CN207832183U - A kind of aerial survey gondola - Google Patents

A kind of aerial survey gondola Download PDF

Info

Publication number
CN207832183U
CN207832183U CN201820082397.7U CN201820082397U CN207832183U CN 207832183 U CN207832183 U CN 207832183U CN 201820082397 U CN201820082397 U CN 201820082397U CN 207832183 U CN207832183 U CN 207832183U
Authority
CN
China
Prior art keywords
sensor
aerial survey
circumferential
fixed frame
frame
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
CN201820082397.7U
Other languages
Chinese (zh)
Inventor
许素棚
张毛雨
富雷
单辉
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.)
Beijing Xingguang Tongshi Technology Co ltd
Original Assignee
Beijing Quantum Starlight 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 Beijing Quantum Starlight Technology Co Ltd filed Critical Beijing Quantum Starlight Technology Co Ltd
Priority to CN201820082397.7U priority Critical patent/CN207832183U/en
Application granted granted Critical
Publication of CN207832183U publication Critical patent/CN207832183U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model provides a kind of aerial survey gondola comprising fixed frame;And a central sensor being arranged on the fixed frame and several circumferential sensors;The central sensor is vertically set on the fixed frame;Several described circumferential sensors are arranged on same circumference centered on by the central sensor;Helically type is obliquely installed several described circumferential sensors, and angle of inclination is identical.The specific laying form for several the circumferential sensors and centrally disposed central sensor that the utility model is laid by screw type, can make full use of space, effectively reduce the volume of entire structure for pod, structure is compacter;First, the gondola is small, light-weight.Simultaneously by way of this kind of laying, the information such as figure acquired in multiple sensor combinations are more accurate.

