WO2019109622A1 - Optimizing propeller direction in drone design using onboard network of sensors - Google Patents
Optimizing propeller direction in drone design using onboard network of sensors Download PDFInfo
- Publication number
- WO2019109622A1 WO2019109622A1 PCT/CN2018/091592 CN2018091592W WO2019109622A1 WO 2019109622 A1 WO2019109622 A1 WO 2019109622A1 CN 2018091592 W CN2018091592 W CN 2018091592W WO 2019109622 A1 WO2019109622 A1 WO 2019109622A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- drone
- rotatable
- propellers
- sensors
- movement
- Prior art date
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- 238000005516 engineering process Methods 0.000 claims description 5
- 238000004891 communication Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/20—Vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/296—Rotors with variable spatial positions relative to the UAV body
- B64U30/297—Tilting rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8236—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft including pusher propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/296—Rotors with variable spatial positions relative to the UAV body
Definitions
- the present disclosure relates generally to drone based systems, and more specifically to optimizing propeller direction in drone design using an onboard network of sensors.
- a drone corresponds to a flying object of a shape such as a plane or a helicopter flying by a control signal of a radio wave while not carrying a human. They may carry various items such as cameras, sensors, and communications equipment. Drones can vary greatly in terms of size and complexity.
- a drone includes a propulsion system, a power source for powering the propulsion system, a steering mechanism, a controller including a remote communication system, and a frame maintaining all other components.
- the small-sized drones include multiple propellers or rotors to reduce an overall footprint of the drone while increasing lift, each propeller provided with an electric motor.
- rotors include, but are not limited to banana-type twin-rotors, counter-rotating coaxial rotors, quadcopter and quadrotors.
- a drone that includes a set of rotatable and fixed propellers powered by one or more battery powered electric motor for providing upward/forward thrust to the drone during upward/forward movement of the drone respectively.
- the rotatable propellers are rotatable from 0-90 degrees according to the direction of movement of the drone.
- the rotatable propellers when the rotatable propellers are disposed in a plane parallel to the wings of the drone, during the upward movement of the drone, they provide an upward thrust to the drone, facilitating the drone to lift higher and remain in the air for a longer duration, thereby increasing the flying time of the drone, and optimizing the battery usage.
- first and second rotatable propellers when they and are in a plane perpendicular to the wings during the forward movement of the drone, they provide a forward thrust to the drone, facilitating the drone to remain in the air for a longer duration, thereby increasing the flying time of the drone, and optimizing the battery usage.
- FIG. 1 illustrates a drone moving in an upward direction, in accordance with an embodiment of the present invention
- FIG.2 illustrates a drone moving in a forward direction, in accordance with an embodiment of the present invention.
- FIG. 3 illustrates a camera of the drone, in accordance with an embodiment of the present invention.
- FIG. 1 illustrates a drone 100 moving in an upward direction, in accordance with an embodiment of the present invention.
- the drone 100 is a shape of an aircraft with wings 102, first and second rotatable propellers 104a and 104b, and first, second and third fixed propellers 104c, 104d (not shown) and 104e (hereinafter collectively referred to as propellers 104). It will be apparent to a person skilled in the art that further propellers 104 may be added to the drone 100, without limiting the scope of the disclosure.
- the propellers 104 may be powered by one or more battery powered electric motors (not shown) and provide necessary upward/forward thrust to the drone 100 during upward/forward movement of the drone 100 respectively.
- the drone 100 may be remotely controlled by a remote control device using RF technology.
- the drone 100 includes a processor so that it can be remotely controlled using an application executing on a smart phone of the user.
- the first rotatable propeller 104a is fixedly attached to a first attachment 108a that is rotatably attached to a front end of a first hanger 110a.
- the second rotatable propeller 104b is fixedly attached to a second attachment 108b that is rotatably attached to a front end of a second hanger 110a.
- the first and second attachments 108a and 108b are rotatable so as to rotate the first and second rotatable propellers 104a and 104b from 0-90 degrees according to the direction of movement of the drone 100.
- the first and second attachments 108a and 108b may be rotated either manually or automatically so as to set the first and second rotatable propellers 104a and 104b in a plane parallel to the wings 102.
- the first and second rotatable propellers 104a and 104b are disposed in a plane parallel to the wings 102 during the upward movement of the drone 100, they provide an upward thrust to the drone 100, facilitating the drone 100 to lift higher and remain in the air for a longer duration, thereby increasing the flying time of the drone 100, and optimizing the battery usage.
- the drone 100 includes one or more on-board sensors (not shown) such as wind direction sensor, speed sensor, thermos sensor, drone direction sensor, so as to automatically/manually align the first and second rotatable propellers 104a and 104b in the direction of the movement of the drone 100.
