• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The rotary wing drone comprises at least one rotor carried by a drone structure (10), the drone structure (10) comprising a drone body (12) and at least one arm group (18) comprising a plurality of arms (14). ) rotatably mounted on the drone body (12) about a same axis of rotation (A) between an unfolded position for the flight and a folded position for transport.
    公开号:FR3070607A1
    申请号:FR1758270
    申请日:2017-09-07
    公开日:2019-03-08
    发明作者:Christine Caubel
    申请人:Parrot Drones SAS；
    IPC主号:
    专利说明:

    Rotary airfoil drone comprising a foldable drone structure
    The present invention relates to the field of rotary-wing drones comprising a foldable drone structure.
    A rotary-wing drone comprises a drone structure and at least one rotor for ensuring the vertical lift of the drone structure, each rotor being carried by the drone structure.
    In order to facilitate the transport of a rotary-wing drone, it is possible to provide a foldable drone structure, which can pass from an unfolded configuration intended for the flight of the drone, to a folded configuration intended for transport and in which the drone structure is more compact.
    Such a drone structure comprises for example a drone body and several arms articulated on the drone structure. Each arm can for example carry a respective rotor of the rotary wing.
    However, a foldable drone structure can be heavier than a non-foldable drone structure, for example due to the presence of the joints of the foldable structure. The increased weight of the drone structure can affect the flight dynamics of the drone and / or its autonomy in flight.
    One of the aims of the invention is to provide a rotary wing drone having a foldable drone structure which can have a contained weight.
    To this end, the invention provides a rotary wing drone comprising at least one rotor carried by a drone structure, the drone structure comprising a drone body and at least one group of arms comprising several arms mounted to rotate in rotation on the drone body around the same axis of rotation, between an unfolded position for flight and a folded position for transport.
    The provision of a group of arms comprising several arms mounted mobile in rotation on the body of the drone around the same axis of rotation can allow the arms to share a common articulation system, which makes it possible to reduce the number of systems of articulation and the weight of the drone structure. In addition, the drone body can be configured with a limited number of locations for the reception of articulation systems, which limits the weight of the drone body itself.
    According to particular embodiments, the drone may include one or more of the following optional characteristics, taken in isolation or in any technically possible combination:
    - each arm supports a rotor and / or is provided with a support leg to place the drone on a surface;
    - each arm is mounted mobile in rotation on the drone body by means of an articulation system comprising an articulation assembly configured to lock the arm selectively in the unfolded position or in the folded position.
    each articulation assembly includes a first locking member and a second locking member configured to engage with each other to prevent rotation of the arm relative to the drone body and to disengage one of the other to allow rotation of the arm relative to the drone, and an elastic return member configured to return the first locking member and the second locking member engaged with each other;
    - The first locking member and the second locking member engage and disengage from each other by axial translation along the axis of rotation;
    - one of the first locking member and the second locking member comprises at least one tooth, the other comprising at least two notches, the tooth passing from one notch to the other notch during the rotation of the arm between the position unfolded and folded position;
    each articulation assembly comprises a tubular bushing extending along the axis of rotation, the first locking member being slidably mounted axially inside the bushing and integral in rotation with the bushing, the return member being housed inside the sleeve and pushing the first locking member towards the second locking member;
    - the drone includes a respective articulation set for each arm of the group of arms;
    the arms of the group of arms are mounted so as to be able to rotate on the drone body by means of the same common articulation shaft extending along the axis of rotation;
    - at least one or each group of arms comprises exactly two arms;
    the drone comprises at least two groups of arms, each group of arms having a respective axis of rotation distinct from that of each other group of arms;
    - at least one or each arm of at least one or each group of arms is separated from the drone body in the unfolded position and folded against the drone body in the folded position;
    - at least one group of arms comprises an arm extending longitudinally along the drone body and towards the front of the drone body when this arm is in the folded position, and one arm extends longitudinally along the drone body and towards the rear of the drone body when this arm is in the folded position;
    - the drone has a reception space for receiving a payload, two arms being configured to extend longitudinally by framing the reception space laterally when these arms are in the folded position.
