A safe take-off and landing fighter plane with multiple security facilities

Abstract

The invention is titled "A Safe Takeoff and Landing Fighter Jet Equipped with Multiple Support Facilities." It belongs to the field of fighter jet technology. Its main purpose is to solve the problems of existing fighter jets being unable to take off and land quickly, and being unable to take off and land in situations without a runway. Its main features include: a fighter jet fuselage, nose, tail, cockpit, control keyboard, front left, front right, rear left, rear right wings, front left, front right, rear left, rear right engines, and front and rear ground contact buffers; electrically driven turntables for adjusting the rotation angle of the front left, front right, rear left, rear right wings are respectively located between the front left, front right, rear left, rear right wings and the fighter jet fuselage; electrically driven turntables for adjusting the rotation angle of the front left, front right, rear left, rear right engines are respectively located between the front left, front right, rear left, rear right engines and ... rear right engines are respectively located between the front left, front right, rear left, rear right engines and the front left, rear right engines are respectively located between the front left, front right, rear left, rear right engines and the front left, rear right engines are respectively located between the front left, front right, rear

Description

Technical Field

[0001] This invention belongs to the field of fighter jet technology, specifically relating to a fighter jet that is equipped with a variety of support facilities, can adapt to different environments, and can take off and land with or without an airport runway, and can take off and land at multiple angles. Background Technology

[0002] At the beginning of the 20th century, the Wright brothers in the United States invented the airplane. On December 17, 1903, the Wright brothers successfully test-flew their Flyer I, finally realizing humanity's dream of soaring through the air like birds. This marked the beginning of a great era of development in human aviation technology. With the continuous development of various industries and the increasing demand for efficiency, aviation technology has found more and more applications in human life.

[0003] In modern warfare, especially in naval and long-range operations, it is common for aircraft carriers and ships to carry fighter jets. Because fighter jets can only take off at a certain speed and require long runways for takeoff and landing, they can only take off and land at airports with runways, which greatly limits their effectiveness.

[0004] The present invention provides a safe take-off and landing fighter jet equipped with multiple support facilities, which solves the problem of fighter jets being able to take off and land in places with airport runways, and also in places without airport runways.

[0005] When fighter jets take off and land, especially at high altitudes, accidents often result in the destruction of the aircraft and loss of life. Each air disaster not only causes unbearable grief to the families of the victims but also brings enormous losses to the country.

[0006] The purpose of this invention is to address the above-mentioned shortcomings by providing a safe take-off and landing fighter jet equipped with multiple support facilities, which is not limited by airport runways and can safely take off and land in any geographical environment.

[0007] The technical solution of this invention is: a safe takeoff and landing fighter jet equipped with multiple support facilities, including a fighter jet fuselage, a fighter jet nose, a fighter jet tail, a fighter jet cockpit, a fighter jet control keyboard, a fighter jet front left wing, a fighter jet front right wing, a fighter jet rear left wing, a fighter jet rear right wing, a fighter jet front left engine, a fighter jet front right engine, a fighter jet rear left engine, and a fighter jet rear right engine; the fighter jet nose is equipped with a fighter jet front ground contact buffer, and the fighter jet tail is equipped with a fighter jet rear ground contact buffer; the fighter jet front left wing, fighter jet front right wing, fighter jet rear left wing, and fighter jet rear right wing are respectively equipped with an electrically driven turntable for adjusting the rotation angle of the fighter jet front left wing, a fighter jet... The fighter jet has an electrically driven turntable for adjusting the rotation angle of its front right wing, a electrically driven turntable for adjusting the rotation angle of its rear left wing, and an electrically driven turntable for adjusting the rotation angle of its rear right wing. The turntable is characterized in that: the fighter jet's front left engine, front right engine, rear left engine, and rear right engine are respectively connected to the fighter jet's front left wing, front right wing, rear left wing, and rear right wing via electrically driven turntables for adjusting the rotation angle of their respective engines.

[0008] The left and right front wings of the fighter jet described in the technical solution of this invention are foldable wings.

[0009] The technical solution of the present invention provides folding mechanisms on the front left wing, front right wing, rear left wing, and rear right wing of the fighter jet.

[0010] The technical solution of the present invention describes that the fighter jet's front left wing, front right wing, rear left wing, and rear right wing are all equipped with fighter jet parachute ejectors and fighter jet parachutes.

[0011] The fighter jet in the technical solution of this invention is equipped with a fighter jet propeller catapult and a fighter jet propeller on its nose.

[0012] The fighter cockpit described in the technical solution of this invention includes a spherical cockpit body, a circular fighter cockpit fixing frame, a fighter cockpit gyroscope balancer, a fighter cockpit gyroscope balancer guide rail, a fighter cockpit gyroscope balancer ball bearing, a fighter cockpit parachute ejector, a fighter cockpit parachute, a fighter cockpit propeller ejector, a fighter cockpit propeller, a fighter cockpit airbag compartment, and a fighter cockpit airbag; the cockpit body is equipped with a fighter cockpit door and a fighter display screen, and the fighter operation keyboard is located inside the cockpit body; the fighter cockpit gyroscope balancer guide rail is distributed on both sides, and the fighter cockpit gyroscope balancer ball bearing connects with the fighter cockpit airbag. The cockpit fixed frame is connected to form a spherical space; the fighter jet cockpit gyroscope balancer is fixed inside the fighter jet cockpit fixed frame and the fighter jet cockpit gyroscope balancer guide rail, and is symmetrically distributed; the cockpit body is installed in the spherical space inside the fighter jet cockpit gyroscope balancer; the fighter jet cockpit parachute ejector and fighter jet cockpit parachute are located on the upper part of the fighter jet cockpit fixed frame, and the fighter jet cockpit propeller ejector and fighter jet cockpit propeller are located on the lower part of the fighter jet cockpit fixed frame; the fighter jet cockpit airbag compartment and fighter jet cockpit airbag are located in the lower half of the cockpit body; the fighter jet cockpit ejector is installed below the cockpit body.

