Flying machine and flying unit

• US 20180022453A1
• Filed: 09/08/2017
• Published: 01/25/2018
• Est. Priority Date: 12/31/2016
• Status: Abandoned Application

• Current Assignee: Haoxiang Electric Energy (Kunshan) Co., Ltd.
• Original Assignee: Haoxiang Electric Energy (Kunshan) Co., Ltd.
• Inventors: Tian, Yu, Jiang, Wenyan
• Application Number:
  US15/698,641
• Publication Number:
  US 20180022453A1
• Time in Patent Office: Days
• CPC Class Codes: B64C 2211/00 Modular constructions of airplanes or helicopters
• CPC Class Codes: B64C 37/02 Flying units formed by separate aircraft towing B64D3/00; aircraft transported by aircraft B64D5/00; air-refuelling B64D39/00
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2101/60 for transporting passengers; for transporting goods other than weapons
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/10 Wings
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors
• CPC Class Codes: B64U 50/14 ducted or shrouded
• CPC Class Codes: B64U 50/19 using electrically powered motors

Abstract

A flying machine disclosed in the present application includes a main body, a flying module and a function module which is for controlling working state of the flying module. The flying module includes at least one pair of flying units, wherein the flying unit includes a flying frame, rotors and a steering oar which works with the rotors to propel the flying machine. Compared with the conventional flying machine which requires four rotors, while loaded with the same power source, the present flying machine doubles the flight time, which solve the problem of short working time.

Claims

1. A flying apparatus, comprising:

a main body;

a flying module disposed on the body; and

a function module disposed on the main body, which is configured to control a working state of the flying module;

wherein the flying module comprises at least one pair of flying units;

each of the flying units comprises;

a flying frame;

to rotors disposed on the flying frame;

a steer disposed on the flying frame, which is configured to work with the rotors to propel the flying apparatus.

2. The flying machine, as recited in claim 1, wherein the flying module comprises one pair of the flying units.

3. The flying machine, as recited in claim 2, wherein the flying frame comprises a circular wall;

wherein the circular wall, which is enclosed, forms a wind tunnel in which the flying frame is contained;

the wind tunnel comprises an air outlet;

the steering oar is disposed on the air outlet.

4. The flying machine, as recited in claim 3, wherein a mounting axis of the steering oar runs through and along a diameter of the circular wall;

the steering oar is rotatable within the flying frame.

5. The flying machine, as recited in claim 4, wherein the flying machine has a vertical indication line to indicate a moving direction;

the pair of the flying units are disposed symmetrically along a horizontal direction intersecting with the vertical indication line.

6. The flying machine, as recited in claim 5, wherein a mounting axis of the steering oar is perpendicular to the vertical indication line.

7. The flying unit, as recited in claim 3, wherein a mounting axis of the steering oar runs through and along a diameter of the circular wall;

the steering oar is rotatable within the flying frame.

8. The flying unit, as recited in claim 7, wherein a casing tube is disposed along a diameter of the flying frame, the steering oar is fixed on the casing tube, which rotates integrally with the casing tube relative to the flying frame.

9. A flying unit for experiment, comprising:

a flying frame;

rotors disposed on the flying frame; and

a steering oar disposed on the flying frame, which cooperates with the rotors to propel the flying machine;

wherein

the flying frame comprises a circular wall;

a plurality of extension arms extending on the circular wall along an axis of the circular wall; and

a coating film covers the extension arms, which forms an extension wall;

wherein the circular wall and the extension wall are enclosed to form a wind tunnel.

10. The flying unit, as recited in claim 9, wherein a plurality of axial positioning structures are disposed along an axis of the extension arms;

the coating film has a series of customized axial depth corresponding to the positioning structures.

11. A strengthened flying unit, comprising:

a flying frame;

rotors disposed on the flying frame; and

a steering oar disposed on the flying frame, which cooperates with the rotors to propel the flying machine;

wherein the flying frame comprises;

a circular wall;

a center pillar disposed in an enclosed hollow part by the circular wall; and

a rod stiffener with a first end connected to the circular wall and a second end connected to the center pillar.

12. The flying unit, as recited in claim 11, wherein a vertical height of the first end of the stiffener is higher than a vertical height of the second end of the stiffener.

13. A flying machine, comprising

a main body;

a flying module disposed on the main body;

a function module on the main body, which is for controlling working state of the flying module;

wherein the flying module comprises at least one pair of flying units;

each of the flying units comprises;

a flying frame;

rotors disposed on the flying frame;

a steering oar disposed on the flying frame, which works with the rotors to propel the flying machine;

the flying frame comprises a circular wall;

wherein a casing tube is disposed along a diameter of the circular wall, the steering oar is fixed on the casing tube, which rotates integrally with the casing tube relatively to the flying frame;

wherein the casing tube is hollow inside, which is for distributing a current traverse to provide power for the rotors to rotate.

14. The flying machine, as recited in claim 13, wherein a center pillar disposed in a center part of the circular wall of the flying frame;

the casing tube extends from the circular wall to the center pillar.