    The invention and its advantages will be better understood on reading the description which follows, given solely by way of nonlimiting example, and made with reference to the appended drawings, in which:
    - Figures 1 and 2 are perspective views of a drone having a foldable drone structure, the drone structure being respectively in the unfolded configuration and in the folded configuration;
    - Figures 3 and 4 are perspective views, respectively assembled and exploded, of an articulation system common to the arms of a group of arms.
    In the following description, the terms "longitudinal", "transverse", "horizontal", "vertical", "top", "bottom", "front", "rear", "right" and "left" are extend by reference to the usual aircraft reference shown in Figures and 2, and comprising a longitudinal axis X (or roll axis), horizontal and directed from rear to front, a transverse axis Y (or pitch axis) , horizontal and directed from right to left, and a vertical axis Z (or yaw axis), vertical and directed from bottom to top.
    The drone 2 illustrated in Figures 1 and 2 is a rotary wing drone. The drone comprises at least one rotor (or propeller) 4 configured to ensure the vertical lift of the drone 2.
    The drone 2 comprises for example several rotors 4. Such a drone is called “multirotor”. Drone 2 here comprises exactly four rotors 4. Such a drone is called a “quadrotor”. The drone 2 could alternatively include a different number of rotors.
    The drone 2 comprises at least one motor 6 for driving in rotation of each rotor. The drone 2 here comprises a respective motor associated with each rotor. Each rotor 4 and the associated motor 6 form a motorized rotor assembly 8.
    The drone 2 comprises a drone structure 10. Each rotor 4 is carried by the drone structure 10. More specifically here, each motorized rotor assembly 8 is carried by the drone structure 10.
    The drone 2 also includes on-board electronic equipment which is also carried by the drone structure 10, and which is not visible in the figures. The on-board electronic equipment includes for example a radiocommunication device, a satellite geolocation receiver and / or an inertial unit, which allow manual, assisted and / or automatic piloting of the drone.
    The drone structure 10 is foldable. It can adopt an unfolded configuration (Figure 1), which is a flight configuration of the drone, and a folded configuration (Figure 2), which is a transport configuration of the drone.
    The drone structure 10 includes a drone body 12 and foldable arms 14. Each arm 14 is mounted mobile in rotation on the drone body 12 between an unfolded position (Figure 1) and a folded position (Figure 2).
    Each arm 14 passes from one position among the unfolded position and from the folded position to the other by rotation of the arm 14 relative to the drone body 12 about an axis of rotation A.
    The unfolded position of each arm 14 corresponds to the unfolded configuration of the drone structure 10, and the folded position of each arm 14 corresponds to the folded configuration of the drone structure 10.
    Each arm 14 is here spaced from the drone body 12 in the unfolded position of the arm 14, and folded against the drone body 12 in the folded position.
    Each arm 14 has a proximal end articulated on the drone body 12 and a free distal end. Each arm 14 is mounted cantilevered on the drone body 12 from its proximal end articulated on the drone body 12.
    The distal end of each arm 14 carries for example a respective rotor 4. The distal end of each arm 14 here carries a respective motorized rotor assembly 8.
    As a variant or as an option, the distal ends of the arms 14 define support feet making it possible to place the drone 2 on a horizontal surface, in support by means of these feet.
    As an option, as illustrated in Figure 2, the blades 16 of each rotor 4 are foldable to facilitate the transport of the drone 2 in the folded configuration.
    The arms 14 are grouped into at least one group of arms 18, here two groups of arms 18, each group of arms 18 including several of the arms 14 of the drone structure 10, the arms 14 of each group of arms 18 being mounted movable rotating on the drone body 12 around the same single axis of rotation A. All of the arms 14 of the same group of arms 18 share the same single axis of rotation A for their rotation relative to the drone body 12.
    When the drone structure 10 comprises several groups of arms 18 distinct, each group of arms 18 has a respective axis of rotation A, distinct from that of the other groups of arms 18.
    The axis of rotation A of the arms 14 of each group of arms 18 is here substantially vertical.