[0013] The technical solution of the present invention describes that the lower sides of the fighter jet fuselage are provided with fighter jet airbag compartments and fighter jet airbags.

[0014] The electric drive turntable for adjusting the rotation angle of the front left engine, the front right engine, the rear left engine, and the rear right engine of the fighter jet, as described in the technical solution of this invention, all include a motor drive turntable frame, a motor drive turntable stator, a motor drive turntable rotor, a motor drive turntable coil winding, a motor drive turntable permanent magnet, a motor drive turntable controller, a motor drive turntable bearing (53), a motor drive turntable brake shoe, a motor drive turntable wiring harness, a motor drive turntable balance guide rail, a motor drive turntable balance ball, and a motor drive turntable hydraulic brake pump, with a circular cross-section; wherein, the motor drive turntable frame is a shell with a circular groove, the cylindrical motor drive turntable stator is fixed at the center of the motor drive turntable frame, and the annular motor drive turntable... The motor coil winding is mounted on the stator of the motor drive turntable; the motor drive turntable rotor is disc-shaped, and its center is connected to the motor drive turntable stator via a motor drive turntable bearing; the motor drive turntable permanent magnet is surrounded by the outer side of the motor drive turntable coil winding and fixed to the motor drive turntable rotor; the motor drive turntable controller is located outside the motor drive turntable permanent magnet; the motor drive turntable brake shoes are mounted on the inner side wall of the motor drive turntable frame; the motor drive turntable hydraulic brake pump is mounted at the port of the motor drive turntable frame and connected to the motor drive turntable brake shoes; the motor drive turntable rotor is provided with brake rings that correspond to and cooperate with the motor drive turntable brake shoes; the inner side wall of the motor drive turntable frame and the outer side wall of the brake ring are provided with cooperating motor drive turntable balance guide rails, and motor drive turntable balance balls are installed between the two motor drive turntable balance guide rails.

[0015] The electric drive turntable for adjusting the rotation angle of the fighter jet's front left wing, the electric drive turntable for adjusting the rotation angle of the fighter jet's front right wing, the electric drive turntable for adjusting the rotation angle of the fighter jet's rear left wing, and the electric drive turntable for adjusting the rotation angle of the fighter jet's rear right wing all include a motor drive turntable frame, a motor drive turntable stator, a motor drive turntable rotor, a motor drive turntable coil winding, a motor drive turntable permanent magnet, a motor drive turntable controller, a motor drive turntable bearing (53), a motor drive turntable brake shoe, a motor drive turntable wiring harness, a motor drive turntable balance guide rail, a motor drive turntable balance ball, and a motor drive turntable hydraulic brake pump, with a circular cross-section; wherein, the motor drive turntable frame is a shell with a circular groove, the cylindrical motor drive turntable stator is fixed at the center of the motor drive turntable frame, and the annular motor drive turntable coil winding is assembled. The motor drives a rotary table. The rotor is disc-shaped, with its center connected to the stator via a bearing. A permanent magnet surrounds the outer side of the coil windings and is fixed to the rotor. A controller is located outside the permanent magnet. Brake shoes are mounted on the inner wall of the frame. A hydraulic brake pump is installed at the frame port and connected to the brake shoes. The rotor has brake rings that mate with the brake shoes. The inner wall of the frame and the outer wall of the brake rings have mate balancing guides, with balancing balls between them.

[0016] The fighter jet described in the technical solution of this invention is equipped with fighter jet landing gear on its fuselage.

[0017] The fighter jet's front left engine, front right engine, rear left engine, and rear right engine are respectively connected to the fighter jet's front left wing, front right wing, rear left wing, and rear right wing with electrically driven turntables for adjusting the rotation angle of the front left engine, front right engine, rear left engine, and rear right engine.

[0018] This invention not only employs a rotatable connection between the four wings and the fuselage of the fighter jet, but also a rotatable connection between the four engines and the four wings. These movable wings and engines can be adjusted relative to the fuselage and wings as needed, allowing the fighter jet to take off and land in any region without being restricted by airport runways. This increases the aircraft carrying capacity of aircraft carriers and ships, and enables fighter jets to take off and land in areas where airport runways are not feasible, reducing the need for ground crew and supporting facilities for fighter jets, thus saving the country the manpower and financial resources required for airport construction.

[0019] The present invention mainly solves the problem of fighter jets taking off and landing in the same way as existing fighter jets when there is an airport runway, and can also break the traditional take-off and landing method to take off and land quickly.

[0020] This invention improves upon the shortcomings of traditional fighter jets, enabling them to demonstrate their superiority, flexibility, safety, and powerful combat capabilities in combat.

[0021] This invention features the advantages of not being limited by airport runways, enabling rapid takeoff and landing, and significantly improved safety. This invention is primarily intended for use in fighter jets. Attached Figure Description

[0022] Figure 1 This is a schematic diagram of the structure of the present invention.

[0023] Figure 2 This is a schematic diagram of the underside of a fighter jet before the engine was installed, according to the present invention.

[0024] Figure 3 This is a schematic diagram of the fighter jet's underside after the engine has been installed according to the present invention.

[0025] Figure 4 This is a schematic diagram of a fighter jet taking off in the presence of an airport runway, according to the present invention.

