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CN-224211256-U - Sports aircraft

CN224211256UCN 224211256 UCN224211256 UCN 224211256UCN-224211256-U

Abstract

The utility model relates to the technical field of aircrafts and discloses an exercise type aircrafts, which comprises an airframe, wherein an inner cavity for a user can be taken in the airframe, a plurality of motor connecting rods which are arranged at intervals and surround the airframe are arranged on the airframe, each motor connecting rod comprises a fixed section fixedly connected to the airframe and a folding section which is folded relative to the fixed section, a motor is arranged on the folding section, the motor is provided with a rotating shaft, a propeller is connected to the rotating shaft, when the airframe is in a flying state, the fixed section and the folding section are coaxially arranged, the plurality of motor connecting rods are horizontally unfolded, when the airframe is in a non-use state, the folding section is folded relative to the fixed section and is stored at the periphery of the airframe, when the airframe is in a non-use state, the folding section can be folded relative to the fixed section, the folding section is stored at the periphery of the airframe, the motor connecting rods are prevented from occupying excessive space, the storage of the exercise type aircrafts is facilitated, and the like.

Inventors

  • XIE ENLI
  • WU YUNLONG
  • GUO YUEWEI
  • FENG PING
  • LU SHAOPING
  • LIAO GUOPING
  • Chi Youwei
  • WU BOHUAN
  • WU YIFAN
  • HUANG FEILONG
  • TANG JUNYAN

Assignees

  • 希龙科技(深圳)有限公司

Dates

Publication Date
20260508
Application Date
20250626

Claims (10)

  1. 1. The sports aircraft is characterized by comprising a machine body, wherein an inner cavity for a user to sit is formed in the machine body, a plurality of motor connecting rods which are arranged in a surrounding mode at intervals are arranged on the machine body, the motor connecting rods comprise fixed sections fixedly connected to the machine body and folding sections which are folded relative to the fixed sections, a motor is arranged on the folding sections, the motor is provided with a rotating shaft, and a propeller is connected to the rotating shaft; when the machine body is in a flying state, the fixed section and the folding section are coaxially arranged, the motor connecting rods are horizontally unfolded, and when the machine body is in a non-use state, the folding section is bent and arranged relative to the fixed section and is contained at the periphery of the machine body.
  2. 2. The sports type aircraft as claimed in claim 1, wherein the top of the body is provided with a top frame, the inner ends of the fixing sections are fixedly connected with the top frame, a plurality of the fixing sections are circumferentially arranged at intervals along the top frame, and the outer ends of the fixing sections are hinged with the inner ends of the folding sections.
  3. 3. The sport-like vehicle as recited in claim 2, wherein the motor is disposed on an outer end of the folding section.
  4. 4. A sports type aircraft according to any one of claims 1 to 3, wherein a hinge structure is provided between the outer end of the fixed section and the inner end of the folding section, the folding section being folded with respect to the fixed section in a folded position with the hinge structure, the hinge structure being provided with a movably arranged fixed structure which locks the hinge structure so that the folding section is fixed relative to the fixed section, the fixed section being arranged coaxially with the folding section.
  5. 5. The sports type aircraft as defined in claim 4, wherein the hinge structure includes an outer end and an inner end hinged to the outer end, the outer end being connected to the outer end of the fixed section, the inner end being connected to the inner end of the folded section.
  6. 6. The sports type aircraft as defined in claim 5, wherein the fixing structure includes a pin movably penetrating through the inner and outer ends, the pin penetrating through the inner and outer ends to fix the fixing and folding sections relative to each other when the fixing and folding sections are coaxially arranged.
  7. 7. A sports aircraft according to any one of claims 1 to 3, wherein the fixed section extends into the interior of the roof frame and is fixedly connected to the bottom of the roof frame.
  8. 8. The sports type aircraft as claimed in claim 7, wherein the outer periphery of the roof frame is formed with a laterally arranged locating hole, the outer periphery of the locating hole is formed with an annularly arranged surrounding wall, the fixing section passes through the locating hole, and the outer periphery of the fixing section abuts against the surrounding wall.
  9. 9. A sports aircraft according to any one of claims 1 to 3, wherein the fixed section is connected to a stiffening section, the outer end of the stiffening section being connected to the fixed section and the inner end of the stiffening section being connected to the roof rack.
  10. 10. A sports type aircraft as claimed in any one of claims 1 to 3 wherein the bottom of the body has a support frame for supporting on the ground, the support frame having two support bars arranged in parallel and supported on the ground, the support bars being arranged in a curved configuration.