    Each group of arms 18 comprises for example exactly two arms 14. Thus, each group of arms 18 is a pair of arms 14 mounted so as to be able to rotate on the drone body 12 around the same single axis of rotation A.
    The drone structure 10 comprises for example two groups of arms 18 arranged symmetrically with respect to a median longitudinal plane P of the drone structure 10. The median longitudinal plane P is the plane containing the longitudinal axis X and the axis vertical Y of the drone. The two groups of arms 18 are arranged laterally on one side of the drone 4.
    The drone structure 10 here comprises four arms 14 grouped into two groups of arms 18 (or pairs of arms 18), each group of arms 18 having a common axis of rotation A for the two arms 14 of this group of arms 18, distinct of the axis of rotation A of the arms 14 of the other group of arms 18, the two groups of arms 18 being arranged symmetrically with respect to the median longitudinal plane.
    The arms 14 of each group of arms 18 are mounted mobile in rotation on the drone body 12 by means of an articulation system 20 of the group of arms 18, common to all the arms 14 of this group of arms 18 .
    The proximal end of each arm 14 is articulated on the drone body 12 by means of the articulation system 20 of the group of arms 18 to which this arm 14 belongs.
    Each group of arms 18 has its own respective articulation system 20 for the rotational mounting of the arms 14 of this group of arms 18 on the drone body 12. The articulation systems 20 of the different groups of arms 18 are similar.
    FIGS. 3 and 4 illustrate an articulation system 20 of a group of arms 18, by means of which the arms 14 of this group of arms 18 are mounted so as to be able to rotate on the drone body 12.
    The articulation system 20 comprises an articulation shaft 22 extending along the axis of rotation of the arms 14 of the group of arms 18, each arm 14 of the group of arms 18 being rotatably mounted on the shaft. The articulation shaft 22 is common to the arms 14 of the group of arms 18.
    The articulation system 20 comprises an articulation assembly 24 associated with each arm 14, the articulation assembly 24 being configured to guide the arm 14 in rotation about the axis of rotation, and to lock the arm 14 selectively in the unfolded position or in the folded position.
    Each articulation assembly 24 is configured to allow manual movement of the arm 14 associated between the unfolded position and the folded position of this arm 14, with a hard point between the unfolded position and the folded position.
    Each articulation assembly 24 comprises a first locking member 26 and a second locking member 28 configured to be engaged with each other to lock the arm 14 selectively in the unfolded position or in the folded position of the arm. 14, and to disengage from one another to allow rotation of the arm 14 between the folded position and the unfolded position.
    When the first locking member 26 and the second locking member 28 are engaged with each other, they oppose the rotation of the arm 14 between the unfolded position and the folded position of the arm 14.
    When the first locking member 26 and the second locking member 28 are released from one another, they allow the arm 14 to rotate between the unfolded position and the folded position.
    The first locking member 26 and the second locking member 28 are mounted axially movable relative to each other along the axis of rotation A of the arm 14, so as to selectively engage while approaching axially, or disengage from each other by deviating axially.
    In the example illustrated, the first locking member 26 is axially movable along the axis of rotation A, and the second locking member 28 is axially fixed along the axis of rotation A.
    The first locking member 26 and the second locking member 28 are mounted to rotate relative to each other about the axis of rotation A of the arm 14 to allow rotation of the arm 14 about the axis of rotation when the first locking member 26 and the second locking member 28 are released from each other.
    In the example illustrated, the first locking member 26 is movable in rotation about the axis of rotation A, and the second locking member 28 is fixed in rotation around the axis of rotation A. The first locking member 26 is integral in rotation with the arm 14 associated with the articulation assembly 24.
    The articulation assembly 24 includes a return member 30 configured to urge the first locking member 26 and the second locking member 28 in engagement with each other.
    The return member 30 is configured to oppose the disengagement of the first locking member 26 and the second locking member 28 from one another. The first locking member 26 and the second locking member 28 disengage from each other against the action of the return member 30.
    The return member 30 is an elastic return member. It is arranged to permanently urge the first locking member 26 and the second locking member 28 in engagement with each other.