[0026] Figure 5 This is a schematic diagram of a fighter jet taking off in the absence of an airport, according to the present invention.

[0027] Figure 6 This is a schematic diagram of a fighter jet taking off with its wings folded, according to the present invention.

[0028] Figure 7 This is a schematic diagram of a fighter jet in flight during vertical landing according to the present invention.

[0029] Figure 8 This is a schematic diagram of a fighter jet landing in the presence of an airport runway, according to the present invention.

[0030] Figure 9 This is a schematic diagram of a fighter jet landing in the absence of an airport runway, according to the present invention.

[0031] Figure 10 This is a schematic diagram of the fighter jet landing when its wings are folded, according to the present invention.

[0032] Figure 11 This is a schematic diagram of a fighter jet landing after a malfunction in the front-mounted engine during flight, according to the present invention.

[0033] Figure 12 This is a schematic diagram of a fighter jet landing after a malfunction of its rear-mounted engine during flight, according to the present invention.

[0034] Figure 13 This is a schematic diagram illustrating the landing of a fighter jet in the event of an accident involving the left-hand engine during flight, according to the present invention.

[0035] Figure 14 This is a schematic diagram illustrating the landing of a fighter jet when its left-mounted engine malfunctions during flight.

[0036] Figure 15 This is a schematic diagram of the parachute deployment when all engines of the present invention experience an unexpected malfunction during flight.

[0037] Figure 16 This is a schematic diagram of the propeller popping out and opening when all engines of the present invention fail unexpectedly during flight.

[0038] Figure 17 This is a schematic diagram of the airbag deployment in the fighter jet according to the present invention.

[0039] Figure 18 This is a schematic diagram of the fighter jet's cockpit when the fuselage of the present invention is opened.

[0040] Figure 19 This is a schematic diagram of the fighter jet cockpit ejection according to the present invention.

[0041] Figure 20 This is a schematic diagram of the fighter jet cockpit parachute deploying during the invention.

[0042] Figure 21 This is a schematic diagram of the fighter jet cockpit propeller popping out and opening.

[0043] Figure 22 This is a schematic diagram of the deployment and timing of the airbags in the cockpit of the fighter jet according to the present invention.

[0044] Figure 23 This is a schematic diagram of the cockpit structure of the fighter jet of the present invention. Figure 1 .

[0045] Figure 24 This is a schematic diagram of the cockpit structure of the fighter jet of the present invention. Figure 2 .

[0046] Figure 25This is a cross-sectional view of the electrically driven turntable for adjusting the rotation angle of the front left, front right, rear left, and rear right engines of the fighter jet engine according to the present invention.

[0047] In the image: 1. Fighter jet nose; 2. Fighter jet fuselage; 3. Fighter jet tail; 4. Fighter jet landing gear; 5. Fighter jet cockpit; 6. Fighter jet control keyboard; 7. Fighter jet display screen; 8. Fighter jet forward left wing; 9. Fighter jet forward right wing; 10. Fighter jet rear left wing; 11. Fighter jet rear right wing; 12. Fighter jet forward left wing folding connector; 13. Fighter jet forward right wing folding connector; 14. Fighter jet forward left engine adjustment rotation angle electric drive turntable; 15. Fighter jet forward right engine adjustment rotation angle electric drive turntable; 16. Fighter jet rear left engine 17. Electric-driven turntable for adjusting the rotation angle of the fighter jet's rear right engine; 18. Electric-driven turntable for adjusting the rotation angle of the fighter jet's front left engine; 19. Electric-driven turntable for adjusting the rotation angle of the fighter jet's front right engine; 20. Electric-driven turntable for adjusting the rotation angle of the fighter jet's rear left engine; 21. Electric-driven turntable for adjusting the rotation angle of the fighter jet's rear right engine; 22. Electric-driven turntable for adjusting the rotation angle of the fighter jet's front left wing; 23. Electric-driven turntable for adjusting the rotation angle of the fighter jet's rear right wing; 24. Electric-driven turntable for adjusting the rotation angle of the fighter jet's front left wing; 25. Electric-driven turntable for adjusting the rotation angle of the fighter jet's front right wing; 26. Electric-driven turntable for adjusting the rotation angle of the fighter jet's rear left wing; 27. Electric-driven turntable for adjusting the rotation angle of the fighter jet's rear right wing; 28. 29. Fighter jet cockpit door; 30. Fighter jet spiral staircase; 31. Fighter jet parachute ejector; 32. Fighter jet parachute; 33. Fighter jet propeller ejector; 34. Fighter jet propeller; 35. Fighter jet cockpit ejector; 36. Fighter jet airbag compartment; 37. Fighter jet airbag; 38. Fighter jet cockpit fixed frame; 39. Fighter jet cockpit gyroscope balancer; 40. Fighter jet cockpit gyroscope balancer guide rail; 41. Fighter jet cockpit gyroscope balancer ball bearing; 42. Fighter jet cockpit parachute ejector; 43. Fighter jet cockpit parachute; 44. Fighter jet cockpit propeller ejector; 4 4. Fighter jet cockpit propeller; 45. Fighter jet cockpit airbag compartment; 46. Fighter jet cockpit airbag; 47. Motor-driven turntable frame; 48. Motor-driven turntable motor stator; 49. Motor-driven turntable motor rotor; 50. Motor-driven turntable motor coil winding; 51. Motor-driven turntable motor permanent magnet; 52. Motor-driven turntable motor controller; 53. Motor-driven turntable motor bearing; 54. Motor-driven turntable brake shoes; 55. Motor-driven turntable motor wiring harness; 56. Motor-driven turntable balance guide rail; 57. Motor-driven turntable balance ball bearing; 58. Motor-driven turntable hydraulic brake pump. Detailed Implementation

[0048] The invention will now be further described with reference to the accompanying drawings.

