Electric wing assembly driven by impeller

Abstract

The utility model discloses an impeller-driven electric wing assembly which comprises a flying suit body, U-shaped fixing frames are symmetrically and fixedly installed at the left end and the right end of the front side of the flying suit body, and two arms of each U-shaped fixing frame are vertically and symmetrically fixedly installed on the upper portion and the middle portion of the front side of the flying suit body respectively. Mounting seats are detachably and fixedly mounted on the front sides of the horizontal ends of the two U-shaped fixing frames through adjusting fixing assemblies, rotating assemblies are correspondingly and fixedly mounted on the upper portions of the front sides of the mounting seats, and impeller driving assemblies are fixedly mounted at the outer side ends of the two rotating assemblies correspondingly; according to the electric wing device driven by the impeller, the driving angle can be conveniently adjusted according to the flight requirement, mounting and dismounting are convenient, the mounting position can be conveniently adjusted according to the requirements of different users, the flight direction can be conveniently controlled, and the electric wing device driven by the impeller is convenient to use. And accidents are not easy to occur, and the use requirements of different users are well met.

Description

Technical Field

[0001] The utility model relates to the technical field of flying equipment, in particular to an electric wing suit driven by an impeller. Background Art

[0002] The traditional wing suit (hereinafter referred to as wing suit), also known as flying squirrel suit, is a kind of unpowered gliding flying sports equipment worn by glider athletes like clothes and pants. Its appearance is similar to bat shirt and crotch-hanging pants.

[0003] The reason why wing suit flying is possible is mainly due to the wing suit's unique wing membrane structure, that is, the ram-type inflatable airbags sewn directly under the armpits and between the legs. The ram-type inflatable airbags of the wing suit are made of nylon material with extremely high toughness and tension. In particular, large, strong, freely retractable, bat-wing-like wings are sewn directly between the legs, arms and torso of the wing suit. They can fill the flight suit with air and generate buoyancy. Gliding athletes can control the direction and speed of their bodies gliding in the air by adjusting their arms and legs.

[0004] After jumping off a platform or aircraft, gliders can unfold their wing membranes by opening their arms and legs. Then, like a flying squirrel, they use air resistance to slow down their descent while creating forward momentum. They use body swings to accurately turn and control the direction and speed of flight, and finally open their parachutes to land at a certain distance close to the ground. Wingsuit flying is known as the king of extreme sports because of its super cool first-person perspective, visual stimulation brought by unobstructed vision, and agility and control brought by direct control of the body's limbs. However, due to the small area of ​​the wing membrane, the resistance is too small, and there is no external power source, the descent speed and flight speed are too fast, with a maximum speed of 250 kilometers per hour, resulting in high risks and mortality rates, and a short time in the air of only a few minutes.

[0005] Also, due to the high risk and mortality rate of traditional wing suit flying, athletes need to undergo long-term, rigorous, and various related boring training and assessments, including at least 100 to 200 skydiving experiences, a large amount of wind tunnel wing suit flying training, etc., and expensive wing suit flying suits need to be customized. This consumes a lot of time, energy, and financial resources of athletes, and greatly affects the playability, promotion, economy, and scalability of wing suit flying.

[0006] For this reason, electric wing suits are now available on the market. However, the electric wing suits in the prior art are not convenient for adjusting the driving angle according to flight needs, and are not convenient for installation and disassembly, and for adjusting the installation position according to the needs of different users. They are also not convenient for controlling the flight direction, and accidents are prone to occur. Utility Model Content

[0007] In order to effectively solve the problems in the background technology and overcome the technical defects in the prior art, the utility model provides the following technical solutions:

[0008] An impeller-driven electric wing suit comprises a flight suit main body, wherein U-shaped fixing frames are symmetrically fixedly installed on the left and right ends of the front side of the flight suit main body, and two arms of the U-shaped fixing frames are symmetrically fixedly installed on the upper and middle parts of the front side of the flight suit main body respectively, and a mounting seat is detachably fixedly installed on the front side of the horizontal ends of the two U-shaped fixing frames by adjusting the fixing components, a rotating component is correspondingly fixedly installed on the upper part of the front side of the mounting seat, and impeller driving components are respectively fixedly installed on the outer ends of the two rotating components, and a synchronous driving component corresponding to the two rotating components is fixedly installed on the lower part of the front side of the mounting seat.