    The return member 30 is here a helical spring arranged to push the first locking member 26 axially towards the second locking member 28, along the axis of rotation A.
    The articulation assembly 24 is configured so that the forced rotation of the arm 14 between the unfolded position and the folded position causes the first locking member 26 and the second locking member 28 to be released against the member reminder 30.
    The return member 30 therefore generates a resistant torque opposing the rotation of the arm 14 and having to be overcome to move the arm 14 between the folded position and the unfolded position.
    In the example illustrated, the first locking member 26 and the second locking member 28 are provided with respective contact surfaces which are oblique to a plane perpendicular to the axis of rotation A.
    The oblique contact surfaces include first contact surfaces coming into contact when the arm 14 rotates to the unfolded position, and second contact surfaces coming into contact when the arm 14 rotates to the folded position.
    The oblique contact surfaces are inclined so that, during the forced rotation of the arm 14 towards the unfolded position or towards the folded position, the oblique contact surfaces coming into contact cause the axial locking of the first locking member 26 and the second locking member 28 against the return member 30 until disengagement.
    This makes it possible to move the arm 14 between the folded position and the unfolded position, with a hard point between the two positions.
    In an exemplary embodiment, at least one of the first locking member 26 and the second locking member 28 is provided with at least one tooth 32, the other comprising at least two notches 34, each tooth 32 passing through a notch 34 to another notch 34 during the rotation of the arm 14 between the unfolded position and the folded position of the arm 14.
    Each oblique contact surface is a lateral face of a tooth 32 or a notch 34.
    Optionally, each articulation assembly 24 is configured so that, in the unfolded position and / or in the folded position, each arm 14 is preloaded in rotation against a rotation stop formed on the drone body, due to the action of the return member 30. This limits the vibrations of the arm 14 in the unfolded position or in the folded position.
    In the present case, when the arm 14 is in the unfolded position, the first locking member 26 and the second locking member 28 are in contact by inclined oblique contact surfaces so that the arm 14 is biased in abutment against a stop. corresponding rotation under the action of the return member 30.
    As a variant or as an option, when the arm 14 is in the unfolded position, the first locking member 26 and the second locking member 28 are in contact by inclined oblique contact surfaces so that the arm 14 is pressed against a corresponding rotation stop under the action of the return member 30.
    Each rotation stop is for example formed on the drone body 12. In FIG. 1, a rotation stop 35 for blocking in the unfolded position of an arm 14 is visible. In Figure 2, this rotation stop 35 and the rotation stop 35 for blocking in the unfolded position of the other arm 14 of the same group of arms 18 are visible.
    In the example illustrated, the first locking member 26 and the second locking member 28 are each provided with several teeth 32 delimiting between them notches 34, each notch 34 of one being adapted to receive a tooth 32 of the other.
    The teeth 32 and the notches 34 of each of the first locking member 26 and the second locking member 28 are distributed circumferentially around the axis of rotation A.
    The teeth 32 of each of the first locking member 26 and the second locking member 28 are offset by an angle greater than the angle of rotation of the arm 14 between the unfolded position and the folded position.
    This ensures that in the unfolded position and / or in the folded position, each tooth 32 and the notch 34 receiving the tooth 32 are supported via their oblique lateral faces to ensure the preload of the arm 14 against an associated rotation locking stop.
    The first locking member 26 and the second locking member 28 here each include four teeth 32 distributed at 90 ° and delimiting between them four notches 34 distributed at 90 °. The angle of rotation of each arm 14 between the folded position and the unfolded position is for example between 45 ° and 80 °.
    During the rotation of the arm 14 between the unfolded position and the folded position, each tooth 32 of the first locking member 26 passes from a notch 34 of the second locking member 28 to the adjacent notch 34 by passing over the tooth 32 of the second locking member 28 located between these two notches 34.
    In the example illustrated, the second locking member 28 is fixedly mounted on the drone body 12, and the first locking member 26 is mounted integral with the arm 14 in rotation about the axis of rotation A.