Description

Sports aircraft Technical Field The utility model relates to the technical field of aircrafts, in particular to an athletic aircraft. Background Aircraft generally refers to an instrument that can fly in the air, the variety of which is diversified, which is applicable to different fields of demand. Currently, sports aircrafts are also widely used in current life, as air transportation or as sports. In the prior art, the sports type aircraft comprises a machine body, wherein a motor connecting rod is arranged on the machine body, a motor is arranged on the motor connecting rod, a propeller is arranged on the motor, and the machine body is driven to fly in the air by utilizing the rotation of the propeller and is in a flying state. However, due to the large size of the motor connecting rod, when the machine body is in a non-use state, the occupied space is large, and the storage is inconvenient. Disclosure of utility model The utility model aims to provide a sports aircraft, and aims to solve the problem that in the prior art, when the sports aircraft is in a non-use state, the occupied space is large. The utility model discloses an athletic aircraft, which comprises an aircraft body, wherein the aircraft body is provided with an inner cavity for a user to sit, the aircraft body is provided with a plurality of motor connecting rods which are arranged at intervals in a surrounding way, the motor connecting rods comprise a fixed section fixedly connected to the aircraft body and a folding section which is folded relative to the fixed section, the folding section is provided with a motor, the motor is provided with a rotating shaft, and the rotating shaft is connected with a propeller; when the machine body is in a flying state, the fixed section and the folding section are coaxially arranged, the motor connecting rods are horizontally unfolded, and when the machine body is in a non-use state, the folding section is bent and arranged relative to the fixed section and is contained at the periphery of the machine body. Further, the top of organism is equipped with the top frame, the inner and the top frame fixed connection of fixed section, a plurality of fixed section is along the circumference interval surrounding arrangement of top frame, the outer end of fixed section is articulated with the inner of folding section. Further, the motor is disposed on an outer end of the folding section. Further, a hinge structure is arranged between the outer end of the fixed section and the inner end of the folding section, the folding section takes the hinge structure as a folding position and is folded relative to the fixed section, the hinge structure is provided with a movably arranged fixed structure, the fixed structure locks the hinge structure so that the folding section and the fixed section are relatively fixed, and the fixed section and the folding section are coaxially arranged. Further, the hinge structure comprises an outer end head and an inner end head hinged with the outer end head, wherein the outer end head is connected with the outer end of the fixed section, and the inner end head is connected with the inner end of the folding section. Further, the fixing structure comprises a bolt movably penetrating through the inner end socket and the outer end socket, and when the fixing section and the folding section are coaxially arranged, the bolt penetrates through the inner end socket and the outer end socket to fix the fixing section and the folding section relatively. Further, the fixed section extends to the inside of the top frame and is fixedly connected with the bottom of the top frame. Further, a positioning hole which is transversely arranged is formed in the periphery of the top frame, an annular surrounding wall which is arranged in an annular mode is formed in the periphery of the positioning hole, the fixing section penetrates through the positioning hole, and the periphery of the fixing section abuts against the surrounding wall. Further, the fixed section is connected with the reinforcing section, the outer end of the reinforcing section is connected with the fixed section, and the inner end of the reinforcing section is connected with the top frame. Further, the bottom of the machine body is provided with a supporting frame used for being supported on the ground, the supporting frame is provided with two supporting rods which are arranged in parallel and supported on the ground, and the supporting rods are arranged in a bending mode. Compared with the prior art, the inner cavity is arranged in the machine body, so that a user can sit, the motor is arranged on the motor connecting rod, the propeller is arranged on the rotating shaft of the motor, the machine body is driven to fly in the air through the rotation of the plurality of propellers, and in a flying state, when the machine body is in a non-use state, the folding section can be bent relative to the fixed section, the folding section is sto