- sensors such as wind direction sensor, speed sensor, thermos sensor, drone direction sensor, so as to automatically/manually align the first and second rotatable propellers 104a and 104b in the direction of the movement of the drone 100.
- the drone 100 carries a camera 112 that may be used to do aerial scanning of the outdoor environment, wherein the aerial scanning results in two-dimensional/three dimensional view of the outdoor environment. It will be apparent to a person skilled in the art that further cameras, RGB cameras, sensors may be added to the drone 100, without limiting the scope of the disclosure.
- FIG.2 illustrates the drone 100 moving in a forward direction, in accordance with an embodiment of the present invention.
- the first and second attachments 108a and 108b may be rotated either manually or automatically so as to set the first and second rotatable propellers 104a and 104b in a plane perpendicular to the wings 102.
- the first and second rotatable propellers 104a and 104b are in a plane perpendicular to the wings 102 during the forward movement of the drone 100, they provide a forward thrust to the drone 100, facilitating the drone 100 to remain in the air for a longer duration, thereby increasing the flying time of the drone 100, and optimizing the battery usage.
- FIG.3 illustrates an inbuilt camera 114 embedded in the drone 100 for performing an aerial scanning of the outdoor environment, in accordance with an embodiment of the present invention.
- the drone 100 may be used for applications other than capturing videos/images, without limiting the scope of the disclosure.
- the drone 100 may be used for remote sensing applications, delivery applications, commercial aerial surveillance, commercial and motion picture filmmaking, oil, gas and mineral exploration, disaster relief, real estate and construction, and recreational use.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Abstract
A drone (100) includes one or more rotatable propellers (104a, 104b) and one or more fixed propellers (104c, 104d, 104e) powered by one or more battery powered electric motors for providing upward and forward thrust to the drone (100) during upward and forward movement of the drone (100) respectively. The drone (100) includes a set of sensors, so as to align the rotatable propellers (104a, 104b) in the direction of the movement of the drone (100) based on sensed data.
Description
TECHNICAL FIELD
The present disclosure relates generally to drone based
systems, and more specifically to optimizing propeller direction in drone
design using an onboard network of sensors.
BACKGROUND
A drone corresponds to a flying object of a shape such
as a plane or a helicopter flying by a control signal of a radio wave while not
carrying a human. They may carry various items such as cameras, sensors, and
communications equipment. Drones can vary greatly in terms of size and
complexity. Typically, a drone includes a propulsion system, a power source for
powering the propulsion system, a steering mechanism, a controller including a
remote communication system, and a frame maintaining all other components.
The small-sized drones include multiple propellers or
rotors to reduce an overall footprint of the drone while increasing lift, each
propeller provided with an electric motor. Examples of rotors include, but are
not limited to banana-type twin-rotors, counter-rotating coaxial rotors,
quadcopter and quadrotors.
However, existing drones are not able to achieve very
high flying heights and also not able to stay in air for a long time, because
of limited battery available. Small drones typically employ battery-powered
electric motors, and it is not possible to increase the size of battery as it
may affect the overall weight of the drone.
In light of the above, a need exists for increasing the
flying time of a drone without increasing the size of the battery.
SUMMARY
In accordance with an embodiment of the present
disclosure, there is provided a drone that includes a set of rotatable and
fixed propellers powered by one or more battery powered electric motor for
providing upward/forward thrust to the drone during upward/forward movement of
the drone respectively.
In accordance with an embodiment of the present
disclosure, the rotatable propellers are rotatable from 0-90 degrees according
to the direction of movement of the drone.
In accordance with an embodiment of the present
disclosure, when the rotatable propellers are disposed in a plane parallel to
the wings of the drone, during the upward movement of the drone, they provide
an upward thrust to the drone, facilitating the drone to lift higher and remain
in the air for a longer duration, thereby increasing the flying time of the
drone, and optimizing the battery usage.
In accordance with an embodiment of the present
disclosure, when the first and second rotatable propellers and are in a plane
perpendicular to the wings during the forward movement of the drone, they
provide a forward thrust to the drone, facilitating the drone to remain in the
air for a longer duration, thereby increasing the flying time of the drone, and
optimizing the battery usage.
It will be appreciated that features of the present
disclosure are susceptible to being combined in various combinations without
departing from the scope of the present disclosure as defined by the appended
claims.
BRIEF DESCRIPTION OF THE DRAWINGS
In the following description, for purposes of
explanation, numerous specific details are set forth in order to provide a
thorough understanding of the invention. It will be apparent, however, to one
skilled in the art that the invention can be practiced without these specific
details. In other instances, structures and devices are shown in block diagram
form only in order to avoid obscuring the invention.
The present invention, in accordance with one or more
various embodiments, is described in detail with reference to the following
figures. The drawings are provided for purposes of illustration only and merely
depict exemplary embodiments of the invention. These drawings are provided to
facilitate the reader’s understanding of the invention and shall not be
considered limiting of the breadth, scope, or applicability of the invention.