    The return member 30 is arranged to push the first locking member 26 axially along the axis of rotation A to keep it engaged with the first locking member 26.
    Each articulation assembly 24 here comprises a tubular bush 36 rotatably mounted on the drone body 12 around the axis of rotation, the first locking member 26 being slidably mounted inside the bush 36 while being integral in rotation of the bush 36, the return member 30 being housed inside the bush 36 axially between an internal shoulder of the bush 36 and the first locking member 26, so as to push the first locking member 26 toward the second locking member 28.
    In the example illustrated, the bush 36 and the first locking member 26 respectively have an internal surface and an external surface cooperating so as to rotate the bush 36 and the first locking member 26 around the axis of rotation A .
    The internal surface and the external surface each have, for example, at least one planar facet for ensuring the connection in rotation. The internal surface and the external surface are here square (with rounded corners) and complementary.
    In the example illustrated, the bush 36 is separate from the arm 14, the arm 14 being mounted on the bush 36, the arm 14 and the bush 36 being integral in rotation about the axis of rotation.
    To do this, the arm 14 has for example a housing for receiving the bush 36, the housing and the bush 36 having respectively an internal surface and an external surface cooperating to link in rotation the arm 14 and the bush 36.
    The internal surface and the external surface each have, for example, at least one planar facet for ensuring the connection in rotation. The external surface of the sleeve 36 is here square (with rounded corners). The housing of the arm 14 may have a complementary internal square surface (with rounded corners).
    In a variant, the sleeve 36 and the arm 14 are made integrally in a single piece of material. The socket 36 constitutes a proximal end of the arm 14 articulated on the drone body 12 by the articulation system 20.
    The second locking member 28 of each articulation assembly 24 is fixedly mounted on the drone body 12.
    In the example illustrated, in FIGS. 3 and 4, the second locking member 28 of one of the two articulation assemblies 24 comprises a fixing base 38 having holes 40 for its screwing on the drone body 12.
    The second locking member 28 of the other articulation assembly 24 is designed to be housed in a cavity 42 of a fixing part 43 fixed to the drone body 12, while being locked in rotation in this cavity 42.
    The fixing part 43 is provided so that the second locking member 28 is in radial abutment against one side of the cavity 42, in order to preload the return member 30.
    This second locking member 28 and the cavity 42 respectively have an external surface and an internal surface cooperating to keep the second locking member 28 fixed in rotation relative to the drone body 12. This second locking member 28 here has an external surface square (with rounded corners).
    Each articulation assembly 24 is threaded on the articulation shaft 22 of the articulation system 20. The articulation shaft 22 is engaged through each articulation assembly 24. The articulation shaft extends through the first locking member 26, the second locking member 28 and the sleeve 36 of each articulation assembly 24. In the present case, it also extends inside the return member 30 of each articulation assembly 24, provided in the form of a helical spring.
    In the example illustrated in FIGS. 3 and 4, the bush 36 and the first locking member 26 ensure the rotational guidance of the arm 14 on the articulation shaft 22 around the axis of rotation A, the first member locking 26 further cooperating with the second locking member 28 under the effect of the return member 30 for locking in rotation of the arm 14 selectively in the unfolded position or the folded position.
    Each articulation assembly 24 is received on a respective section of the articulation shaft 22.
    In the example illustrated, the articulation shaft 22 is provided with axial stops 44, 46, each articulation assembly 24 being disposed axially on a section delimited between two axial stops 44, 46.
    Each articulation assembly 24 has its bush 36 abutting against an axial stop 46 and its second locking member 28 abutting against another axial stop 44, the first locking member 26 sliding axially along the shaft and in the socket 36 for engaging with or disengaging from the second locking member 28.
    The articulation shaft 22 is provided with three axial stops comprising two axial end stops 44 and an intermediate axial stop 46, each articulation assembly 24 being disposed between the axial stop 46 intermediate and one of the two axial stops 44 d 'end.
    An axial stop, here the end axial stop 44 located on the side of the first locking member 28 provided with the base 38, is formed by a flange of the articulation shaft 22 formed integrally from a single piece of material with the articulation shaft 22, and the two other axial stops 44, 46 are attached and mounted on the articulation shaft 22, here each in a groove formed on the articulation shaft 22.
