CN206039120U - Camera subassembly and use shooting device and aircraft of this camera subassembly - Google Patents

Camera subassembly and use shooting device and aircraft of this camera subassembly Download PDF

Info

Publication number
CN206039120U
CN206039120U CN201620780189.5U CN201620780189U CN206039120U CN 206039120 U CN206039120 U CN 206039120U CN 201620780189 U CN201620780189 U CN 201620780189U CN 206039120 U CN206039120 U CN 206039120U
Authority
CN
China
Prior art keywords
lens
thermal expansion
camera
camera assembly
ring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201620780189.5U
Other languages
Chinese (zh)
Inventor
宾朋
刘浩
廖然
赵喜峰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Feilai Information Technology Co ltd
Original Assignee
Shenzhen Dajiang Innovations Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenzhen Dajiang Innovations Technology Co Ltd filed Critical Shenzhen Dajiang Innovations Technology Co Ltd
Priority to CN201620780189.5U priority Critical patent/CN206039120U/en
Application granted granted Critical
Publication of CN206039120U publication Critical patent/CN206039120U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Lens Barrels (AREA)

Abstract

The utility model provides a camera subassembly and use shooting device and aircraft of this camera subassembly, this aircraft include the fuselage and install in the shooting device of fuselage, it is in with the setting including the body of shooing the device to shoot the device camera subassembly on the body, the camera subassembly includes: the microscope base with install the camera lens subassembly on the microscope base, the camera lens subassembly include the lens cone with at least one encapsulate in lens in the lens cone, the microscope base includes the connecting piece, the connecting piece with the camera lens subassembly is connected, the connecting piece is used for the inside temperature of microscope base drives when rising the camera lens subassembly is followed the optical axis direction of lens removes predetermines the displacement, it is used for the compensation to predetermine the displacement the focus change volume that the lens inflation arouses.