Description

A kind of aerial survey gondola
Technical field
The utility model is related to Aerial Surveying Technology fields, more particularly, to a kind of aerial survey gondola.
Background technology
In aerial survey, generally use aerial survey gondola hang sensor (usually for unmanned plane and other fixed wing aircrafts For camera), and current aerial survey gondola is unreasonable, occupied space is larger, while when the laying of multiple cameras, can not obtain preferable Shooting effect.
Utility model content
The purpose of this utility model is to provide a kind of aerial survey gondolas, are not conformed to solving structure existing in the prior art Reason, occupied space is larger, while when multiple cameras are laid, the technical issues of can not obtaining preferable shooting effect.
The structure for pod of the utility model have small, light weight, simple in structure, operating mode is various, can be used it is more Kind flight carrier more improves the quality of image and precision while improving operating efficiency.
In order to solve the above technical problems, a kind of aerial survey gondola provided by the utility model, including:Fixed frame;
And a central sensor being arranged on the fixed frame and several circumferential sensors;
The central sensor be vertically set on the fixed frame (fixed frame is horizontally set on uav bottom, then in Heart sensor is vertically arranged);
Several described circumferential sensors are arranged on same circumference centered on by the central sensor;
Helically type is obliquely installed several described circumferential sensors, and angle of inclination is identical.
Helically type is obliquely installed multiple circumferential sensors in the utility model and angle of inclination is identical, will be perpendicular to institute It states fixed frame and include the plane definition of circumference point tangent line is the section at the point, each circumferential sensor is in its section Projection tilt (or deflection) setting to same direction (clockwise or counter-clockwise), and angle of inclination is identical, wherein inclining Rake angle is the angle of two projection line of the central axis of circumferential sensor with the vertical line perpendicular to fixed frame on section.
Compared with the aerial survey gondola with configuration, several circumferential sensors that the utility model is laid by screw type and The specific laying form of centrally disposed central sensor, can make full use of space, effectively reduce entire structure for pod Volume, structure are compacter;The gondola is small, light-weight.Simultaneously by way of this kind of laying, multiple sensor combinations are obtained The information such as the figure taken are more accurate.
Further, the sensor is the camera of information used to capture images.
Further, the angle of inclination is 30 degree to 75 degree.
Wherein more preferably angle of inclination is 40-50 degree.
Further, the quantity of the circumferential sensor is 3-10.
The particular number of circumferential sensor can be arranged according to the actual application, it is therefore preferable to 3-6.
Further, further include centralized positioning frame;
The central sensor is removably relatively fixed by the centralized positioning frame and is connected on the fixed frame;
The location structure positioned for centralized positioning frame is provided between the centralized positioning frame and the fixed frame.
Further, further include circumferentially positioned frame;
The circumferential direction sensor is removably relatively fixed by the circumferentially positioned frame to be connected on the fixed frame;
The location structure positioned for circumferentially positioned frame is provided between the circumferentially positioned frame and the fixed frame.
Wherein, there are many location structure form, and the repetition for being mainly used for locating rack in locating rack disassembly process is accurately positioned, example Locating rack and the positioning pin and/or locating slot on the fixed frame is such as respectively set;
Alternatively, the positioning groove being arranged on fixed frame, bottom and the positioning groove of the locating rack match, locating rack Plug-in card is in positioning groove;
Alternatively, be provided with limiting stand on fixed frame, locating rack is provided with positioning end face, when installation, the positioning end of locating rack Face acts against on limiting stand.
Further, the aerial survey gondola further includes POS modules;The POS modules are exposed for recording in operation process The position of point and posture.
The position limiting structure for limiting the POS module positions is provided on the fixed frame.
Wherein position limiting structure can be the forms such as locating slot, positioning protrusion or positioning surface, be mainly used for realizing POS modules Positioning.
Location structure and position limiting structure can guarantee that in the gondola course of work, the relative position between sensor is kept not Become and the relative position between sensor and POS modules remains unchanged.
In the prior art, POS modules and sensor are fixed position when mounted, and in the gondola course of work, POS Relative position between module and sensor changes, in this way, subsequently in the location data based on POS modules, (data are The position data of each sensor determined relative to the relative position of POS modules according to each sensor) sensor is adopted When the data of collection are handled, since the relative position between POS modules and sensor can change, data processing precision meeting Generate deviation.And in the utility model, the relative position between POS modules and sensor is fixed, and therefore, data processing is smart Degree is high.
Further, the location structure for limiting center sensor location is provided on the centralized positioning frame;
And/or the location structure for limiting circumferential sensing station is provided on the circumferentially positioned frame.
Further, the fixed frame includes top plate and bottom plate and connecting pole, top plate and the setting of bottom plate interval, the two it Between be fixedly connected by several connecting poles;
The accommodation space for accommodating the central sensor and circumferential sensor is formed between top plate and the bottom plate;
It is enclosed with shell on the outside of the accommodation space;
The bottom plate center is provided with center mounting hole and location structure for installing the central sensor;
Several peripheries for installing the circumferential sensor are evenly arranged in the circumferential direction of the center mounting hole Mounting hole and location structure;
The central sensor and the circumferential sensor are arranged in the accommodation space, and the location structure is for protecting It demonstrate,proves central sensor and circumferential sensor and fixed frame bottom plate relative position is constant;The central sensor and the circumferential sensing The front end of device on the center mounting hole and periphery mounting hole respectively by extending downwardly the bottom plate.