    In operation, to move each arm 14 from the unfolded position to the folded position, the user manually forces the arm 14 to rotate it. In doing so the arm 14 forces the first locking member 26 to rotate about the axis of rotation. The first locking member tends to disengage from the first member away from it axially so as to allow each tooth 32 to come out of a notch 34 in which it was engaged. The first locking member 26 moves axially against the elastic return member 30. When each tooth 32 e finds opposite the next notch 34, the first locking member 26 engages with the second locking member 28, and the arm 14 is again locked, in the folded position this time.
    To move from the folded position to the unfolded position, the user acts in the same way by manually forcing the arm 14 to pivot relative to the drone body 12, but in the opposite direction.
    Returning to Figures 1 and 2, the drone body 12 is configured for mounting a payload on the drone body 12.
    The payload is for example permanently mounted on the drone body 12. As a variant, the drone body 12 is provided with a mounting device (not visible) allowing rapid mounting and dismounting of the payload. The mounting device is for example of the type by screwing a mounting ring or bayonet.
    As illustrated in FIGS. 1 and 2, the payload is for example an image capture system 50 comprising an image capture device 52, in particular a camera.
    The image capture system 50 here comprises an orientation device 54 making it possible to control the orientation of the image capture device 52 relative to the drone body 12.
    The orientation device 54 here allows the orientation by rotation around two axes of orientation perpendicular to each other, namely the longitudinal axis X and the transverse axis Y. As a variant, it allows orientation around three axes of perpendicular orientation between them, which are for example the longitudinal axis X, the transverse axis Y and the vertical axis Z.
    The drone body 12 has a reception space 56 for the reception of the payload. The reception space 56 is located at one end of the drone body 12 along the longitudinal axis X, here the front end of the drone body 12.
    As an option, and as illustrated in FIGS. 1 and 2, the drone body 12 has two longitudinal extensions 58 extending projecting laterally on either side of the reception space 56. The longitudinal extensions 58 s' here protrude forward.
    Such longitudinal extensions 58 make it possible to protect and / or maintain the payload laterally, without hampering the field of vision of the image capture device 52 when the payload is an image capture system 50.
    In the folded position, two arms 14, each belonging to a respective group of arms 18, extend longitudinally by being placed laterally on either side of the reception space 56. The two arms 14 in the folded position extend on either side of the drone body 12 symmetrically with respect to the median longitudinal plane P.
    Thus, in the folded position, these two arms 14 of the drone protect the payload received in the reception space 56, by being placed laterally on either side of the reception space 56 and therefore of the payload.
    These two arms 14 in the folded position extend substantially parallel with each other, along the longitudinal axis X.
    In addition, as an option, the distal ends of these two arms 14 partially close the receiving space 56 longitudinally. The reception space 56 is thus located longitudinally between the drone body 12 and the distal end of each of the two arms 14 framing the reception space 56.
    Optionally, at least one of the two arms 14 framing the reception space 56 has a wedging member configured to wedge the payload in a transport position when the arm 14 is in the folded position.
    In particular, when the payload includes an orientation device 54, the setting of the payload makes it possible to avoid uncontrolled movements of the payload which could damage it.
    Thus, in the folded position of the arms 14, the payload is surrounded by the drone body 12 and by the arms 14, and protected by them. As a result, it is possible to limit the risk of damage to the payload during the transport of the drone 2 in the folded configuration.
    In the example illustrated, each group of arms 18 comprises a front arm 14 and a rear arm 14.
    The reception space 56 is here located at the front longitudinal end of the drone body 12 and the front arms 14 in the folded position frame the reception space 56.
    In the folded position, the free ends of the rear arms 14, in particular the motorized rotor assemblies 8 carried by these free ends, are placed behind the drone body 12. This allows compact storage.
    In the example illustrated, the front arm 14 of each group of arms 18 extends longitudinally towards the front of the drone body 12 from its proximal end when it is in the folded position, and the rear arm 14 of each arm group 18 extends longitudinally towards the rear of the drone body 12 from its proximal end when it is in the folded position.
