UNMANNED AERIAL VEHICLE

• US 20160144954A1
• Filed: 11/16/2015
• Published: 05/26/2016
• Est. Priority Date: 11/26/2014
• Status: Abandoned Application

• Current Assignee: Skymetro UAV Technology Inc.
• Original Assignee: Skymetro UAV Technology Inc.
• Inventors: Daigle, Gilles
• Application Number:
  US14/942,469
• Publication Number:
  US 20160144954A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/16 with five or more distinct rotor axes, e.g. octocopters
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 60/50 with landing legs

Abstract

Herein is disclosed an unmanned aerial vehicle having motor arm holders configured such that when inserted into its corresponding arm holder on the central hub or holder, the motor arm holders are tilted at an angle between 6 to 10 degrees angle upwards. This drops the entire machine relative to the central hub making the UAV unit more “bottom heavy”, thus creating a pendulum effect, which is more stable in flight.

Claims

1. An unmanned aerial vehicle, comprising:

a) a landing gear including a support platform having opposed sides and a pair of landing gear legs descending from each of said opposed sides;

b) a housing and a support hub located therein;

c) a selected number of motor support arm holders evenly distributed about a periphery of said support hub;

d) each of said selected number of motor support arm holders having a proximal end portion of a corresponding motor support arm locked therein, said motor support arm holders being configured to lock the proximal end portion of the motor support arm such that the each motor support arm is inclined upwardly from horizontal by an angle in a range from about 6 to 10 degrees;

e) each motor support arm having a distal end and having a motor holder affixed thereto, and each motor holder having a propeller motor locked therein and each propeller motor having a propeller attached thereto;

f) an electronic control circuit array mounted on top of said top center plate;

g) a quick release universal utility plate releasably attached to, and spaced below, said bottom center plate, said quick release utility plate configured to releasably receive instrumentation for transportation by the unmanned aerial vehicle, said quick release universal utility plate being attached to said support platform;

h) said housing including a top canopy for enclosing and covering said electronic control circuit array and said hub which is releasably secured to said support platform; and

i) a space between said quick release utility plate and said bottom center plate configured to be a battery compartment and to receive therein one or two batteries electrically connected to said propeller motors and said electronic circuit array.

2. The unmanned aerial vehicle according to claim 1 wherein said support hub includes a top center plate and bottom center plate spaced apart and bolted together, and wherein said selected number of motor support arm holders evenly distributed about a periphery of said support hub are sandwiched between, and secured to, said top center plate and said bottom center plate.

3. The unmanned aerial vehicle according to claim 1 wherein each motor support arm is inclined upwardly from horizontal by an angle of about 8 degrees.

4. The unmanned aerial vehicle according to claim 1 wherein said motor support arms are hollow having a hollow interior, and wherein said motor holders include a port located below said propeller motor which is aligned with said hollow interior of said motor support arm so that air from propeller wash is forced through said port down said hollow interior into an interior of said support hub, and wherein said proximal ends of said motor support arms are positioned to direct said air towards said electronic circuit array for air cooling said electronic circuit array.

5. The unmanned aerial vehicle according to claim 1 wherein said motor holder includes a stabilizer fin extending below a bottom of said motor holder.

6. The unmanned aerial vehicle according to claim 5 wherein said stabilizer fin is generally triangular in shape and positioned on said bottom of said propeller motor holder so that air from the propeller wash is forced past said stabilizer fin 38 thereby acting to aid in stabilizing the unmanned aerial vehicle in flight.

7. The unmanned aerial vehicle according to claim 1 wherein said battery compartment is configured to receive one battery inserted from a side of said unmanned aerial vehicle with said one rectangular battery being centered in said battery compartment.

8. The unmanned aerial vehicle according to claim 1 wherein said battery compartment is configured to receive two batteries inserted from a front of said unmanned aerial vehicle with said two batteries being centered in said battery compartment.

9. The unmanned aerial vehicle according to claim 1 wherein said selected number of motor arm support holders is any one of four, (4), six (6), and eight (8), and including a corresponding number of support arms mounted symmetrically around the hub.

10. The unmanned aerial vehicle according to claim 1 wherein said motor support arm holders include a two (2) piece clamp including two (2) clamp sections, which upon being assembled together, between said top center plate and said bottom center plate, has an interior to receive therein said proximal end of said motor support arm, and upon being bolted together locks said motor support arm in place.

11. The unmanned aerial vehicle according to claim 1 wherein said motor support arm holders and associated motor support arms clamped therein include a locking mechanism configured to prevent rotation of the motor support arm with respect to said motor support arm holder.

12. The unmanned aerial vehicle according to claim 11 wherein said locking mechanism includes a stud located on an inner surface of at least one of said clamp sections, and said proximal end of said motor support arm clamped between said two clamp sections including a hole having a size sufficiently large to receive said stud therein.

13. The unmanned aerial vehicle according to claim 11 wherein said locking mechanism includes a stud located on the proximal end of said motor support arm and one of said two clamp sections including a hole having a size sufficiently large to receive said stud therein.