Description

Camera assembly, shooting device using camera assembly and aircraft
Technical Field
The embodiment of the utility model provides a relate to optical imaging technology field, especially relate to a camera subassembly and use shooting device and aircraft of this camera subassembly.
Background
With the development of the camera technology, the fixed-focus camera assembly has the advantages of simple design, high focusing speed and stable imaging quality, and is widely applied to camera electronic equipment with various purposes.
The current commonly used fixed focus camera component generally comprises a lens, a lens base and an image sensor chip; the lens is arranged on the lens base, and the image sensor chip is arranged in an accommodating space formed by the lens and the lens base. Be equipped with the plastic lens in the camera lens, the plastic lens is sensitive to ambient temperature, and when the image sensor chip dispelled the heat, perhaps ambient temperature risees, the plastic lens is heated and takes place thermal expansion, and the shape of plastic lens changes, leads to the focus of camera lens to change for the out-of-focus phenomenon appears in the camera lens, and imaging quality is not good.
SUMMERY OF THE UTILITY MODEL
The utility model provides a camera subassembly and use shooting device and aircraft of this camera subassembly, this camera subassembly can compensate the focus variation volume that the lens inflation arouses.
In one aspect, the utility model provides a camera assembly, include: the lens assembly comprises a lens barrel and at least one lens packaged in the lens barrel; the microscope base includes the connecting piece, the connecting piece with the lens subassembly is connected, the connecting piece is used for driving when the inside temperature of microscope base risees the lens subassembly is followed the optical axis direction of lens removes and predetermines the displacement, predetermine the displacement and be used for compensating the focus variation volume that the lens inflation arouses.
In one possible implementation, the connecting member is a thermal expansion member, and the top end of the thermal expansion member is connected with the lens assembly.
In a possible implementation manner, when the interior of the lens holder is heated, the expansion displacement of the thermal expansion piece along the optical axis direction is equal to the displacement of the lens along the focal plane of the optical axis direction.
In one possible implementation, the thermal expansion member is a thermal expansion ring disposed around the lens assembly.
In one possible implementation, the top edge of the thermal expansion ring is concavely formed with a concave portion.
In one possible implementation, the thermal expansion ring top edge is recessed to form at least two recesses.
In one possible implementation, the recesses are equally spaced.
In a possible implementation manner, a convex portion is formed between the two adjacent concave portions, and the convex portion is used for driving the lens assembly to move for a preset displacement along the optical axis direction of the lens when the temperature inside the lens seat is increased.
In a possible implementation manner, the lens mount further includes a mounting seat, the lens assembly is disposed in the accommodating cavity of the mounting seat, and the thermal expansion ring is disposed on the mounting seat.
In a feasible implementation manner, the thermal expansion ring is in a ring shape and is arranged in a surrounding manner, the mounting seat is in a boss structure arranged in a surrounding manner, and each convex part of the thermal expansion ring is correspondingly sleeved at one corner of the boss.
In one possible implementation, the lens assembly further includes a rigid connection frame, the lens barrel is connected with the rigid connection frame, and the rigid connection frame is connected with the thermal expansion ring.
In a possible implementation, the rigid connection frame is disposed at the periphery of the lens barrel.
In one possible implementation, the top end of the thermal expansion loop is connected to the rigid link.
In a possible implementation manner, the mirror base further includes a base disposed at the bottom of the mounting base, and an end surface of the bottom end of the thermal expansion ring is connected to a top end of the base.
In a possible implementation, the thermal expansion ring has a length in the optical axis direction that is greater than a length of the mount.
In one possible implementation, the rigid connection frame includes a bearing part and a fixing part arranged at the edge of the bearing part;
the bearing part is connected with the lens cone, and the fixing part is connected with the top end of the thermal expansion ring.
In a feasible implementation manner, a through hole is formed in the bearing part, and a ring-shaped fixing member is connected to one side of the through hole, which faces the lens barrel, and is connected with the lens barrel.
In a possible implementation manner, the fixing portion includes a pillar and a protrusion, a first end of the pillar is connected to the bearing portion, the protrusion is disposed at a second end of the pillar, and the protrusion is connected to a top end of the thermal expansion ring.
In one possible implementation, the method further includes: the image sensor chip is arranged at the bottom of the microscope base and is arranged in the accommodating cavity of the microscope base.
In a possible implementation manner, the material of the thermal expansion member is plastic satisfying a preset thermal expansion coefficient.
In one possible implementation, at least one of the lenses is made of plastic.
In one possible implementation, an end face of the bottom end of the thermal expansion ring is bonded to the top end of the base.
In a possible implementation, the lens barrel is bonded to the annular fixture.
