IP Library Granted Patent US 11,939,046
Granted Patent B1
US 11,939,046 · App. 17/513,256 · Granted Mar 26, 2024

Attachment sub-systems for vertically-stacked multicopters

Inventors: Benjamin Otto Berry (Mountain View, CA); Graham Bowen-Davies (San Jose, CA); Madeline Elliott Parker (San Francisco, CA); Cameron Robertson (San Mateo, CA); Christopher Scott Saunders (San Jose, CA)
Assignee: Kitty Hawk Corporation
B64C27/08B64C39/02B64C39/024B64C2211/00B64U10/13B64U30/20B64U80/70
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Quick Facts
Patent No.
US 11,939,046
App. No.
17/513,256
Granted
Mar 26, 2024
Kind
B1
Abstract

A plurality of propellers generate vertical thrust at least some of the time. An attachment sub-system detachably couples to a vertical connector, where a plurality of vertically-stacked multicopters are configured to detachably couple to the vertical connector in order to transport a load at a bottom end of the vertical connector. There is an opening in a vehicle frame that is configured to: (1) receive the vertical connector prior to the attachment sub-system detachably coupling to the vertical connector and (2) hold the vertical connector while the attachment sub-system is detachably coupled to the vertical connector.

Claims (54)

1. A system, comprising:

a plurality of propellers that generate vertical thrust at least some of the time;

an attachment sub-system that detachably couples to a vertical connector, wherein a plurality of vertically-stacked multicopters detachably couple to the vertical connector in order to transport a load at a bottom end of the vertical connector; and

an opening in a vehicle frame that: (1) receives the vertical connector prior to the attachment sub-system detachably coupling to the vertical connector and (2) holds the vertical connector while the attachment sub-system is detachably coupled to the vertical connector; wherein:

the system is included in a second-from-top multicopter in the plurality of vertically-stacked multicopters;

the attachment sub-system:

detaches from the vertical connector; and

after moving into a topmost position associated with the vertical connector, detachably couples to the vertical connector; and

the system further includes a flight controller that: after the attachment sub-system detaches from the vertical connector, generates one or more control signals for the plurality of propellers associated with moving to the topmost position.

2. The system of claim 1 , wherein:

the vertical connector includes a stopper; and

the attachment sub-system includes a passive holder that is open on at least one side where an opening of the passive holder is narrower than a width of the passive holder.

3. A system, comprising:

a plurality of propellers that generate vertical thrust at least some of the time;

an attachment sub-system that detachably couples to a vertical connector, wherein a plurality of vertically-stacked multicopters detachably couple to the vertical connector in order to transport a load at a bottom end of the vertical connector; and

an opening in a vehicle frame that: (1) receives the vertical connector prior to the attachment sub-system detachably coupling to the vertical connector and (2) holds the vertical connector while the attachment sub-system is detachably coupled to the vertical connector, wherein:

the attachment sub-system includes a non-load-bearing connector and a load-bearing connector, wherein the attachment sub-system further:

detaches the load-bearing connector from the vertical connector while keeping the non-load-bearing connector enclosed around the vertical connector; and

after flying vertically to a higher altitude, detachably couples the load-bearing connector to the vertical connector; and

the system further includes a flight controller that: after the load-bearing connector detaches from the vertical connector, generates one or more control signals for the plurality of propellers associated with flying vertically to the higher altitude.

4. The system recited in claim 3 wherein:

the system is included in a topmost multicopter in the plurality of vertically-stacked multicopters;

the flight controller further: while the attachment sub-system is detachably coupled to the vertical connector, generates one or more control signals for the plurality of propellers associated with moving to a safe position such that if the attachment sub-system were to detach from the vertical connector while in the safe position, a section of the vertical connector that is between the system and a second-from-top multicopter would be clear of one or more propellers in the second-from-top multicopter; and

the attachment sub-system further: while in the safe position, detaches from the vertical connector.

5. The system of claim 3 , wherein:

the vertical connector includes a stopper; and

the attachment sub-system includes a passive holder that is open on at least one side where an opening of the passive holder is narrower than a width of the passive holder.