It should be noted that for clarity and ease of illustration these drawings are
not necessarily made to scale.
FIG. 1 illustrates a drone moving in an upward
direction, in accordance with an embodiment of the present invention;
FIG.2 illustrates a drone moving in a forward
direction, in accordance with an embodiment of the present invention; and
FIG. 3 illustrates a camera of the drone, in
accordance with an embodiment of the present invention.
DETAILED DESCRIPTION
In the following description, for purposes of
explanation, numerous specific details are set forth in order to provide a
thorough understanding of the invention. It will be apparent, however, to one
skilled in the art that the invention can be practiced without these specific
details. In other instances, structures and devices are shown in block diagram
form only in order to avoid obscuring the invention.
Reference in this specification to “one embodiment” or
“an embodiment” means that a particular feature, structure, or characteristic
described in connection with the embodiment is included in at least one
embodiment of the invention. The appearance of the phrase “in one embodiment”
in various places in the specification are not necessarily all referring to the
same embodiment, nor are separate or alternative embodiments mutually exclusive
of other embodiments. Moreover, various features are described which may be
exhibited by some embodiments and not by others. Similarly, various
requirements are described which may be requirements for some embodiments but
not other embodiments.
Moreover, although the following description contains
many specifics for the purposes of illustration, anyone skilled in the art will
appreciate that many variations and/or alterations to said details are within
the scope of the present invention. Similarly, although many of the features of
the present invention are described in terms of each other, or in conjunction
with each other, one skilled in the art will appreciate that many of these
features can be provided independently of other features. Accordingly, this
description of the invention is set forth without any loss of generality to,
and without imposing limitations upon, the invention.
FIG. 1 illustrates a drone 100 moving in an upward
direction, in accordance with an embodiment of the present invention.
The drone 100 is a shape of an aircraft with wings
102, first and second rotatable propellers 104a and 104b, and first, second and
third fixed propellers 104c, 104d (not shown) and 104e (hereinafter
collectively referred to as propellers 104). It will be apparent to a person
skilled in the art that further propellers 104 may be added to the drone 100,
without limiting the scope of the disclosure.
The propellers 104 may be powered by one or more
battery powered electric motors (not shown) and provide necessary
upward/forward thrust to the drone 100 during upward/forward movement of the
drone 100 respectively.
In an embodiment, the drone 100 may be remotely
controlled by a remote control device using RF technology. In another
embodiment, the drone 100 includes a processor so that it can be remotely
controlled using an application executing on a smart phone of the user.
In an embodiment of the present invention, the first
rotatable propeller 104a is fixedly attached to a first attachment 108a that is
rotatably attached to a front end of a first hanger 110a. Similarly, the second
rotatable propeller 104b is fixedly attached to a second attachment 108b that
is rotatably attached to a front end of a second hanger 110a. The first and
second attachments 108a and 108b are rotatable so as to rotate the first and
second rotatable propellers 104a and 104b from 0-90 degrees according to the
direction of movement of the drone 100.
As illustrated in FIG.1, during the upward movement of
the drone 100, the first and second attachments 108a and 108b may be rotated
either manually or automatically so as to set the first and second rotatable
propellers 104a and 104b in a plane parallel to the wings 102. When the first
and second rotatable propellers 104a and 104b are disposed in a plane parallel
to the wings 102 during the upward movement of the drone 100, they provide an
upward thrust to the drone 100, facilitating the drone 100 to lift higher and
remain in the air for a longer duration, thereby increasing the flying time of
the drone 100, and optimizing the battery usage.
In an embodiment of the present invention, the drone
100 includes one or more on-board sensors (not shown) such as wind direction
sensor, speed sensor, thermos sensor, drone direction sensor, so as to
automatically/manually align the first and second rotatable propellers 104a and
104b in the direction of the movement of the drone 100.
In an embodiment, the drone 100 carries a camera 112
that may be used to do aerial scanning of the outdoor environment, wherein the
aerial scanning results in two-dimensional/three dimensional view of the
outdoor environment. It will be apparent to a person skilled in the art that
further cameras, RGB cameras, sensors may be added to the drone 100, without
limiting the scope of the disclosure.
FIG.2 illustrates the drone 100 moving in a forward
direction, in accordance with an embodiment of the present invention.
During the forward movement of the drone 100, the
first and second attachments 108a and 108b may be rotated either manually or
automatically so as to set the first and second rotatable propellers 104a and
104b in a plane perpendicular to the wings 102. When the first and second
rotatable propellers 104a and 104b are in a plane perpendicular to the wings
102 during the forward movement of the drone 100, they provide a forward thrust
to the drone 100, facilitating the drone 100 to remain in the air for a longer
duration, thereby increasing the flying time of the drone 100, and optimizing
the battery usage.