On the other hand, the utility model provides a shooting device, shooting device including shooting device's body with set up in camera subassembly on the body, camera subassembly includes: the lens assembly comprises a lens barrel and at least one lens packaged in the lens barrel; the microscope base includes the connecting piece, the connecting piece with the lens subassembly is connected, the connecting piece is used for driving when the inside temperature of microscope base risees the lens subassembly is followed the optical axis direction of lens removes and predetermines the displacement, predetermine the displacement and be used for compensating the focus variation volume that the lens inflation arouses.
In another aspect, the present invention provides an aircraft, the aircraft including a fuselage and an imaging device mounted on the fuselage, the imaging device including an imaging device body and a camera assembly mounted on the body, the camera assembly including: the lens assembly comprises a lens barrel and at least one lens packaged in the lens barrel; the microscope base includes the connecting piece, the connecting piece with the lens subassembly is connected, the connecting piece is used for driving when the inside temperature of microscope base risees the lens subassembly is followed the optical axis direction of lens removes and predetermines the displacement, predetermine the displacement and be used for compensating the focus variation volume that the lens inflation arouses.
In a feasible implementation, the aircraft further comprises a cradle head, the cradle head is arranged below the central part of the fuselage, an installation part is arranged on the cradle head, and a mirror base in a camera assembly of the shooting device is installed on the installation part.
In one possible implementation, the fuselage includes an upper shell and a lower shell; wherein,
the upper shell and the lower shell are arranged in a matching mode to form the central portion of the machine body and at least one machine arm extending along the central portion of the machine body.
In one possible implementation, the aircraft is an unmanned aircraft.
The utility model provides a camera component, a shooting device using the camera component and an aircraft, wherein the camera component comprises a lens base and a lens component arranged on the lens base, and the lens component comprises a lens cone and at least one lens encapsulated in the lens cone; the lens base comprises a connecting piece, the connecting piece is connected with the lens assembly, the connecting piece drives the lens assembly to move along the optical axis direction of the lens when the temperature in the lens base rises to preset displacement, and the preset displacement is used for compensating the focal length variation caused by the expansion of the lens, so that the position of a focal plane after the temperature change is coincident with the position of the focal plane before the temperature change, and clear images can be shot by the camera assembly.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive labor.
Fig. 1 is a schematic structural diagram of a camera assembly provided by the present invention;
fig. 2 is a schematic view of the working principle of the camera assembly provided by the present invention;
fig. 3 is an exploded schematic view of the camera module provided by the present invention;
fig. 4 is a schematic view of an angle of view of the camera assembly provided by the present invention;
fig. 5 is a schematic top view of a camera module provided by the present invention;
FIG. 6 is a schematic cross-sectional view taken along plane A-A of FIG. 5;
fig. 7 is a schematic structural diagram of the aircraft provided by the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
The camera assembly provided by the embodiment can be applied to various camera fields so as to overcome the problem of lens defocusing caused by thermal expansion of the lens. The camera assembly can be applied to various electronic devices, such as mobile phones, flat panels, video cameras, cameras and other electronic devices with camera functions, and can also be applied to aircrafts, unmanned vehicles, unmanned ships and the like. In this embodiment, the camera assembly is applied to an aircraft as an example, and a detailed description is given.
The structure and implementation principle of the camera assembly and the aircraft of the present embodiment are described in detail below with specific embodiments. The following specific embodiments may be combined with each other, and details of the same or similar concepts or processes may not be repeated in some embodiments.
Fig. 1 is the structural schematic diagram of the camera module provided by the utility model. As shown in fig. 1, the camera assembly comprises a lens mount 20 and a lens assembly 40 mounted on the lens mount 20, wherein the lens assembly 40 comprises a lens barrel 10 and at least one lens enclosed in the lens barrel 10;
the lens holder 20 includes a connection member connected to the lens assembly for driving the lens assembly 40 to move a preset displacement in the optical axis direction of the lens when the temperature inside the lens holder 20 rises, the preset displacement being used to compensate for the amount of change in the focal length caused by the expansion of the lens.
In this embodiment, the connecting member may specifically be a connecting structure having expansion with heat and contraction with cold functions. The lens assembly can be driven to move for a preset displacement. The connector may or may not be connected to the lens assembly. Taking the example that the connecting piece drives the lens assembly to move upwards, when in connection, the connecting piece can be connected with one end of the lens assembly far away from the lens base and drive the lens assembly to move upwards from one end of the lens assembly far away from the lens base, and the connecting piece can also be connected with one end of the lens assembly close to the lens base and push the lens assembly to move upwards from one end of the lens assembly close to the lens base. The above description only schematically illustrates the implementation of the connection, and the embodiment is not particularly limited herein with respect to other connection relationships between the connection member and the lens assembly.
