric cylinder. The electric control system is powered by the generator and the lithium battery to complete the running of the vertical take-off and landing highway. The water navigation battery supplies power, and the electromagnetic valve controls the water wheel to rotate to navigate on water. An emergency danger avoiding facility is arranged in the device. The servo motor controls the forward inclination angle of the ducted rotor tyre to increase the forward flying speed. A three-purpose military land airship capable of timely coping with various conditions of water, land and air. Civil does not equip the weapon attack system.

Inventors

  • FENG JICHENG
  • Hao Qiue
  • FENG GUANJIANG
  • FENG GUANMING
  • Feng Guansheng
  • FENG JINGJING
  • FENG GUANLIN
  • Feng Shuiru

Assignees

  • 郝秋娥

Dates

Publication Date
20260512
Application Date
20260331

Claims (10)

  1. 1. A military water, land and air carrier-based reconnaissance attack machine and a land spacecraft are composed of a body bottom shell (1), a laser weapon (2), a radar (3), an engine (4), a generator (4 a), a muzzle (5), a camera (6), an ammunition box (8), a landing gear (9), a high-energy battery (10), a water wheel driver (11) and a ducted rotor tire (12) (the interior of the system comprises a hollow brushless motor (21)), a bidirectional double-control electromagnetic valve brake (18), rotor blades (20), a navigation control system, an automobile assembly and a cab, and the military water, land and air carrier-based reconnaissance attack machine is characterized in that the design structure of the body bottom shell (1) is suitable for two requirements of highway driving on water, and the laser weapon (2) and the radar (3) are connected and controlled by the cab and are all arranged at the top of the shell; In a mechanical transmission mode, an engine (4) is arranged on a front axle, two-drive or four-drive switching can be realized during highway driving, the engine (4) outputs power to left and right tires through a clutch (30) and a gearbox (31) to finish driving, the engine (4) is fixed with a shell at the upper part and fixed with an outer sleeve through a damping shock absorption (25) and a single ball cage transmission shaft (26) is a shock absorption shaft through a clutch (30), the gearbox (31) and a transmission shaft (32) during four-drive, and the two-drive and four-drive switching is controlled by a tail one-way electromagnetic valve (33) and a magnetic differential (34); In a mechanical transmission mode of taking off of the land spacecraft, a four-wheel drive engine (4) is transmitted through a clutch (30), a gearbox (31), a transmission shaft (32), a one-way electromagnetic valve (33) and a magnetic differential (34), four bypass rotor tires are diagonally rotated in the forward direction and the reverse direction, one-way electromagnetic valve (29) arranged on one side of the differential (34) is used for controlling one-side tire rotation, an electric cylinder (24) is used for lifting a tire (12), and a two-way double-control electromagnetic valve (18) magnetic brushless motor (21) is used for driving rotor blades (20) to rotate to finish taking off; When the electric transmission takes off, the lithium battery (10) supplies power, the electric cylinder (24) pushes the double-ball-cage universal folding shaft (26) to lift the tire, the brushless motor (21) and the double-control electromagnetic valve (18) magnetically-closed rim fixed shaft head (15), the brushless motor (21) rotates, and the ducted rotor tire (12) does not rotate to finish vertical take off; The landing gear (9) is arranged at the bottom of the shell, and is powered by the lithium battery (10) to push the landing gear to stretch out and draw back, the water wheel propeller (11) is an electric transmission system and is arranged at the rear tail part of the shell, and is powered by the lithium battery (10) and controlled by the water wheel propeller servo motor (11); The ammunition bin (8) is arranged in the shell and connected with the muzzle (5) and is controlled by the cab; the lithium battery (10) is arranged in the shell, supplies power for a navigation system of the electric cylinder (24) and the electric cylinder landing gear (9) of the brushless motor (21) as well as a bidirectional double-control electromagnetic valve (18) and is controlled by a cab; the duct rotor tire (12) is arranged on the rim (13), has functions of both a rotor and a tire, can realize highway running and aerial flying, is internally provided with a chute inside the rotor blade sleeve (20) and is fixed on the brushless motor (21), and is arranged in the duct rotor tire (12), and the duct rotor tire is small in size and large in lifting force.