    From the unfolded position of the arms 14, each front arm 14 folds by folding back towards the front of the drone body 12, while each rear arm 14 folds while folding back towards the rear of the drone body 12.
    This arrangement makes it possible to obtain a drone which is particularly compact in the folded transport configuration, as illustrated in FIG. 2.
    The drone 2 comprising a folding drone structure 10 having groups of arms 18 whose arms 14 are rotatably mounted on the drone body 12 about the same axis of rotation, allows the arms 14 of each group of arms 18 to share a common articulation system 20, and in particular a common articulation shaft 22. This makes it possible to limit the weight of the drone 2, which is favorable to the flight performance of the drone, to its autonomy in flight and / or to its ease of transport.
    Each articulation system 20 ensures simple and reliable locking of each arm 14 rotatably mounted on the drone body 12 by means of this articulation system 20, in an unfolded position for flight and a folded position for transport. .
    Arms 14 of the folding drone structure 10 are advantageously used to protect and / or block a payload carried by the drone 2, in particular an image capture system 50 comprising an image capture device 52 which can be oriented relative to to the drone body 12, when these arms 14 are in the folded position.
    The use of foldable arms 14 for the protection of a space 56 for receiving a payload mounted on the drone 2, such as image capture system 50, is advantageous independently of the mounting of arms 14 of the same group of arms 18 rotating around the same single axis of rotation A.
    Thus, in general, the invention also relates to a rotary-wing drone comprising at least one rotor 4 and a drone structure 10, each rotor being carried by the drone structure 10, the drone structure 10 comprising a drone body 12 and a plurality of arms 14, each arm 14 being mounted mobile on the drone body 12 between an unfolded flight position and a folded transport position, the drone body 12 having a space 56 for receiving a payload, two arms 14 being configured to extend on either side of the reception space 56 in the folded position of these two arms 14, so as to laterally frame the reception space between them.
    Optionally, the distal ends of these two arms 14 are configured to longitudinally close the reception space 56 in the folded position of these two arms 14, so that the reception space 56 is situated between the distal ends of the two arms longitudinally 14 and the drone body 12.
    Likewise, the configuration of folding forwards and backwards of the arms 14 of each group of arms 18 is advantageous independently of the articulation of the arms 14 on the drone body 12 around a same axis of rotation.
    Thus, in general, the invention also relates to a rotary-wing drone comprising at least one rotor 4 and a drone structure 10 carrying each rotor, the drone structure 10 comprising a drone body 12 and two groups of arms 18 arranged laterally on either side of the drone, each arm 14 being movably mounted on the drone body 12 between an unfolded position in which the arm 14 is separated from the drone body 12 and a folded position in which the arm 14 is folded against the drone body 12, each group of arms 18 comprising an arm 14 folding by folding backwards, and an arm 14 folding by folding backwards.
    权利要求:
    Claims (14)
    [1" id="c-fr-0001]
    1, rotary wing drone comprising at least one rotor carried by a drone structure (10), the drone structure (10) comprising a drone body (12) and at least one group of arms (18) comprising several arms (14) mounted mobile in rotation on the drone body (12) around a same axis of rotation (A), between an unfolded position for the flight and a folded position for the transport.
    [2" id="c-fr-0002]
    2, - Drone according to claim 1, wherein each arm (14) supports a rotor (4) and / or is provided with a support leg for placing the drone on a surface.
    [3" id="c-fr-0003]
    3. - Drone according to claim 1 or 2, wherein each arm (14) is mounted so as to be able to rotate on the drone body (12) by means of an articulation system (20) comprising a set of articulation (24) configured to lock the arm (14) selectively in the unfolded position or in the folded position.
    [4" id="c-fr-0004]
    4, - Drone according to claim 3, wherein each articulation assembly (24) comprises a first locking member (26) and a second locking member (28) configured to engage with each other for prevent rotation of the arm (14) relative to the drone body (12) and to disengage from each other to allow rotation of the arm (14) relative to the drone, and a return member (30) elastic configured to recall the first locking member (26) and the second locking member (28) engaged with each other.