One possible implementation is shown in fig. 1, and as shown in fig. 1, the connecting member may be specifically a thermal expansion member 30, and the top end of the thermal expansion member 30 is connected to a lens assembly 40. The lens assembly 40 includes a lens of at least one lens. Among the materials constituting the lenses, at least one of the lenses is made of plastic, and the other lenses may be made of glass or the like.
In the specific implementation process, when the temperature rises, the thermal expansion member 30 thermally expands, the lens thermally expands, and at this time, the thermal expansion member 30 drives the lens assembly 40 to move along the optical axis direction of the lens by a preset displacement, so as to compensate the focal length variation caused by the expansion of the lens.
The following describes in detail the implementation principle of the present camera module with reference to fig. 2. Fig. 2 is the working principle schematic diagram of the camera assembly provided by the utility model. As shown in fig. 2, (one) represents the position of the focal plane when the lens assembly 40 is unheated. Specifically, when the lens assembly 40 is not heated, the optical path is shown by a solid line, and at this time, the normal focal plane is located at a position a1, which is the plane L where the image sensor chip is located. And (ii) represents the position of the focal plane when the lens assembly 40 is heated in the prior art. Specifically, when the lens assembly 40 is heated, the lens in the lens assembly 40 is thermally expanded, and in the view shown in fig. 2, after the lens is thermally expanded, the specific optical path is shown by a dotted line, and the focal plane is located at a position a2, that is, the focal plane is moved downward by a distance Y, and the focal plane does not fall on the image sensor chip. And (iii) represents the position of the focal plane when the lens assembly 40 is heated when a thermal expansion member is provided in the camera head assembly. Specifically, in the view shown in fig. 2, when the lens assembly 40 is heated, the lens thermally expands, which will cause the focal plane to move downward, but at the same time, the thermal expansion member thermally expands, after being heated and expanded, the length of the thermal expansion piece along the optical axis direction of the lens is extended, so as to drive the lens component to move towards the direction far away from the image sensor chip, i.e., the lens assembly is driven to move upward, in the embodiment, the expansion displacement of the thermal expansion member 30 along the optical axis direction is equal to the displacement of the lens along the focal plane of the optical axis direction, i.e., the focal plane moves down by a distance Y equal to the distance X that the lens assembly moves up, the resulting focal plane a2 falls on the plane L where the image sensor chip is located, therefore, the focal plane after temperature change is coincident with the focal plane before temperature change, namely, the focal plane always falls on the image sensor chip, and the imaging definition is further ensured. This embodiment makes the distance that the connecting piece upwards drove the removal of lens subassembly equal with the distance that focal plane moves down to guaranteed that the focal plane is located the plane that image sensor chip located all the time, made the camera subassembly can shoot clear image.
As will be understood by those skilled in the art, an object expands thermally by an elongation, which is the temperature difference x the length of the object x the rate of thermal expansion. The movement amount of the focal plane of the lens along with the temperature rise can be obtained through limited experiments, and therefore the corresponding relation between the movement amount of the focal plane and the temperature rise is obtained. The final experimental data show that the relationship between the focal plane movement amount and the temperature rise presents a linear relationship. Since the temperature difference is given by the environment, a material having the highest possible thermal expansion coefficient can be selected and the length of the thermal expansion member can be determined by the above formula. Optionally, according to the overall size of the camera head assembly, the length of the thermal expansion member is determined, then the thermal expansion rate is determined, and finally the material corresponding to the thermal expansion rate is selected. That is, the material of the thermal expansion member in this embodiment is plastic satisfying the predetermined thermal expansion coefficient. In the present embodiment, the material of the thermal expansion member and the thermal expansion coefficient of the thermal expansion member are not particularly limited as long as the amount of focal length change caused by the expansion of the lens can be compensated.
The camera assembly provided by the embodiment comprises a lens base and a lens assembly arranged on the lens base, wherein the lens assembly comprises a lens formed by at least one lens; the lens base comprises a connecting piece, the connecting piece drives the lens assembly to move along the optical axis direction of the lens when the temperature in the lens base rises to preset displacement, and the preset displacement is used for compensating the focal length variation caused by the expansion of the lens, so that the position of a focal plane after the temperature change is coincident with the position of the focal plane before the temperature change, and clear images can be shot by the camera assembly.
The structure of the camera head assembly provided in this embodiment will be described in detail below with reference to fig. 3 to 5.
Fig. 3 is an explosion structure schematic diagram of the camera assembly provided by the present invention, fig. 5 is a schematic diagram of a top view of the camera assembly provided by the present invention, and fig. 6 is a schematic cross-sectional diagram of the a-a surface in fig. 5. As shown in fig. 3, 5 and 6, the thermal expansion member 30 is a thermal expansion ring disposed around the lens assembly.