[0009] As a preferred technical solution of the utility model, the adjustment and fixing assembly includes a groove, an adjustment hole, a fixing bolt, a nut and a fixing hole. The left and right ends of the rear side of the mounting seat are symmetrically provided with grooves, and the two grooves are respectively movably connected with the horizontal ends of the two U-shaped fixing frames in front and back correspondence. The horizontal ends of the U-shaped fixing frames are provided with adjustment holes arranged from top to bottom, and the front side of the mounting seat is provided with fixing holes connecting the grooves and corresponding to the adjustment holes. The fixing holes are correspondingly provided with fixing bolts, and the tail ends of the fixing bolts passing through the corresponding adjustment holes are matched with nuts.

[0010] As a preferred technical solution of the utility model, the rotating assembly includes a rotating shaft, a fixed plate and a driven bevel gear. The fixed plate is fixed on the front side of the mounting seat, the outer side of the fixed plate is rotatably connected to the rotating shaft, and the inner end of the rotating shaft extending to the inner side of the fixed plate is fixedly installed with the driven bevel gear.

[0011] As a preferred technical solution of the utility model, the impeller drive assembly includes a drive motor, a mounting cylinder and an impeller, the outer end of the rotating shaft is fixedly mounted with a mounting cylinder with an upper end opening, the bottom of the mounting cylinder is fixedly mounted with a drive motor, and the top end of the drive motor output shaft is fixedly mounted with an impeller.

[0012] As a preferred technical solution of the utility model, the synchronous drive assembly includes a synchronous drive motor, a bracket and a driving bevel gear. The bracket is fixedly installed on the front side of the mounting seat, the synchronous drive motor is fixedly installed on the bottom of the bracket, and the driving bevel gear is installed on the top of the output shaft of the synchronous drive motor. The driving bevel gear is meshed with the driven bevel gear accordingly.

[0013] As a preferred technical solution of the utility model, a lithium battery is fixedly mounted on the front side of the mounting seat.

[0014] As a preferred technical solution of the utility model, an electronic gyroscope is fixedly mounted on the front side of the mounting seat.

[0015] As a preferred technical solution of the present utility model, a controller is fixedly mounted on the mounting seat.

[0016] As a preferred technical solution of the utility model, it also includes an electric parachute assembly, which includes a fixing frame, a parachute battery, a control device and an O-shaped parachute bag. The fixing frame is fixedly installed on the rear side of the flight suit body, the parachute battery is fixedly installed in the fixing frame, the control device is fixedly installed on the rear side of the fixing frame, and the O-shaped parachute bag is fixedly installed on the rear side of the control device.

[0017] As a preferred technical solution of the utility model, a heat insulation layer is fixedly installed between the fixing frame and the flight suit body.

[0018] Compared with the prior art, the beneficial effects of the utility model are as follows: the impeller-driven electric wing suit has a reasonable and practical structure, is easy to operate, is convenient for adjusting the driving angle according to flight needs, is convenient for installation and disassembly, and can adjust the installation position according to the needs of different users, and is convenient for controlling the flight direction, is not prone to accidents, and well meets the use needs of different users; specifically, through the joint cooperation of the synchronous drive assembly, the driving angle can be adjusted according to flight needs, and through the joint cooperation of the U-shaped fixing frame, the mounting seat and the adjustment fixing assembly, convenient installation and disassembly and adjustment of the installation position can be carried out, power can be provided by a lithium battery, and the flight direction can be controlled by the joint cooperation of the electronic gyroscope and the controller. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a structural schematic diagram of the utility model.

[0020] Figure 2 It is a structural schematic diagram of the main body of the flight suit of the present utility model.

[0021] Figure 3 It is a structural schematic diagram of the mounting seat of the utility model.