  2. 2. The military amphibious aircraft carrier-borne aircraft of claim 1, wherein the mechanical structure transmission system is formed by sequentially connecting an engine (4), a gearbox (31), a transmission shaft (32), a one-way electromagnetic valve (33), a differential (34), a double-ball-cage universal folding shaft (26), an electric cylinder (24), a damping shock absorption shaft (25), a servo motor (22), a spherical fluted disc (23), a transmission shaft (16), a hollow brushless motor (21), rotor blades (20), a two-way double-control electromagnetic valve brake (18), a rim fixed disc (15), a rim (13) and a ducted rotor tire (12), and the whole mechanical structure transmission system is connected with and controlled by a cab; the double-ball-cage universal folding shaft is driven by 90 degrees when in highway running, is pushed by an electric cylinder (24) to be 180 degrees when in take-off, and the transmission shaft (26 a) realizes power transmission of vertical take-off.
  3. 3. The land-based aircraft carrier of claim 1, wherein the electric system of the land-based aircraft carrier is characterized in that an engine (4) drives a generator (4 a) to generate electricity, the electric energy is converted into direct current through an inverter and then stored and supplied by a lithium battery (10), the lithium battery (10) supplies power to an electric cylinder, a hollow brushless motor, a laser weapon, a radar and a camera to form an unmanned plane power supply system, and the electric system is integrally installed on the engine body and is controlled by a cab.
  4. 4. The land craft of claim 1, wherein the upper part of the damping shock absorber (25) is fixedly connected with the shell, and the lower part is fixedly connected with the outer sleeve (27) to form a shock absorbing structure.
  5. 5. The military amphibious aircraft carrier-borne aircraft carrier according to claim 1, wherein the hollow outer-transmission sub brushless motor (21) can realize forward and reverse rotation control, is arranged on a transmission shaft fixing sleeve (19), is connected with a lithium battery (10) through an electric wire (28) to obtain power supply, is integrally arranged in a rim, and is characterized in that a tire rotates and the brushless motor does not rotate during highway running, and the brushless motor rotates and the outer-culvert tire (12) does not rotate during take-off.
  6. 6. The land craft of claim 1, wherein the water wheel driver (11) is installed at the rear tail of the shell, and is powered by the generator (4 a) and the lithium battery (10), and is controlled by the water wheel propeller servo motor (11) to realize the forward and steering actions.
  7. 7. The military amphibious aircraft carrier-borne aircraft land craft according to claim 1, wherein the laser weapon (2) and the radar navigation system (3) are arranged at the top of the shell, and are powered by the lithium battery (10), and the two are connected to realize a reconnaissance positioning function, so that the omnidirectional attack operation is facilitated.
  8. 8. The land craft of claim 1, wherein the lithium battery (10) is charged by a generator (4 a) and is installed in a shell to supply power to all electric components, the energy can be supplemented by an alternating current charging mode, alternating current energy is converted into direct current through inversion and then stored in the lithium battery (10), the lithium battery (10) supplies power to the laser weapon (2), the radar (3), the infrared camera (6), the hollow brushless motor (21) and the electric cylinder (24) through a line (28), and all power supply operations are completed by a cab.
  9. 9. The land craft of claim 1, wherein the landing gear (9) is mounted at the bottom of the chassis, the high-energy battery (10) supplies power and pushes the electric cylinder (24) to extend the landing gear during take-off, the rotation speed of the rotor is increased after the tyre is separated from the ground to realize vertical take-off, and the landing gear is controlled and retracted by the cab during highway driving.
  10. 10. The land craft of the military amphibious aircraft carrier of claim 1, wherein 12 rotor blades are arranged in each tire of the ducted rotor tires (12), 48 blades are arranged in total of 4 ducted rotor tires, the diameter of each tire is 800-1000mm, the length of each blade is 280-380mm, the specific size can be customized according to the dead weight and the carrying capacity of the land craft, the ducted rotor tires are arranged on two sides of a shell and can be pushed by an electric cylinder (24) to lift to two sides, 6 supporting upright posts are arranged in the middle of a rim (13), and the structural stability of the rim is improved.