The top end of the thermal expansion ring of this embodiment is connected with the lens component 40, and the thermal expansion ring is arranged around the thermal expansion piece, so that when the thermal expansion ring drives the lens component 40 to move upwards, the stress of the lens component 40 can be balanced, and the focal plane can not be inclined.
Optionally, the top edge of the thermal expansion ring is concavely formed with a recess 33. For example, in the embodiment shown in fig. 3, the edge of the top end of the thermal expansion ring is recessed to form at least two recesses 33, each of which is equally spaced. Correspondingly, a convex portion 34 is formed between two adjacent concave portions, and the convex portion 34 is used for driving the lens assembly 40 to move for a preset displacement along the optical axis direction of the lens when the temperature inside the lens holder is increased.
In a specific implementation, the lens in the camera assembly presents a field of view, as shown in particular in fig. 4. Fig. 4 is a schematic view of an angle of view of the camera assembly provided by the present invention. As shown in fig. 4, the angle of view of the lens is generally about 90 to 100 degrees, and is a conical surface. In the embodiment, in order to ensure that the camera assembly has a good angle of view, a concave part is concavely formed at the top end edge of the thermal expansion ring, and the concave part can avoid the angle of view of the lens, so that the angle of view of the lens is complete. Meanwhile, a convex portion 34 is formed between two adjacent concave portions, and the convex portion 34 may be connected to the lens assembly 40 to move the lens assembly 40 by a predetermined displacement in the optical axis direction of the lens.
The structure of the thermal expansion ring will be described in detail below using a specific example.
In one possible implementation, the lens holder 20 further includes a mounting seat 21, the lens assembly 40 is disposed in the accommodating cavity of the mounting seat 21, and the thermal expansion ring is disposed on the mounting seat 21. The thermal expansion ring in this embodiment is in a ring shape, correspondingly, the mounting base 21 is in a boss structure, and each protrusion 34 of the thermal expansion ring is correspondingly sleeved on one corner of the boss. It is understood that the thermal expansion ring may be a polygonal ring, a circular ring, an elliptical ring, an irregular circular arc spliced ring, or the like; the mounting base 21 can be a polygonal boss, an annular boss, an elliptical annular boss, and a boss of a multi-section circular arc splicing surrounding structure.
In this embodiment, the inner side of the protrusion 34 may be further provided with a groove for nesting the corner of the boss. Optionally, the corner of the boss may be further provided with a chamfer 211, and the convex portion 34 may be fitted over the chamfer 211 of the boss. The chamfer 211 provided at the corner of the boss of the present embodiment reduces wear on the thermal expansion ring when the thermal expansion ring extends upward.
Specifically, with continued reference to fig. 3, in the embodiment shown in fig. 3, the lens base 20 is a cube, and the corresponding thermal expansion ring is a quadrilateral thermal expansion ring, which includes four concave portions and four convex portions, and the concave portions and the convex portions are arranged at intervals. The concave part can avoid the visual angle of the lens, and the convex part can be connected with the lens assembly.
The following uses detailed embodiments to describe specific implementations of the connection of the thermal expansion ring and the lens assembly.
Please refer to fig. 3. The lens assembly 40 further includes a rigid connecting frame 400, the lens is mounted in the lens barrel 10, the lens barrel 10 is connected with the rigid connecting frame 400, and the rigid connecting frame 400 is further connected with the thermal expansion ring 30. Alternatively, the rigid link frame 400 is disposed at the periphery of the lens barrel 10. The lens barrel 10 and the rigid connection frame 400 may be connected by bonding, engaging, or fastening.
The rigid link 400 may be made of a rigid material that does not deform when heated. The top end of the thermal expansion loop is connected to a rigid connection frame 400.
Optionally, the mirror base further comprises a base 22 disposed at the bottom of the mounting base 21, and an end surface of the bottom end of the thermal expansion ring is connected to a top end of the base 22. For example, the end face of the bottom end of the thermal expansion ring is connected to the top end of the base 22 by bonding. It will be appreciated that the thermal expansion ring may also be connected to the base 22 by snap-fit, or the like.
In the present embodiment, by providing the rigid connection frame, when the length of the thermal expansion ring is greater than the length of the lens barrel, that is, the length of the thermal expansion ring in the optical axis direction is greater than the length of the mount 21, the connection between the thermal expansion ring and the lens barrel can be realized. Namely, the lens cone is reversely fixed through the rigid connecting frame, and then the rigid connecting frame is connected with the top end of the thermal expansion ring.
In the specific implementation process, when the lens base is heated, the lens is heated to generate thermal expansion, so that the focal plane moves downwards, and at the moment, the thermal expansion ring is heated to generate thermal expansion, because the end surface of the bottom end of the thermal expansion ring is connected with the top end of the base 22, after the thermal expansion ring is heated to generate thermal expansion, because of the limitation of the base 22, the thermal expansion ring can only extend towards the direction opposite to the base 22, namely the thermal expansion ring extends towards the direction far away from the base 22, in the process of extending the thermal expansion ring, the rigid connecting frame 400 is driven to move towards the direction far away from the base 22, the rigid connecting frame 400 drives the lens barrel to move, the distance that the lens barrel moves towards the direction far away from the base 22 is equal to the distance that the focal plane moves towards the base 22, so that the position of the focal plane after temperature change coincides with the position of the focal plane before temperature change is realized, and the focal plane always falls on the image, so that the camera assembly can take a sharp image.