[0022] Figure 4 It is a partial structural schematic diagram of the utility model.

[0023] Figure 5 It is a structural schematic diagram of the electric parachute assembly of the utility model.

[0024] In the figure: a flight suit body 1, a U-shaped fixing frame 2, a mounting seat 3, an adjustment fixing assembly 4, a groove 41, an adjustment hole 42, a fixing bolt 43, a nut 44, a fixing hole 45, a rotating assembly 5, a rotating shaft 51, a fixing plate 52, a driven bevel gear 53, an impeller drive assembly 6, a drive motor 61, a mounting tube 62, an impeller 63, a synchronous drive assembly 7, a synchronous drive motor 71, a bracket 72, an active bevel gear 73, a lithium battery 8, an electronic gyroscope 9, a controller 10, an electric parachute assembly 11, a fixing frame 111, an umbrella battery 112, a control device 113, an umbrella bag 114, and an insulation layer 12. DETAILED DESCRIPTION

[0025] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0026] See also Figure 1-4 The utility model provides a technical solution: an impeller-driven electric wing suit, comprising a flight suit main body 1, with U-shaped fixing frames 2 symmetrically fixedly installed on the left and right ends of the front side of the flight suit main body 1, and two arms of the U-shaped fixing frame 2 are symmetrically fixedly installed on the upper and middle parts of the front side of the flight suit main body 1 respectively, and a mounting seat 3 is detachably fixedly installed on the front side of the horizontal ends of the two U-shaped fixing frames 2 by adjusting a fixing component 4, a rotating component 5 is correspondingly fixedly installed on the upper part of the front side of the mounting seat 3, and impeller driving components 6 are respectively fixedly installed on the outer ends of the two rotating components 5, and a synchronous driving component 7 corresponding to the two rotating components 5 is fixedly installed on the lower part of the front side of the mounting seat 3.

[0027] Further, such as Figure 2 and 3As shown, the adjustment and fixing component 4 includes a groove 41, an adjustment hole 42, a fixing bolt 43, a nut 44 and a fixing hole 45. The left and right ends of the rear side of the mounting seat 3 are symmetrically provided with grooves 41. The two grooves 41 are respectively movably connected with the horizontal ends of the two U-shaped fixing frames 2 in front and back correspondence. The horizontal ends of the U-shaped fixing frames 2 are arranged from top to bottom with adjustment holes 42. The front side of the mounting seat 3 is provided with fixing holes 45 that are connected to the grooves 41 and correspond to the adjustment holes 42. The fixing holes 45 are correspondingly provided with fixing bolts 43. The tail ends of the fixing bolts 43 that pass through the corresponding adjustment holes 42 are matched with nuts 44. By sliding the grooves 41 on the mounting seat 3 on the U-shaped fixing frame 2, the fixing holes 45 can be adjusted and aligned with different adjustment holes 42 as needed, and then fixed by fixing bolts 43 and nuts 44, so as to facilitate installation and disassembly and adjust the installation position according to the needs of different users.

[0028] Further, such as Figure 4 As shown, the rotating assembly 5 includes a rotating shaft 51, a fixed plate 52 and a driven bevel gear 53. The fixed plate 52 is fixed to the front side of the mounting seat 3. The outer side of the fixed plate 52 is rotatably connected to the rotating shaft 51. The rotating shaft 51 extends to the inner end of the inner side of the fixed plate 52 and is fixedly installed with the driven bevel gear 53.

[0029] Further, such as Figure 4 As shown, the impeller drive assembly 6 includes a drive motor 61, a mounting tube 62 and an impeller 63. The outer end of the rotating shaft 51 is fixedly mounted with a mounting tube 62 with an upper end open, the bottom of the mounting tube 62 is fixedly mounted with a drive motor 61, and the top of the output shaft of the drive motor 61 is fixedly mounted with an impeller 63. The impeller 63 is driven to rotate by the drive motor 61, so that flight driving can be performed.