[0049] like Figures 1 to 23 As shown in the figure. An embodiment of the present invention provides a safe takeoff and landing fighter jet equipped with multiple support facilities, comprising a fighter jet fuselage 2, a fighter jet nose 1, a fighter jet tail 3, a fighter jet cockpit 5, a fighter jet control keyboard 6, a fighter jet front left wing 8, a fighter jet front right wing 9, a fighter jet rear left wing 10, a fighter jet rear right wing 11, four fighter jet engines 11, a fighter jet front left engine 18, a fighter jet front right engine 19, a fighter jet rear left engine 20, and a fighter jet rear right engine 21. The fighter jet nose 1 is equipped with a fighter jet front ground contact buffer 22, the fighter jet tail 3 is equipped with a fighter jet rear ground contact buffer 23, and the fighter jet fuselage 2 is equipped with a fighter jet landing gear 4. Between the fighter jet front left wing 8, the fighter jet front right wing 9, the fighter jet rear left wing 10, and the fighter jet rear right wing 11 and the fighter jet fuselage 2, respectively, are electrically driven turntables 24, 25, 26, and 27 for adjusting the rotation angle of the fighter jet front left wing, 25, 26, and 27. Among them, the nose 1, tail 3, cockpit 5, engine 11, fuselage 2, and wings, except for the connection with the wings, are the same as the corresponding parts of existing fighter jets and are existing technologies.

[0050] The electric drive turntables 24, 25, 26, 27 for adjusting the rotation angle of the fighter jet's front left wing, 27, 28, 29, 20, 20, 21, 22, 23, 24, 25, 26, 27, and 28 all include a motor drive turntable frame 47, a motor drive turntable stator 48, a motor drive turntable rotor 49, a motor drive turntable coil winding 50, a motor drive turntable permanent magnet 51, a motor drive turntable controller 52, a motor drive turntable bearing 53, a motor drive turntable brake shoe 54, a motor drive turntable wiring harness 55, a motor drive turntable balance guide rail 56, a motor drive turntable balance ball bearing 57, and a motor drive turntable hydraulic brake pump 58, all with a circular cross-section. The motor drive turntable frame 47 is a housing with a circular groove. A cylindrical motor drive turntable stator 48 is fixed at the center of the motor drive turntable frame 47, and an annular motor drive turntable coil winding 50 is fitted onto the motor drive turntable stator 48. The motor drive turntable rotor 49 is disc-shaped, and its center is connected to the motor drive turntable stator 48 via a motor drive turntable bearing 53. A permanent magnet 51 surrounds the outside of the motor drive turntable coil winding 50 and is fixed to the motor drive turntable rotor 49. A motor drive turntable controller 52 is located outside the permanent magnet 51. A brake shoe 54 is mounted on the inner wall of the motor drive turntable frame 47. A hydraulic brake pump 58 is mounted at the port of the motor drive turntable frame 47 and connected to the brake shoe 54. The rotor 49 of the motor-driven turntable is equipped with a brake ring that corresponds to and engages with the brake shoes 54 of the motor-driven turntable. The inner wall of the motor frame 47 and the outer wall of the brake ring are equipped with matching motor-driven turntable balance rails 56, and motor-driven turntable balance balls 57 are installed between the two balance rails 56. The electrically driven turntables 24, 25, 26, 27, and 26 adjust the rotation angle of the fighter jet's left front wing, right front wing, and rear left and right rear wing, respectively. These allow the fighter jet to adjust its wing angle in different regions, harsh environments, and in situations without an airport runway, enabling safe takeoff and landing. This method of takeoff eliminates the need for an airport runway, allowing multiple fighter jets to take off simultaneously, significantly increasing the aircraft capacity and combat power of aircraft carriers and ships, shortening combat time, and reducing unnecessary expenses.

[0051] The fighter jet's forward left wing 8 and forward right wing 9 are foldable wings. The fighter jet's rear left wing 10 and rear right wing 11 are the same as existing fighter jets and are considered prior art. Both the forward left wing 8 and forward right wing 9 are equipped with folding mechanisms. The purpose of foldable wings is to reduce the wing area of ​​the fighter jet, increasing the aircraft carrying capacity of ships; this is also prior art. The fighter jet's forward left wing 8, forward right wing 9, rear left wing 10, and rear right wing 11 are all equipped with fighter jet parachute ejectors 30 and fighter jet parachutes 31. The fighter jet parachute ejector 30 is used when a fighter jet encounters various accidents in the air and all its engines stop running. The fighter jet pilot operates the fighter jet control keyboard 6 to open the fighter jet parachute ejector 30, allowing the fighter jet parachute 31 to deploy and lift the fighter jet to a landing. At the same time, the fighter jet pilot can open the fighter jet propeller ejector 32, causing the fighter jet propeller 33 to start running and propel the fighter jet away from densely populated areas and tall buildings, allowing the fighter jet to land in a safe area. If the fighter jet lands on the surface of the sea, river, lake, or water, the fighter jet pilot operates the fighter jet control keyboard 6 to open the fighter jet airbag compartment 35, and the fighter jet airbag 36 deploys to increase the buoyancy of the fighter jet, allowing the fighter jet to float on the water. At this time, the fighter jet propeller 33 continues to run, propelling the fighter jet toward the shore and waiting for rescue.