The structure of the rigid link 400 will be described in detail below with reference to fig. 3 and 6. As shown in fig. 3 and 6, the rigid connection frame 400 includes a bearing portion 41 and a fixing portion 42 disposed at an edge of the bearing portion 41; the supporting portion 41 is connected to the lens barrel 10, and the fixing portion 42 is connected to the top end 32 of the thermal expansion ring.
In a specific implementation process, the bearing portion 41 may be connected to the lens barrel through bonding, fastening, overlapping, sleeving, or the like, that is, the lens barrel is disposed at the bottom of the bearing portion 41. Optionally, a through hole 411 is disposed on the bearing portion 41, a ring-shaped fixing member 412 is connected to one side of the through hole 411 facing the lens barrel 10, and the ring-shaped fixing member 412 is connected to the lens barrel 10. Alternatively, the lens barrel 10 may be connected to the ring fixture 412 by bonding.
As shown in fig. 3, the projection area of the bearing portion 41 toward the lens holder 20 is larger than the projection area of the lens barrel 10 toward the lens holder 20, the lens barrel 10 is disposed in the accommodating cavity formed by the lens holder 20, and the bearing portion 41 is disposed above the lens barrel 10 and is supported by the upper edge 23 of the accommodating cavity.
In the embodiment, the through hole and the annular fixing piece are arranged, so that the lens barrel can be fixedly arranged at the bottom of the bearing part on the one hand, and the through hole ensures the visual field of the lens on the other hand.
Further, as shown in fig. 3, the fixing portion 42 includes a pillar 421 and a protrusion 422, a first end of the pillar 421 is connected with the bearing portion 41, the protrusion 422 is disposed at a second end of the pillar 421, and the protrusion 422 is connected with the top end 31 of the thermal expansion ring.
In this embodiment, the protrusion 422 is coupled to the top end 31 of the thermal expansion ring. Taking fig. 3 as an example, the projection 422 is attached to the projection 31 of the thermal expansion ring and fixed by adhesion.
Further, on the basis of the above embodiment, the camera assembly provided by this embodiment further includes an image sensor chip, where the image sensor chip is disposed in the accommodating cavity of the lens holder and at the bottom of the lens holder. Therefore, when the thermal expansion ring moves the position of the lens to change, the focal plane of the lens is ensured to always fall on the image sensor chip.
Further, the camera assembly in this embodiment further includes a substrate disposed at the bottom of the lens holder, and the image sensor chip is disposed on the substrate.
The following describes a specific example of the application of the above-described camera assembly to an aircraft in a specific embodiment. When the camera assembly is applied to an aircraft, the aircraft can realize various aerial photographing functions.
Fig. 7 is a schematic structural diagram of the aircraft provided by the present invention. The aircraft may be, for example, an unmanned aircraft. As shown in fig. 7, the aircraft includes a body 100 and a camera assembly (not shown) mounted to the body 100. For a specific implementation manner of the camera assembly, reference may be made to the embodiments shown in fig. 1 to 6, and details of this embodiment are not described herein again.
In this embodiment, the aircraft further comprises a power assembly 110, and the power assembly 110 comprises a propeller 111 and a motor 112 for driving the propeller 111 to rotate so as to provide lift for the aircraft.
The fuselage 100 includes a fuselage center section 120 and at least one horn 130 extending along the fuselage center section 120. The power assembly 110 described above may be provided on the horn 130.
Optionally, the fuselage 100 comprises an upper shell 101 and a lower shell 102; wherein,
the upper housing 101 and the lower housing 102 are arranged in an apposition forming a fuselage center section 120 and at least one horn 130 extending along the fuselage center section 120.
Optionally, the drone further comprises: a metal cavity (not shown) and a foot rest 150;
the metal cavity is provided between the upper case 101 and the lower case 102, the metal cavity is used for placing a battery, and the foot stand 150 is provided below the lower case 102.
Optionally, the camera assembly may include a pan and tilt head 140 disposed on the body. Specifically, the pan/tilt head 140 is disposed below the body center portion 120, and the pan/tilt head 140 is provided with a mounting portion 141 on which the mirror base is mounted.
It should be noted that fig. 7 illustrates a physical structure diagram of an aircraft by way of example only, and is not a limitation on the structure of the aircraft, and the structure of the aircraft is not specifically limited by the present invention.
The aircraft that this embodiment provided, including the fuselage and install the camera subassembly in the fuselage, this camera subassembly includes: the lens assembly comprises a lens formed by at least one lens; the microscope base includes the connecting piece, and the connecting piece is used for driving the lens subassembly to remove along the optical axis direction of lens when the inside temperature of microscope base risees and predetermines the displacement, predetermines the displacement and is used for compensating the focus variation volume that the lens inflation arouses, and this embodiment makes the aircraft at the in-process of taking photo by plane, and when the temperature in the microscope base risees, focal plane's position coincidence before focal plane behind the temperature variation and the temperature variation makes the camera subassembly can shoot clear image.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention.