[0030] Further, such as Figure 4 As shown, the synchronous drive assembly 7 includes a synchronous drive motor 71, a bracket 72 and a driving bevel gear 73. The bracket 72 is fixedly mounted on the front side of the mounting seat 3. The synchronous drive motor 71 is fixedly mounted on the bottom of the bracket 72. The driving bevel gear 73 is mounted on the top of the output shaft of the synchronous drive motor 71. The driving bevel gear 73 is correspondingly meshed with the driven bevel gear 53. The driving bevel gear 73 is driven to rotate by the synchronous drive motor 71, thereby driving the rotation of the rotating shaft 51 and the impeller drive assembly 6 (the forward and reverse angles do not exceed 180°). The drive angle can be adjusted according to flight needs, thereby facilitating the control of the flight direction.

[0031] Further, such as Figure 3 As shown, a lithium battery 8 is fixedly mounted on the front side of the mounting base 3, and the lithium battery 8 can provide power.

[0032] Further, such as Figure 3As shown, an electronic gyroscope 9 is fixedly mounted on the front side of the mounting seat 3 .

[0033] Further, such as Figure 3 As shown, a controller 10 is fixedly mounted on the mounting seat 3. The flight direction can be controlled through the cooperation of the electronic gyroscope 9 and the controller 10. The working principle is an existing mature technology and will not be further described here.

[0034] Furthermore, it also includes an electric parachute assembly 11, which includes a fixing frame 111, an umbrella battery 112, a control device 113 and an O-shaped umbrella bag 114. The fixing frame 111 is fixedly installed on the rear side of the flight suit body 1, and the umbrella battery 112 is fixedly installed in the fixing frame 111. The rear side of the fixing frame 111 is fixedly installed with a control device 113, and the rear side of the control device 113 is fixedly installed with an O-shaped umbrella bag 114 (a flying saucer-shaped O-shaped umbrella bag is used to prevent it from tipping to one side during the use of the function). Specifically, the electric parachute assembly 11 is arranged on the wing suit, and the electric parachute assembly 11 can be used to control the wing suit when the person is not gliding. The parachute assembly 11 automatically flies into the air, which is equivalent to expanding the wingspan area ten times, thereby ensuring that the lift can lift people into the air even when there is no wind, and there will be no accidents caused by falling due to insufficient lift (the use method and working principle of the electric parachute assembly 11 are existing technologies and will not be described in detail here). The electric parachute assembly 11 used in the present invention adopts common general equipment commonly used in the prior art, weighs 5 kilograms, is made of high-strength lightweight materials, and has multiple lift micro motors. The labor-saving size can be adjusted according to needs during use. The battery is rechargeable and has a battery life of half an hour. The control buttons use conventional buttons and are fixed to the arm position when in use for easy operation.

[0035] Furthermore, a heat insulating layer 12 is fixedly installed between the fixing frame 111 and the flight suit body 1 . Specifically, the heat insulating layer 12 may be a heat insulating tile or a heat insulating cotton.

[0036] When using:

[0037] The flight suit body 1 is worn on the user, and the fixing hole 45 can be adjusted and aligned with different adjustment holes 42 as needed by sliding the groove 41 on the mounting seat 3 on the U-shaped fixing frame 2, and then fixed by fixing bolts 43 and nuts 44; during the flight of the wing suit, the flight direction can be controlled by the joint cooperation of the electronic gyroscope 9 and the controller 10, and the flight drive can be performed by driving the impeller 63 to rotate by the driving motor 61. When the driving angle needs to be adjusted, the driving bevel gear 73 is driven to rotate by the synchronous driving motor 71, and then the rotating shaft 51 and the impeller driving assembly 6 are driven to rotate, so that the driving angle can be adjusted according to the flight needs, and the lithium battery 8 can provide power.