[0052] The fighter jet's front left engine 18, fighter jet's front right engine 19, fighter jet's rear left engine 20, and fighter jet's rear right engine 21 are respectively connected to the fighter jet's front left wing 8, fighter jet's front right wing 9, fighter jet's rear left wing 10, and fighter jet's rear right wing 11 with electrically driven turntables 14, 15, 16, 17 for adjusting the rotation angle of the fighter jet's front left engine, 15, 16, and 17.

[0053] The electric drive turntables 14, 15, 16, and 17 for adjusting the rotation angle of the front left engine, 15, 16, and 17 of the fighter jet engine are structurally identical to those 24, 25, 26, and 27 for adjusting the rotation angle of the front left wing, 26, and 27 of the fighter jet engine. They all include a motor drive turntable frame, a motor drive turntable stator, a motor drive turntable rotor, a motor drive turntable coil winding, a motor drive turntable permanent magnet, a motor drive turntable controller, a motor drive turntable bearing, a motor drive turntable brake shoes, a motor drive turntable wiring harness, a motor drive turntable balance guide rail, a motor drive turntable balance ball bearing, and a motor drive turntable hydraulic brake pump, all with a circular cross-section. The motor drive turntable frame is a shell with a circular groove. A cylindrical motor drive turntable stator is fixed at the center of the frame, and an annular motor drive turntable coil winding is fitted onto the stator. The motor drive turntable rotor is disc-shaped, connected to the stator at its center via a bearing. A permanent magnet surrounds the coil winding and is fixed to the rotor. A controller is located outside the permanent magnet. Brake shoes are mounted on the inner wall of the frame. A hydraulic brake pump is installed at the frame port and connected to the brake shoes. A brake ring corresponding to the brake shoes is located on the rotor. The inner wall of the motor frame and the outer wall of the brake ring of the motor-driven turntable are equipped with matching motor-driven turntable balance guide rails, and motor-driven turntable balance balls are installed between the two motor-driven turntable balance guide rails. The fighter jet engine front left engine adjustment rotation angle electric drive turntable 14, fighter jet engine front right engine adjustment rotation angle electric drive turntable 15, fighter jet engine rear left engine adjustment rotation angle electric drive turntable 16, and fighter jet engine rear right engine adjustment rotation angle electric drive turntable 17 are used by the pilot to adjust the engine angle through the fighter jet keypad and the engine adjustment rotation angle electric drive turntable to ensure a safe landing of the fighter jet after one of the engines fails and stops in flight.

[0054] The nose of the fighter jet is equipped with a fighter propeller catapult 32 and a fighter propeller 33.

[0055] The lower sides of the fighter jet fuselage 2 are equipped with fighter jet airbag compartments 35 and fighter jet airbags 36.

[0056] The fighter cockpit 5 includes a spherical cockpit body, a circular fighter cockpit fixing frame 37, a fighter cockpit gyroscope balancer 38, a fighter cockpit gyroscope balancer guide rail 39, a fighter cockpit gyroscope balancer ball bearing 40, a fighter cockpit parachute ejector 41, a fighter cockpit parachute 42, a fighter cockpit propeller ejector 43, a fighter cockpit propeller 44, a fighter cockpit airbag compartment 45, and a fighter cockpit airbag 46. The cockpit body is equipped with a fighter cockpit door 28 and a fighter display screen 7. The fighter cockpit door 28 is the only passage for the pilot to enter the fighter cockpit and is existing technology. The fighter display screen 7 transmits data from multiple cameras installed on the outside of the fighter jet or multiple cameras installed on the outside of the fighter cockpit to the display screen inside the cockpit. The fighter pilot controls the fighter jet by pressing the control wheel based on the images and data on the display screen, which is also existing technology. The fighter jet control keyboard 6 is located inside the cockpit and serves as the function keypad for operating all components of the fighter jet, including communication between the fighter jet and the outside world and for sending relevant signals to the outside world; this is existing technology. The fighter jet cockpit gyroscope balancer rails 39 are distributed on both sides and connected to the fighter jet cockpit fixed frame 37 via the fighter jet cockpit gyroscope balancer balls 40, forming a spherical space. The fighter jet cockpit gyroscope balancer 38 is fixed inside the fighter jet cockpit fixed frame 37 and the fighter jet cockpit gyroscope balancer rails 39, symmetrically distributed. The cockpit body is installed within the spherical space inside the fighter jet cockpit gyroscope balancer 38. The fighter jet cockpit parachute ejector 41 and fighter jet cockpit parachute 42 are located on the upper part of the fighter jet cockpit fixed frame 37, and the fighter jet cockpit propeller ejector 43 and fighter jet cockpit propeller 44 are located on the lower part of the fighter jet cockpit fixed frame 37. The fighter jet cockpit airbag compartment 45 and fighter jet cockpit airbag 46 are located in the lower half of the cockpit body. A fighter jet cockpit ejection system 34 is installed below the cockpit fuselage. A fighter jet cockpit gyroscope balancer 38 is installed inside the fighter jet cockpit fixing frame 37. The fighter jet cockpit gyroscope balancer ball 40 on the fighter jet cockpit gyroscope balancer 38 is connected to the fighter jet cockpit gyroscope balancer guide rail 39 on the outside of the fighter jet cockpit 5. In this way, the fighter jet cockpit 5 is fixed in the fighter jet cockpit fixing frame 37, so that the fighter jet cockpit 5 is always kept in a horizontal state.The fighter jet cockpit ejection system 41 is used when a fighter jet is in flight and all engines fail, it is hit by enemy fire, it burns in the air, or it explodes, making it impossible for the pilot to land safely. In the imminent moment of imminent destruction, the pilot can use the control keyboard 6 to open the ejection system 34, ejecting the cockpit 5. After the cockpit separates from the fighter jet, the pilot can then open the ejection system 34 again, causing the cockpit parachute 42 to deploy and support the cockpit 5, allowing it to gently float down. The pilot operates the fighter jet control keyboard 6 to launch the fighter jet's cockpit propeller catapult 43, which in turn launches the electrically driven propeller 44, propelling the fighter jet's cockpit away from densely populated areas and tall buildings, allowing the fighter jet to land in a safe area. If the fighter jet's cockpit lands on the sea, river, lake, or water, the pilot operates the control keyboard 6 to deploy the cockpit airbag compartment 45, simultaneously deploying the airbag 46 to increase the buoyancy of the fighter jet's cockpit, making it float on the water's surface. At this time, the cockpit propeller 44 rotates, propelling the fighter jet's cockpit towards the shore and awaiting rescue. The fighter jet's cockpit 5 is made of special materials that are bulletproof, explosion-proof, and fireproof. It is designed to maintain a level position regardless of any accidents or rollovers that occur in the air, thus preventing the fighter jet pilot from mistaking the sea for the sky in an emergency and continuing to descend, resulting in a tragic crash into the sea.