14. The unmanned aerial vehicle according to claim 1 wherein each motor holder includes a two (2) piece clamp including two (2) clamp sections, which upon being assembled together, has an interior to receive therein said distal end of said motor support arm, and upon being bolted together locks said motor holder to said motor arm, and wherein a top clamp section of said two clamp sections includes a receptacle to receive therein said propeller motor, and wherein a bottom clamp section of said two clamp sections includes a stabilizer fin integrally formed therewith on a bottom surface of said bottom clamp section.

15. The unmanned aerial vehicle according to claim 14 wherein said motor holder and associated distal end of said motor support arm clamped therein include a locking mechanism configured to prevent rotation of the motor holder with respect to said motor support arm.

16. The unmanned aerial vehicle according to claim 15 wherein said locking mechanism includes a stud located on an inner surface of at least one of said clamp sections, and said distal end of said motor support arm clamped between said two clamp sections including a hole having a size sufficiently large to receive said stud therein.

17. The unmanned aerial vehicle according to claim 15 wherein said locking mechanism includes a stud located on the distal end of said motor support arm and one of said two clamp sections including a hole having a size sufficiently large to receive said stud therein.

18. The unmanned aerial vehicle according to claim 1 wherein said motor arm holders and said motor support arms are configured such that each motor support arm is moveable in said motor arm holder between at least two positions and can be locked in each position to provide at least two pre-set lengths of the motor support arm with respect to the hub.

19. The unmanned aerial vehicle according to claim 18 wherein said motor arm holders include a two (2) piece clamp including two (2) clamp sections, which upon being assembled together, has an interior to receive therein said proximal end of said motor support arm, and upon being bolted together locks said motor arm in place.

20. The unmanned aerial vehicle according to claim 18 wherein said motor arm holders and associated motor support arms clamped therein include a locking mechanism configured to lock said motor support arms in said at least two positions with respect to said motor support arm holders, and to prevent rotation of the motor support arm with respect to said motor support arm holder when locked in each of said at least two positions.

21. The unmanned aerial vehicle according to claim 20 wherein said locking mechanism includes a stud located on an inner surface of at least one of said clamp sections, and said proximal end of said motor support arm clamped between said two clamp sections including at least two holes spaced apart having a size sufficiently large to receive said stud therein, and wherein in at least a first of said at least two positions said stud is inserted through a first hole of two holes, and in a second of said at least two positions said stud is inserted through a second hole of the two holes.

22. The unmanned aerial vehicle according to claim 20 wherein said locking mechanism includes at least two spaced studs located on the proximal end of said motor support arm and one of said two clamp sections including hole having a size sufficiently large to receive each stud therein.

23. The unmanned aerial vehicle according to claim 1 configured such that said distal end of said motor support arms are above a top surface of said canopy such that in the event said unmanned aerial vehicle is inverted upside down on the ground it rests on the propellers and not said top surface of said canopy thereby providing protection for said electronic array.

24. The unmanned aerial vehicle according to claim 1 wherein said selected number of motor arm support holders is six (6), and including a six (6) corresponding support arms mounted symmetrically around the hub.

25. The unmanned aerial vehicle according to claim 1 wherein said support platform includes a support plate mounted on spaced beams oriented at about 90 degrees to a planar surface of said support plate, each end of each of said spaced beams having a hole extending therethrough, including O-rings mounted in said holes, including a first and second tubes mounted on said support platform at opposed sides thereof with said tubes extending through corresponding ends of said spaced beams such that said support plate is slidable back and forth towards the front and back of said support platform such that when a load is attached to said support plate its center of gravity can be adjusted.

26. The unmanned aerial vehicle according to claim 1 wherein said quick release universal adapter plate includes a pair of spaced holes located at side edges of said utility plate, and wherein said support platform includes a pair of spaced plates located on the side edges of said support platform each having two spaced holes extending therethrough in registration with corresponding holes in said quick release utility plate which are used to attach said universal adapter plate to said support platform.

27. An unmanned aerial vehicle kit, comprising:

a) a landing gear including a support platform having opposed sides and a pair of landing gear legs descending from each of said opposed sides;

b) four (4), six (6) and eight (8) motor support arms;

c) support hubs for each of said four (4), six (6) and eight (8) motor support arms, each support hub including support arm holders evenly distributed about a periphery of said support hub;

d) each of said motor support arm holders having a proximal end portion of a corresponding motor support arm locked therein, said motor support arm holders being configured to lock the proximal end portion of the motor support arm such that the each motor support arm is inclined upwardly from horizontal by an angle in a range from about 6 to 10 degrees;

e) each motor support arm having a distal end and having a motor holder affixed thereto, and each motor holder having a propeller motor locked therein and each propeller motor having a propeller attached thereto;

f) an electronic control circuit array mounted on top of said top center plate;

g) a quick release universal plate releasably attached to, and spaced below, said bottom center plate, said quick release utility plate configured to releasably receive instrumentation for transportation by the unmanned aerial vehicle, said quick release universal plate being attached to said support platform;

h) a housing including a top canopy for enclosing and covering said electronic control circuit array and said hubs which is releasably secured to said support platform; and

i) a space between said quick release utility plate and said bottom center plate configured to be a battery compartment and to receive therein one or two batteries electrically connected to said propeller motors and said electronic circuit array.