[0038] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An impeller-driven electric wing suit, comprising a flight suit body (1), characterized in that: A U-shaped fixing frame (2) is symmetrically fixedly installed at the left and right ends of the front side of the flight suit body (1), and two arms of the U-shaped fixing frame (2) are respectively symmetrically fixedly installed at the upper part and the middle part of the front side of the flight suit body (1). The front sides of the horizontal ends of the two U-shaped fixing frames (2) are detachably fixedly installed with a mounting seat (3) by adjusting a fixing assembly (4), and a rotating assembly (5) is correspondingly fixedly installed at the upper part of the front side of the mounting seat (3), and the outer ends of the two rotating assemblies (5) are respectively fixedly installed with an impeller driving assembly (6), and the lower part of the front side of the mounting seat (3) is fixedly installed with a synchronous driving assembly (7) corresponding to the two rotating assemblies (5).

2. The impeller-driven electric wing suit according to claim 1, characterized in that: The adjusting and fixing assembly (4) comprises a groove (41), an adjusting hole (42), a fixing bolt (43), a nut (44) and a fixing hole (45); the grooves (41) are symmetrically provided at the left and right ends of the rear side of the mounting seat (3); the two grooves (41) are respectively and movably engaged with the horizontal ends of the two U-shaped fixing frames (2) in a front-to-back corresponding manner; the horizontal ends of the U-shaped fixing frames (2) are provided with adjusting holes (42) arranged from top to bottom; the front side of the mounting seat (3) is provided with fixing holes (45) communicating with the grooves (41) and corresponding to the adjusting holes (42); the fixing bolts (43) are correspondingly provided in the fixing holes (45); and the tail ends of the fixing bolts (43) passing through the corresponding adjusting holes (42) are matched with nuts (44).

3. The impeller-driven electric wing suit according to claim 1, characterized in that: The rotating assembly (5) comprises a rotating shaft (51), a fixing plate (52) and a driven bevel gear (53); the fixing plate (52) is fixed to the front side of the mounting seat (3); the outer side of the fixing plate (52) is rotatably connected to the rotating shaft (51); the inner end of the rotating shaft (51) extending to the inner side of the fixing plate (52) is fixedly mounted with the driven bevel gear (53).

4. The impeller-driven electric wing suit according to claim 3, characterized in that: The impeller drive assembly (6) comprises a drive motor (61), a mounting tube (62) and an impeller (63); the outer end of the rotating shaft (51) is fixedly mounted with a mounting tube (62) with an upper end open; the bottom of the mounting tube (62) is fixedly mounted with a drive motor (61); and the top end of the output shaft of the drive motor (61) is fixedly mounted with an impeller (63).

5. The impeller-driven electric wing suit according to claim 3, characterized in that: The synchronous drive assembly (7) comprises a synchronous drive motor (71), a bracket (72) and a driving bevel gear (73); the bracket (72) is fixedly mounted on the front side of the mounting seat (3); the synchronous drive motor (71) is fixedly mounted on the bottom of the bracket (72); the driving bevel gear (73) is mounted on the top end of the output shaft of the synchronous drive motor (71); the driving bevel gear (73) is correspondingly meshed with the driven bevel gear (53).

6. The impeller-driven electric wing suit according to claim 1, characterized in that: A lithium battery (8) is fixedly mounted on the front side of the mounting seat (3).

7. The impeller-driven electric wing suit according to claim 1, characterized in that: An electronic gyroscope (9) is fixedly mounted on the front side of the mounting seat (3).

8. The impeller-driven electric wing suit according to claim 1, characterized in that: A controller (10) is correspondingly fixedly mounted on the mounting seat (3).

9. The impeller-driven electric wing suit according to claim 1, characterized in that: The invention also comprises an electric parachute assembly (11), the electric parachute assembly (11) comprising a fixing frame (111), a parachute battery (112), a control device (113) and an O-shaped parachute bag (114), the fixing frame (111) being fixedly mounted on the rear side of a flight suit body (1), the parachute battery (112) being fixedly mounted in the fixing frame (111), the control device (113) being fixedly mounted on the rear side of the fixing frame (111), and the O-shaped parachute bag (114) being fixedly mounted on the rear side of the control device (113).

10. The impeller-driven electric wing suit according to claim 9, characterized in that: A heat insulation layer (12) is fixedly installed correspondingly between the fixing frame (111) and the flight suit body (1).

Images