6. A method, comprising:

providing a plurality of propellers that generates vertical thrust at least some of the time;

providing an attachment sub-system that detachably couples to a vertical connector, wherein a plurality of vertically-stacked multicopters are configured to detachably couple to the vertical connector in order to transport a load at a bottom end of the vertical connector; and

providing an opening in a vehicle frame that: (1) receives the vertical connector prior to the attachment sub-system detachably coupling to the vertical connector and (2) holds the vertical connector while the attachment sub-system is detachably coupled to the vertical connector, wherein:

the method is performed by a second-from-top multicopter in the plurality of vertically-stacked multicopters;

the attachment sub-system further:

detaches from the vertical connector; and

after moving into a topmost position associated with the vertical connector, detachably couples to the vertical connector; and

the second-from-top multicopter further includes a flight controller that: after the attachment sub-system detaches from the vertical connector, generates one or more control signals for the plurality of propellers associated with moving to the topmost position.

7. The method recited in claim 6 , wherein:

the vertical connector includes a stopper; and

the attachment sub-system includes a passive holder that is open on at least one side where an opening of the passive holder is narrower than a width of the passive holder.

8. A method, comprising:

providing a plurality of propellers that generates vertical thrust at least some of the time;

providing an attachment sub-system that detachably couples to a vertical connector, wherein a plurality of vertically-stacked multicopters are configured to detachably couple to the vertical connector in order to transport a load at a bottom end of the vertical connector; and

providing an opening in a vehicle frame that: (1) receives the vertical connector prior to the attachment sub-system detachably coupling to the vertical connector and (2) holds the vertical connector while the attachment sub-system is detachably coupled to the vertical connector, wherein:

the attachment sub-system includes a non-load-bearing connector and a load-bearing connector, wherein the attachment sub-system further:

detaches the load-bearing connector from the vertical connector while keeping the non-load-bearing connector enclosed around the vertical connector; and

after flying vertically to a higher altitude, detachably couples the load-bearing connector to the vertical connector; and

the method further includes providing a flight controller that: after the load-bearing connector detaches from the vertical connector, generates one or more control signals for the plurality of propellers associated with flying vertically to the higher altitude.

9. The method recited in claim 8 , wherein:

the method is performed by a topmost multicopter in the plurality of vertically-stacked multicopters;

the flight controller further: while the attachment sub-system is detachably coupled to the vertical connector, generates one or more control signals for the plurality of propellers associated with moving to a safe position such that if the attachment sub-system were to detach from the vertical connector while in the safe position, a section of the vertical connector that is between the topmost multicopter and a second-from-top multicopter would be clear of one or more propellers in the second-from-top multicopter; and

the attachment sub-system further: while in the safe position, detaches from the vertical connector.

10. The method recited in claim 8 , wherein:

the vertical connector includes a stopper; and

the attachment sub-system includes a passive holder that is open on at least one side where an opening of the passive holder is narrower than a width of the passive holder.

Assignments (3)
RELEASE OF SECURITY INTEREST Recorded May 22, 2023
From: ONE AERO, LLC
To: KITTY HAWK CORPORATION
Reel/Frame 063713/0367 →
SECURITY INTEREST Recorded Mar 25, 2022
From: KITTY HAWK CORPORATION
To: ONE AERO, LLC
Reel/Frame 059503/0382 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 4, 2022
From: BERRY, BENJAMIN OTTO; BOWEN-DAVIES, GRAHAM; PARKER, MADELINE ELLIOTT; ROBERTSON, CAMERON; SAUNDERS, CHRISTOPHER SCOTT
To: KITTY HAWK CORPORATION
Reel/Frame 059175/0926 →
Continuity (1)
Provisional Application 63107089 · Oct 29, 2020
Cited By (8)
US 12,391,414 US 12,545,447 US 12,643,696 US 12,649,593 US 12,668,383 US 12,673,792 US 12,692,029 US 12,703,525