Claims (28)

1. A camera head assembly, comprising: the lens assembly comprises a lens barrel and at least one lens packaged in the lens barrel;
the microscope base includes the connecting piece, the connecting piece with the lens subassembly is connected, the connecting piece is used for driving when the inside temperature of microscope base risees the lens subassembly is followed the optical axis direction of lens removes and predetermines the displacement, predetermine the displacement and be used for compensating the focus variation volume that the lens inflation arouses.
2. A camera assembly according to claim 1, wherein the connecting member is a thermal expansion member, the top end of the thermal expansion member being connected to the lens assembly.
3. The camera head assembly of claim 2, wherein when heat is applied to the interior of the lens holder, the amount of expansion displacement of the thermal expansion member in the optical axis direction is equal to the amount of displacement of the lens in the focal plane in the optical axis direction.
4. A camera assembly according to claim 2, wherein the thermal expansion member is a thermal expansion ring disposed around the lens assembly.
5. A camera assembly according to claim 4, wherein the thermal expansion ring top edge is concavely formed with a recess.
6. A camera assembly according to claim 5, wherein the thermal expansion ring top edge is recessed to form at least two recesses.
7. A camera assembly according to claim 6, wherein the recesses are equally spaced.
8. The camera head assembly of claim 6, wherein a convex portion is formed between two adjacent concave portions, and the convex portion is used for driving the lens assembly to move along the optical axis direction of the lens by a preset displacement when the temperature inside the lens holder is increased.
9. The camera assembly of claim 8, wherein the lens mount further comprises a mount, the lens assembly being disposed in a receiving cavity of the mount, the thermal expansion ring being disposed on the mount.
10. The camera assembly of claim 9, wherein the thermal expansion ring is annular and the mounting base is a boss structure, and each of the protrusions of the thermal expansion ring is correspondingly fitted over a corner of the boss.
11. The camera assembly of claim 9, wherein the lens assembly further comprises a rigid connecting frame, the lens barrel being connected to the rigid connecting frame, the rigid connecting frame being connected to the thermal expansion ring.
12. The camera assembly of claim 11, wherein the rigid attachment frame is disposed at a periphery of the lens barrel.
13. A camera assembly according to claim 12, wherein the top end of the thermally expansive ring is connected to the rigid link.
14. The camera assembly of claim 13, wherein the lens mount further comprises a base disposed at a bottom of the mount, an end surface of a bottom end of the thermal expansion ring being connected to a top end of the base.
15. A camera assembly according to claim 14, wherein the thermal expansion ring has a length in the direction of the optical axis greater than the length of the mount.
16. A camera head assembly according to any of claims 12 to 15, wherein the rigid link includes a carrier portion and a securing portion provided at an edge of the carrier portion;
the bearing part is connected with the lens cone, and the fixing part is connected with the top end of the thermal expansion ring.
17. The camera head assembly according to claim 16, wherein the carrying portion is provided with a through hole, and a side of the through hole facing the lens barrel is connected with a ring-shaped fixing member, and the ring-shaped fixing member is connected with the lens barrel.
18. The camera assembly of claim 17, wherein the securing portion comprises a post and a protrusion, a first end of the post is coupled to the carrier portion, the protrusion is disposed at a second end of the post, and the protrusion is coupled to a top end of the thermal expansion ring.
19. A camera assembly according to any one of claims 1 to 15 and 17, 18, further comprising: the image sensor chip is arranged at the bottom of the microscope base and is arranged in the accommodating cavity of the microscope base.
20. A camera assembly according to any one of claims 2 to 15 and 17, wherein the thermal expansion member is of a plastics material which satisfies a predetermined coefficient of thermal expansion.
21. A camera assembly according to any one of claims 1 to 15 and 17, wherein at least one of the lenses is plastic.
22. A camera assembly according to claim 14, wherein the end face of the bottom end of the ring is bonded to the top end of the base.
23. A camera assembly according to claim 17, wherein said lens barrel is bonded to said ring mount.
24. A camera device, comprising a camera device body and the camera assembly of any one of claims 1-23 disposed on the body.
25. An aircraft, characterized in that it comprises: a body and the camera of claim 24 mounted to the body.
26. The aircraft of claim 25, further comprising a cradle head disposed below the central portion of the fuselage, the cradle head having a mounting portion disposed thereon, the mount in the camera assembly of the camera device being mounted on the mounting portion.
27. The aircraft of claim 25, wherein the fuselage comprises an upper shell and a lower shell; wherein,
the upper shell and the lower shell are arranged in a matching mode to form a central portion of the machine body and at least one machine arm extending along the central portion of the machine body.
28. The aircraft of claim 25, wherein the aircraft is an unmanned aircraft.
CN201620780189.5U 2016-07-22 2016-07-22 Camera subassembly and use shooting device and aircraft of this camera subassembly Expired - Fee Related CN206039120U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620780189.5U CN206039120U (en) 2016-07-22 2016-07-22 Camera subassembly and use shooting device and aircraft of this camera subassembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620780189.5U CN206039120U (en) 2016-07-22 2016-07-22 Camera subassembly and use shooting device and aircraft of this camera subassembly