[0057] The fighter jet ladder 29 is used for pilots to board the fighter jet cockpit and exit the cockpit, and is existing technology.

[0058] like Figure 5 As shown, in the absence of an airport runway, the fighter jet pilot uses the control panel 6 to rotate the power-driven dials 14, 15, 16, 17 (forward left engine, forward right engine, rear left engine, and rear right engine) upwards by 90 degrees, putting the fighter jet into vertical takeoff mode and allowing it to take off vertically. This takeoff mode eliminates the need for an airport runway, allowing multiple fighter jets to take off simultaneously. It can shorten combat time, increase combat effectiveness, and reduce unnecessary manpower and financial expenditures for the country.

[0059] like Figure 6As shown, takeoff with folded wings is a method used when fighter jets are parked on ships to increase the ship's aircraft capacity. Before parking, the fighter jet pilot uses the fighter jet control keyboard 6 to operate the electrically driven dials 24, 25, 26, 27 to adjust the rotation angle of the forward left wing, 8, and 9 of the fighter jet, folding them backward. This reduces the wing area, increasing the ship's aircraft capacity and putting the fighter jet in vertical takeoff mode. This takeoff mode eliminates the need for an airport runway, allows multiple fighter jets to take off simultaneously, shortens combat time, increases combat effectiveness, and reduces unnecessary manpower and financial expenditures for the country.

[0060] like Figure 9 As shown, when landing in the absence of an airport runway, the fighter pilot uses the fighter control keyboard 6 to operate the electrically driven turntable 24 for adjusting the rotation angle of the forward left wing, the electrically driven turntable 26 for adjusting the rotation angle of the rear left wing, and the electrically driven turntable 27 for adjusting the rotation angle of the rear right wing, rotating them upwards by 90 degrees. At the same time, the fighter jet lands in a vertical landing mode. This vertical landing mode allows the fighter jet to land without being restricted by an airport runway and can adapt to landing in various different geographical environments.

[0061] like Figure 10 As shown, when a fighter jet lands with its wings folded, the pilot uses the control panel 6 to rotate the power-driven dials 24 (forward left wing), 26 (rear left wing), and 27 (rear right wing) upwards by 90 degrees. Simultaneously, the pilot folds the forward left wing (8) and forward right wing (9) backwards, reducing the wing area and increasing the aircraft capacity of the aircraft carrier. This allows the fighter jet to land vertically in a vertical landing mode. This landing method eliminates the need for an airport runway, and multiple fighter jets can land simultaneously.

[0062] like Figure 11 As shown, after the fighter jet's front engine malfunctions during flight, the pilot uses the fighter jet control keypad 6 to adjust the angles of the rear left and rear right wing engines, rotating the fighter jet 180 degrees backward to make the nose of the fighter jet point downward, allowing the nose of the fighter jet to touch down slowly with the ground buffer block, thus safely landing the fighter jet.

[0063] like Figure 12As shown, if a fighter jet experiences a rear-engine malfunction during flight, the pilot can use the fighter jet control key 6 to operate the left and right front wing engines to continue flying and select an airport for landing. If no nearby airport can be selected, the pilot can use the fighter jet control key 6 to steer the fighter jet nose upwards, allowing the tail buffer block to touch the ground and land the fighter jet safely.

[0064] like Figure 13 As shown, after the left-side engine of the fighter jet malfunctioned during flight, the pilot used the fighter jet control keypad 6 to adjust the front right wing engine and the rear right wing engine of the fighter jet to rotate 90 degrees to the right simultaneously, start the engines, and slowly bring the fighter jet down.

[0065] like Figure 14 As shown, after the right-hand engine of the fighter jet malfunctioned during flight, the pilot used the fighter jet control keypad 6 to adjust the forward left wing engine and the rear left wing engine of the fighter jet to rotate 90 degrees to the left simultaneously, start the engines, and slowly bring the fighter jet down.

[0066] like Figure 15 As shown, after all the engines of the fighter jet fail in flight, the fighter pilot uses the fighter jet operation keyboard 6 to operate the fighter jet parachute ejector 30 to open the fighter jet parachute 31 and lift the fighter jet to land.

[0067] like Figure 16 As shown, after all engines of the fighter jet malfunction during flight, the pilot uses the fighter jet control keyboard 6 to open the fighter jet propeller catapult 32, causing the fighter jet propeller 33 to start running and propel the fighter jet away from densely populated areas and tall buildings, allowing the fighter jet to land in a safe area.