    [5" id="c-fr-0005]
    5. - Drone according to claim 4, wherein the first locking member (26) and the second locking member (28) engage and disengage from each other by axial translation along the axis of rotation .
    [6" id="c-fr-0006]
    6. - Drone according to claim 4 or 5, wherein one of the first locking member (26) and the second locking member (28) comprises at least one tooth (32), the other comprising at least two notches ( 34), the tooth (32) passing from one notch (34) to the other notch (34) during the rotation of the arm (14) between the unfolded position and the folded position.
    [7" id="c-fr-0007]
    7, - Drone according to any one of claims 4 to 6, in which each articulation assembly (24) comprises a tubular bush (36) extending along the axis of rotation, the first locking member (26) being slidably mounted axially inside the bush (36) and integral in rotation with the bush (36), the return member (30) being housed inside the bush (36) and pushing the first member locking (26) to the second locking member (28).
    [8" id="c-fr-0008]
    8. - Drone according to any one of claims 4 to 7, comprising a joint assembly (24) respective for each arm (14) of the group of arms (18).
    [9" id="c-fr-0009]
    9. - Drone according to any one of claims 4 to 8, in which the arms (14) of the group of arms (18) are mounted so as to be able to rotate on the drone body (12) by means of the same common articulation shaft (22) extending along the axis of rotation.
    [10" id="c-fr-0010]
    10. - Drone according to any one of the preceding claims, in which at least one or each group of arms (18) comprises exactly two arms (14).
    [11" id="c-fr-0011]
    11, - Drone according to any one of the preceding claims, comprising at least two groups of arms (18), each group of arms (18) having a respective axis of rotation distinct from that of each other group of arms (18).
    [12" id="c-fr-0012]
    12, - Drone according to any one of the preceding claims, in which at least one or each arm (14) of at least one or each group of arms (18) is separated from the drone body (12) in the unfolded position and folded back against the drone body (12) in the folded position.
    [13" id="c-fr-0013]
    13. - Drone according to any one of the preceding claims, in which at least one group of arms (18) comprises an arm (14) extending longitudinally along the drone body (12) and towards the front of the body. of a drone when this arm (14) is in the folded position, and an arm (14) extends longitudinally along the drone body (12) and towards the rear of the drone body when this arm (14) is in position folded.
    [14" id="c-fr-0014]
    14, - Drone according to any one of the preceding claims, in which the drone has a reception space for receiving a payload, two arms (14) being configured to extend longitudinally by framing the reception space laterally (56 ) when these arms (14) are in the folded position.
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    同族专利:
    公开号 | 公开日
    US11117661B2|2021-09-14|
    EP3453438A1|2019-03-13|
    CN109466741A|2019-03-15|
    US20190071178A1|2019-03-07|
    EP3453438B1|2020-03-18|
    FR3070607B1|2020-09-04|
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    法律状态:
    2019-03-08| PLSC| Publication of the preliminary search report|Effective date: 20190308 |
    2019-08-19| PLFP| Fee payment|Year of fee payment: 3 |
    2020-08-31| PLFP| Fee payment|Year of fee payment: 4 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1758270|2017-09-07|
    FR1758270A|FR3070607B1|2017-09-07|2017-09-07|ROTATING BLADE DRONE INCLUDING A FOLDABLE DRONE STRUCTURE|FR1758270A| FR3070607B1|2017-09-07|2017-09-07|ROTATING BLADE DRONE INCLUDING A FOLDABLE DRONE STRUCTURE|
    EP18191614.9A| EP3453438B1|2017-09-07|2018-08-30|Rotary-wing drone comprising a foldable drone structure|
    CN201811038806.4A| CN109466741A|2017-09-07|2018-09-06|Rotor wing unmanned aerial vehicle including shrinkable unmanned plane structure|
    US16/125,391| US11117661B2|2017-09-07|2018-09-07|Rotary wing drone comprising a collapsible drone structure|
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