Description

Military amphibious aircraft carrier-based aircraft land spacecraft Technical Field The invention belongs to the technical field of military sea, land and air traffic, and particularly relates to a military water, land and air carrier-based reconnaissance attack machine and a land spacecraft, which can realize land vertical take-off and landing, highway running, vertical take-off and landing on the water surface and water navigation, are suitable for water and landing operations, can be also built into a small water surface carrier-based reconnaissance attack machine group during the operations, and can cover severe areas in land mountain areas to run and can complete the vertical take-off and landing of an amphibious military fighter in narrow and small urban spaces. Background Advanced weaponry and carrier-borne aircraft are developed in various countries in the world at present so as to meet the future war demands, and a small carrier reconnaissance attack fighter capable of running under various conditions of water, land and air and taking off and landing vertically is urgently needed in the present stage. The existing military equipment such as warships, carrier-based aircraft, airplanes, armored vehicles and the like has single function and poor maneuverability, and the water, land and air traffic and reconnaissance attack aircraft need to be frequently replaced when a fighter is logged in, so that the fighter is extremely easy to delay and cause serious consequences for determining the success or failure. At present, no amphibious and air vertical take-off and landing multifunctional warplane and land airship capable of realizing three-in-one and one-in-one is available, but automobiles, airplanes, warships, ships, unmanned aerial vehicles, 3D printing technologies and composite materials are developed and mature, and a technical foundation is provided for developing the multifunctional military warplane of the land airship. Based on the current situation, the invention develops a military small-sized water-land-air three-purpose aircraft carrier reconnaissance attack machine, which can be used as an aircraft carrier attack machine, can directly vertically lift from the water surface, aircraft carrier and land, and makes up the blank of the prior art. Disclosure of Invention The invention provides an amphibious three-purpose carrier-borne aircraft land spacecraft, which aims to overcome the technical defects that the existing military traffic and attack equipment is single in function, the carrier-borne aircraft take-off and landing rely on special equipment and is poor in maneuverability. The invention relates to a sea, land and air three-purpose land spacecraft, which mainly comprises a ship body bottom shell, a bypass rotor wing tire, an engine, a generator, a landing gear, a lithium battery, a water wheel driver, an ammunition box, a brushless motor, a laser attack system, a radar infrared camera navigation system, a transmission system, an automobile assembly and a cab operating system, wherein the landing gear is positioned at the lower part of the shell, the water wheel driver is positioned at the rear tail part of the shell, the bypass rotor wing tire is of a dual-purpose structure capable of lifting to two sides and used for land running and air flying, the bypass rotor wing has high lift force and low noise, and the tire consists of an outer rubber tire, a rim, a built-in brushless motor and rotor blades. The invention adopts a hybrid oil-electric mode, is provided with an electric transmission system and a mechanical transmission system, is powered by a generator and a lithium battery, and the cab uniformly controls an electric control system, so that the endurance mileage is effectively increased, and meanwhile, an emergency danger avoiding facility is arranged in the equipment, so that the automatic switching can be realized when the mechanical or electric system fails, and the equipment damage and the casualties are avoided. The specific transmission and driving scheme is as follows: 1. The mechanical transmission structure is that the engine drives the generator to generate electricity at ordinary times to fully charge the lithium battery, the mechanical transmission is driven to the tire by the clutch, the gearbox, the transmission shaft, the differential mechanism, the double-ball-cage universal folding transmission shaft and the bevel gear, and the whole system is controlled by the automobile assembly and the cab operating system. The electric transmission system is powered by a generator and a lithium battery, and is used for powering a laser weapon, a radar, a rotor brushless motor, an electromagnetic valve, an electric cylinder and a landing gear through lines, and for improving the forward flying speed, the forward flying inclination angle of the tire can be adjusted through a servo motor, and all the operations are completed by a cab. The water wheel driver is arranged at the r