Publications (1)

Publication Number Publication Date
CN206039120U true CN206039120U (en) 2017-03-22

Family

ID=58311503

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620780189.5U Expired - Fee Related CN206039120U (en) 2016-07-22 2016-07-22 Camera subassembly and use shooting device and aircraft of this camera subassembly

Country Status (1)

Country Link
CN (1) CN206039120U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107147904A (en) * 2017-06-08 2017-09-08 广东欧珀移动通信有限公司 Method of testing, device and and the computer-readable recording medium of camera module
CN107147905A (en) * 2017-06-08 2017-09-08 广东欧珀移动通信有限公司 Method of testing, device and and the computer-readable recording medium of camera module

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107147904A (en) * 2017-06-08 2017-09-08 广东欧珀移动通信有限公司 Method of testing, device and and the computer-readable recording medium of camera module
CN107147905A (en) * 2017-06-08 2017-09-08 广东欧珀移动通信有限公司 Method of testing, device and and the computer-readable recording medium of camera module
CN107147904B (en) * 2017-06-08 2019-05-24 Oppo广东移动通信有限公司 Test method, device and and the computer readable storage medium of camera module
CN107147905B (en) * 2017-06-08 2020-06-05 Oppo广东移动通信有限公司 Camera module testing method and device and computer readable storage medium

Similar Documents

Publication Publication Date Title
CN107278277B (en) Camera assembly, shooting device using camera assembly and aircraft
WO2021238776A1 (en) Photographing apparatus, electronic device, and control method
EP4120670B1 (en) Photographing module and assembling method therefor, and electronic device
US7491002B2 (en) Spherical enclosure for a camera
JP2019514038A (en) Optical device, in particular a camera including in particular automatic focusing, image stabilization and super-resolution
WO2021104017A1 (en) Camera module and electronic device
US20220026706A1 (en) Camera module and terminal
US20160255276A1 (en) Method for producing camera module
US9426340B2 (en) Vehicle CCTV camera apparatus
CN211206941U (en) Periscopic optical module and optical system
CN206039120U (en) Camera subassembly and use shooting device and aircraft of this camera subassembly
US20210080621A1 (en) Lens module and camera module including the same
WO2020029821A1 (en) Camera apparatus, sma driving device and manufacturing method, driving method and wiring method thereof
KR101634299B1 (en) Optical image stabilizer and method for manufacturing liquid bag for using in the same
KR102508493B1 (en) A camera module and optical instrument including the same
CN115918099B (en) Camera motor, camera module and electronic equipment
CN110365886A (en) Optical anti-shake camera module
JP2018059986A (en) Imaging device
CN210428039U (en) Focal length adjusting device and mobile terminal
US10827128B2 (en) Camera module and electronic device using same
KR102691319B1 (en) Lens Module
CN113905151B (en) Driving device, camera module and electronic equipment
CN110958365A (en) Multi-group lens, camera module, electronic equipment and assembling method
CN214544442U (en) Camera module and digital device
CN211627986U (en) Shooting device and holder assembly

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20170608

Address after: 201100 room 1032, building 555, Dongchuan Road, Minhang District, Shanghai, China

Patentee after: SHANGHAI FEILAI INFORMATION TECHNOLOGY Co.,Ltd.

Address before: 518057 Guangdong province Shenzhen city Nanshan District high tech Zone South Hing a No. 9 Hongkong, Shenzhen building 6 floor

Patentee before: SZ DJI TECHNOLOGY Co.,Ltd.

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170322