[0068] like Figure 17 As shown, when the fighter jet's airbags deploy, the fighter jet floats on the surface of the sea, river, lake, or lake. The fighter jet pilot operates the fighter jet control key 6 to open the fighter jet's airbag compartment 35, and at the same time, the fighter jet's airbags 36 deploy to increase the fighter jet's buoyancy and make the fighter jet float on the water. At this time, the fighter jet's propeller 33 continues to rotate, propelling the fighter jet towards the shore and waiting for rescue.

[0069] like Figure 18 As shown, the fighter jet cockpit opens when the fighter jet encounters an accident in the air, is engaged in combat with an enemy aircraft, all engines are damaged, or the fighter jet is on fire and about to explode. At this time, the fighter jet pilot operates the fighter jet control keyboard 6 to operate the fighter jet cockpit fixed frame 37 to open. At the same time, the fighter jet pilot operates the fighter jet control keyboard 6 to operate the fighter jet cockpit ejector 34 to open and eject the fighter jet cockpit 5 into the air.

[0070] like Figure 19 As shown, after the fighter jet cockpit ejects and is launched into the air, it falls to the ground. At this time, the fighter jet pilot uses the fighter jet operation keyboard 6 to operate the fighter jet cockpit parachute ejector 41 to open the fighter jet cockpit parachute 42, which launches and opens to support the fighter jet cockpit 5 and slowly floats down.

[0071] like Figure 20 As shown, the fighter jet cockpit parachute ejection occurs when the fighter jet cockpit 5 is falling from the air to the ground. The fighter jet pilot uses the fighter jet operation keyboard 6 to operate the fighter jet cockpit parachute ejector 41 to open the fighter jet cockpit parachute 42, which then ejects and opens, supporting the fighter jet cockpit 5 as it falls from the air to the ground.

[0072] like Figure 21 As shown, when the fighter jet cockpit propeller 44 ejects and opens, the fighter jet cockpit parachute 42 ejects and opens, supporting the fighter jet cockpit 5 as it falls from the air to the ground. The fighter jet pilot uses the fighter jet operation keyboard 6 to operate the fighter jet cockpit propeller catapult 43 to open and open the fighter jet cockpit propeller 44, which propels the fighter jet cockpit away from densely populated areas and tall buildings, allowing the fighter jet to fall to a safe area.

[0073] like Figure 22 As shown, the fighter jet cockpit airbags deploy, causing the fighter jet cockpit 5 to fall to the ground in the air. If the fighter jet cockpit lands on the surface of the sea, river, lake, or water, the fighter jet pilot uses the fighter jet control keyboard 6 to operate the fighter jet cockpit airbag compartment 45 to open, and at the same time deploy the fighter jet cockpit airbag 46 to increase the buoyancy of the fighter jet cockpit and make the fighter jet cockpit float on the water. At this time, the fighter jet pilot uses the fighter jet control keyboard 6 to operate the cockpit propeller 44 to open and rotate, pushing the fighter jet cockpit 5 to drift to the shore and wait for rescue.

Claims

1. A safe takeoff and landing fighter jet equipped with multiple safety facilities, comprising a fighter jet fuselage (2), a fighter jet nose (1), a fighter jet tail (3), a fighter jet cockpit (5), a fighter jet control keyboard (6), a fighter jet front left wing (8), a fighter jet front right wing (9), a fighter jet rear left wing (10), a fighter jet rear right wing (11), a fighter jet front left engine (18), a fighter jet front right engine (19), a fighter jet rear left engine (20), and a fighter jet rear right engine (21); wherein the fighter jet nose (1) is provided with a fighter jet front ground contact buffer block ( 22), the fighter jet tail (3) is provided with a fighter jet rear touchdown buffer block (23); the fighter jet front left wing (8), fighter jet front right wing (9), fighter jet rear left wing (10) and fighter jet rear right wing (11) are respectively provided with a fighter jet front left wing adjustment rotation angle electric drive turntable (24), a fighter jet front right wing adjustment rotation angle electric drive turntable (25), a fighter jet rear left wing adjustment rotation angle electric drive turntable (26) and a fighter jet rear right wing adjustment rotation angle electric drive turntable (27) between the fighter jet front left wing adjustment rotation angle and the fighter jet fuselage (2); characterized in that: The fighter jet's front left engine (18), fighter jet's front right engine (19), fighter jet's rear left engine (20), and fighter jet's rear right engine (21) are respectively connected to the fighter jet's front left wing (8), fighter jet's front right wing (9), fighter jet's rear left wing (10), and fighter jet's rear right wing (11) with electrically driven turntables for adjusting the rotation angle of the fighter jet's front left engine (14), fighter jet's front right engine (15), fighter jet's front left engine (16), and fighter jet's rear right engine (17).

2. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 1, characterized in that: The left front wing (8) and the right front wing (9) of the fighter jet are foldable wings.

3. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 2, characterized in that: The fighter jet is equipped with folding mechanisms on its front left wing (8), front right wing (9), rear left wing (10), and rear right wing (11).

4. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 1, 2 or 3, characterized in that: The fighter jet is equipped with a fighter jet parachute ejector (30) and a fighter jet parachute (31) on the front left wing (8), the front right wing (9), the rear left wing (10), and the rear right wing (11).

5. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 1, 2 or 3, characterized in that: The fighter jet nose (1) is equipped with a fighter jet propeller catapult (32) and a fighter jet propeller (33).

6. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 1, 2 or 3, characterized in that: The fighter cockpit (5) includes a spherical cockpit body, a circular fighter cockpit fixing frame (37), a fighter cockpit gyroscope balancer (38), a fighter cockpit gyroscope balancer guide rail (39), a fighter cockpit gyroscope balancer ball bearing (40), a fighter cockpit parachute ejector (41), a fighter cockpit parachute (42), a fighter cockpit propeller ejector (43), a fighter cockpit propeller (44), a fighter cockpit airbag compartment (45), and a fighter cockpit airbag (46); the cockpit body is equipped with a fighter cockpit door (2). 8) and the fighter jet display screen (7), the fighter jet operation keyboard (6) are located in the cockpit body; the fighter jet cockpit gyroscope balancer guide rail (39) is distributed around the cockpit, and is connected to the fighter jet cockpit fixed frame (37) through the fighter jet cockpit gyroscope balancer ball (40) to form a spherical space; the fighter jet cockpit gyroscope balancer (38) is fixed inside the fighter jet cockpit fixed frame (37) and the fighter jet cockpit gyroscope balancer guide rail (39), and is symmetrically distributed; the cockpit body is installed in the spherical space inside the fighter jet cockpit gyroscope balancer (38); The fighter cockpit parachute ejector (41) and fighter cockpit parachute (42) are located on the upper part of the fighter cockpit fixed frame (37), and the fighter cockpit propeller ejector (43) and fighter cockpit propeller (44) are located on the lower part of the fighter cockpit fixed frame (37); the fighter cockpit airbag compartment (45) and fighter cockpit airbag (46) are located on the lower half of the cockpit body; and the fighter cockpit ejector (34) is installed below the cockpit body.

7. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 1, 2 or 3, characterized in that: The lower sides of the fuselage (2) of the fighter jet are provided with fighter jet airbag compartments (35) and fighter jet airbags (36).

8. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 1, 2 or 3, characterized in that: The aforementioned electric drive turntables for adjusting the rotation angle of the front left engine, front right engine, rear left engine, and rear right engine of the fighter jet each include a motor drive turntable frame, a motor drive turntable stator, a motor drive turntable rotor, a motor drive turntable coil winding, a motor drive turntable permanent magnet, a motor drive turntable controller, a motor drive turntable bearing (53), a motor drive turntable brake shoes, a motor drive turntable wiring harness, a motor drive turntable balance guide rail, a motor drive turntable balance ball, and a motor drive turntable hydraulic brake pump, with a circular cross-section. The motor drive turntable frame is a shell with a circular groove, and the cylindrical motor drive turntable stator is fixed at the center of the motor drive turntable frame. The annular motor drive... The rotating disc motor coil winding is mounted on the stator of the rotating disc motor; the rotating disc motor rotor is disc-shaped, and its center is connected to the stator of the rotating disc motor via a rotating disc motor bearing; the rotating disc motor permanent magnet is surrounded by the outer side of the rotating disc motor coil winding and fixed to the rotating disc motor rotor; the rotating disc motor controller is located outside the rotating disc motor permanent magnet; the rotating disc motor brake shoes are mounted on the inner side wall of the rotating disc motor frame; the rotating disc motor hydraulic brake pump is mounted at the port of the rotating disc motor frame and connected to the rotating disc motor brake shoes; the rotating disc motor rotor is provided with brake rings that correspond to and cooperate with the rotating disc motor brake shoes; the inner side wall of the rotating disc motor frame and the outer side wall of the brake ring are provided with cooperating rotating disc motor balance guide rails, and rotating disc motor balance balls are installed between the two rotating disc motor balance guide rails.

9. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 1, 2 or 3, characterized in that: The aforementioned electric drive turntables (24), (25), (26), and (27) for adjusting the rotation angle of the fighter jet's front left wing, front right wing, rear left wing, and rear right wing all include a motor drive turntable frame (47), a motor drive turntable stator (48), a motor drive turntable rotor (49), a motor drive turntable coil winding (50), a motor drive turntable permanent magnet (51), and a motor drive turntable controller (52). The motor drive turntable bearing (53), motor drive turntable brake shoes (54), motor drive turntable wiring harness (55), motor drive turntable balance guide rail (56), motor drive turntable balance ball bearings (57), and motor drive turntable hydraulic brake pump (58) have a circular cross-section; wherein, the motor drive turntable frame (47) is a shell with a circular groove, the cylindrical motor drive turntable stator (48) is fixed at the center of the motor drive turntable frame (47), and the annular motor drive turntable coil winding (50) is fitted on the motor drive turntable. The motor stator (48) is mounted on the motor; the motor drive turntable motor rotor (49) is disc-shaped, and its center is connected to the motor drive turntable motor stator (48) through the motor drive turntable motor bearing (53); the motor drive turntable motor permanent magnet (51) is wrapped around the outside of the motor drive turntable motor coil winding (50) and fixed on the motor drive turntable motor rotor (49); the motor drive turntable motor controller (52) is located outside the motor drive turntable motor permanent magnet (51); the motor drive turntable motor brake shoes (54) are mounted on the motor drive turntable motor. On the inner wall of the motor frame (47); the motor-driven turntable hydraulic brake pump (58) is installed at the port of the motor frame (47) and connected to the motor brake shoes (54); the motor rotor (49) of the motor is provided with a brake ring that corresponds to and cooperates with the motor brake shoes (54); the inner wall of the motor frame (47) and the outer wall of the brake ring are provided with a motor-driven turntable balance guide rail (56) that cooperates with the motor, and a motor-driven turntable balance ball (57) is installed between the two motor-driven turntable balance guide rails (56).

10. A safe takeoff and landing fighter jet equipped with multiple support facilities according to claim 1, 2 or 3, characterized in that: The fighter jet fuselage (2) is equipped with fighter jet landing gear (4).

Images