FIG.3 illustrates an inbuilt camera 114 embedded in
the drone 100 for performing an aerial scanning of the outdoor environment, in
accordance with an embodiment of the present invention.
It will be further apparent to a person skilled in the
art that the drone 100 may be used for applications other than capturing
videos/images, without limiting the scope of the disclosure. For example, the
drone 100 may be used for remote sensing applications, delivery applications,
commercial aerial surveillance, commercial and motion picture filmmaking, oil,
gas and mineral exploration, disaster relief, real estate and construction, and
recreational use.
Numerous specific details may be set forth herein to
provide a thorough understanding of a number of possible embodiments of a drone
incorporating the present disclosure. It will be understood by those skilled in
the art, however, that the embodiments may be practiced without these specific
details. In other instances, well-known methods, procedures, components and
circuits have not been described in detail so as not to obscure the
embodiments. It can be appreciated that the specific structural and functional
details disclosed herein may be representative and do not necessarily limit the
scope of the embodiments.
Although the invention is described above in terms of
various exemplary embodiments and implementations, it should be understood that
the various features, aspects and functionality described in one or more of the
individual embodiments are not limited in their applicability to the particular
embodiment with which they are described, but instead can be applied, alone or
in various combinations, to one or more of the other embodiments of the
invention, whether or not such embodiments are described and whether or not
such features are presented as being a part of a described embodiment. Thus,
the breadth and scope of the present invention should not be limited by any of
the above-described exemplary embodiments.
Terms and phrases used in this document, and
variations thereof, unless otherwise expressly stated, should be construed as
open ended as opposed to limiting. As examples of the foregoing: the term
“including” should be read as meaning “including, without limitation” or the
like; the term “example” is used to provide exemplary instances of the item in
discussion, not an exhaustive or limiting list thereof; the terms “a” or “an”
should be read as meaning “at least one,” “one or more” or the like; and
adjectives such as “conventional,” “traditional,” “normal,” “standard,” “known”
and terms of similar meaning should not be construed as limiting the item
described to a given time period or to an item available as of a given time,
but instead should be read to encompass conventional, traditional, normal, or
standard technologies that may be available or known now or at any time in the
future. Likewise, where this document refers to technologies that would be
apparent or known to one of ordinary skill in the art, such technologies
encompass those apparent or known to the skilled artisan now or at any time in
the future.
Although the invention is described above in terms of
various exemplary embodiments and implementations, it should be understood that
the various features, aspects and functionality described in one or more of the
individual embodiments are not limited in their applicability to the particular
embodiment with which they are described, but instead can be applied, alone or
in various combinations, to one or more of the other embodiments of the
invention, whether or not such embodiments are described and whether or not
such features are presented as being a part of a described embodiment. Thus,
the breadth and scope of the present invention should not be limited by any of
the above-described exemplary embodiments.
Claims (6)
- A drone, comprising:a plurality of fixed propellers;a plurality of rotatable propellers, wherein each rotatable propeller is configured to rotate in a range of 0 to 90 degrees in accordance with a direction of the movement of the drone; anda set of sensors for aligning the plurality of rotatable propellers in the direction of the movement of the drone based on sensed data.,
- The drone as claimed in claim 1, where the drone is remotely controlled by a remote control device using RF technology.
- The drone as claimed in claim 1, where the drone includes a processor so that it is remotely controlled using an application executing on a smart phone of a user.
- The drone as claimed in claim 1, wherein during the upward movement of the drone, each rotatable propeller may be rotated either manually or automatically so as to set each rotatable propeller parallel to wings of the drone.
- The drone as claimed in claim 1, wherein during the forward movement of the drone, each rotatable propeller may be rotated either manually or automatically so as to set each rotatable propeller perpendicular to wings of the drone.
- The drone as claimed in claim 1 further comprising a camera embedded therein for performing an aerial scanning of outdoor environment.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201762595082P | 2017-12-06 | 2017-12-06 | |
US62/595,082 | 2017-12-06 |
Publications (1)
Publication Number | Publication Date |
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WO2019109622A1 true WO2019109622A1 (en) | 2019-06-13 |
Family
ID=62961019
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2018/091592 WO2019109622A1 (en) | 2017-12-06 | 2018-06-15 | Optimizing propeller direction in drone design using onboard network of sensors |
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CN (1) | CN108341050A (en) |
WO (1) | WO2019109622A1 (en) |
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WO2024263593A3 (en) * | 2023-06-19 | 2025-04-10 | Method Aeronautics, LLC | Vertical take-off and landing aircraft |
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- 2018-01-30 CN CN201810087201.8A patent/CN108341050A/en active Pending
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CN108341050A (en) | 2018-07-31 |
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