Further, the aerial survey gondola further includes several hanging plates, and the hanging plate is fixed at the fixation On frame;The top plate is stretched out on the top of hanging plate upwards, for being connected with aircraft.
Hanging plate is generally arranged at the both sides of fixed frame, is provided with threaded hole above, the hanging plate being arranged in pairs by this, The aerial survey gondola and the lifting knot module for aiming at fixed wing aircraft design can be coordinated, be applied to large-scale fixed wing aircraft.
The lifting structure of fixed wing aircraft can have larger lifting space, coordinate with gondola, be fixed in aircraft cabin Bottom plate on, aerial survey gondola is hung on outside ventral by lifting structure, can avoid visual angle interference, improve reliability and peace Quan Xing.And POS modules (locating module) and constant also ensure of relative position of sensor coordinate lifting mould in the aerial survey gondola The block measurement accuracy of aerial survey gondola to image in large-scale fixed-wing.
The extension section plate of the aerial survey gondola both sides can also coordinate damped platform, be mounted below helicopter ventral.Or cooperation Passive energy dissipation structure is hung below the ventrals such as similar mountains and rivers fixed wing aircraft.
Further, the aerial survey gondola further includes for covering the circumferential sensor head (camera lens) and/or center The lens case of sensor head (camera lens), grease proofing windproof for protecting sensor lens, shading avoids veiling glare to being caused at figure It influences.
The lens case includes sequentially connected fixed part, protection department and light shielding part;
The fixed part with the bottom of the fixed frame for connecting;
The protection department is tubular, and is sleeved on the outside for leaning out part that the sensor front end stretches out the bottom plate, For protecting sensor front end to lean out part;
The light shielding part is in the axially projecting in the front end of sensor of the sensor.
The light shielding part prevents veiling glare from being had an impact to sensor shooting, such as prevent in image for blocking veiling glare Hickie is produced, to reduce the quality of image, and light shielding part can also play grease proofing dustproof effect.In flight operation, aircraft oil pipe The oil droplet of generation can drift with the wind, and light shielding part can effectively prevent oil droplet to be splashed on camera lens, avoid generating spot in image;It is anti- Shield portion can also obstruct oil droplet and be splashed on sensor fuselage, while can effectively prevent bulky grain dust contaminant sensor (camera).
Lens case is fixed by screw in use, fixed part is contacted with fixed frame bottom (bottom plate).Sensor passes through positioning Frame is fixed on fixed frame, and to which part camera body is placed in the gondola on fixed frame top, partial denudation is in fixed frame lower part Air in, add lens case at this time, then exposed aerial sensor can be protected.
Using above-mentioned technical proposal, the utility model has the advantages that:
Several circumferential sensors that the utility model is laid by screw type and centrally disposed central sensor It is specific to lay form, space can be made full use of, the volume of entire structure for pod is effectively reduced, structure is compacter;First, The gondola is small, light-weight.Simultaneously by way of this kind of laying, the information such as figure acquired in multiple sensor combinations are more Precisely.
Finally the inclination aerial survey gondola be equipped with general-purpose interface, operating mode is various, can be used for helicopter, small-sized fixed-wing, A variety of flight carriers such as large-scale fixed-wing.
Description of the drawings
It below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art Specific implementation mode or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art Under the premise of labour, other drawings may also be obtained based on these drawings.
Fig. 1 is the stereogram for the aerial survey gondola that the utility model embodiment provides;
Fig. 2 is the stereogram of aerial survey gondola after removing external shell in the utility model embodiment;
Fig. 3 is the structure chart of the laying of sensor in the utility model embodiment;
Fig. 4 is the laying lower section viewing angle constructions figure of sensor in the utility model embodiment;
Fig. 5 is the laying top viewing angle constructions figure of sensor in the utility model embodiment;
Fig. 6 is the structure chart of circumferential sensor in the utility model embodiment;
Fig. 7 is the structure chart of central sensor in the utility model embodiment;
Fig. 8 is the structure chart of circumferentially positioned frame in the utility model embodiment;
Fig. 9 is the exploded view for the aerial survey gondola that the utility model embodiment provides.
Reference numeral:
10- fixed frames;11- bottom plates;12- top plates;13- connecting poles;14- shells;15- hanging plates;21- central sensors; 22- centralized positioning framves;25- circumferential direction sensors;The circumferentially positioned framves of 26-;30-POS modules;40- lens cases;α-angle of inclination.
Specific implementation mode
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, originally The every other embodiment that field those of ordinary skill is obtained without making creative work, belongs to this practicality Novel protected range.
It is in the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", " perpendicular Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only The utility model and simplifying describes for ease of description, do not indicate or imply the indicated device or element must have it is specific Orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.In addition, term " the One ", " second ", " third " are used for description purposes only, and are not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally Connection;It can be mechanical connection, can also be electrical connection;Can be directly connected, can also indirectly connected through an intermediary, It can be the connection inside two elements.For the ordinary skill in the art, it can understand above-mentioned art with concrete condition The concrete meaning of language in the present invention.
Explanation is further explained to the utility model with reference to specific embodiment.
As shown in Figures 1 to 9, a kind of aerial survey gondola provided in this embodiment, including:Fixed frame 10;
And a central sensor 21 being arranged on fixed frame 10 and several circumferential sensors 25;
Emphatically with reference to as shown in Figures 3 to 5, central sensor 21 is vertically set on fixed frame 10 (10 level of fixed frame Setting is vertically arranged in uav bottom, then central sensor 21);Several circumferential sensors 25 are arranged with central sensor On same circumference centered on 21;Helically type is obliquely installed several circumferential sensors 25, and inclination angle alpha is identical.
Helically type is obliquely installed multiple circumferential sensors 25 in the utility model and angle of inclination is identical, will be perpendicular to Fixed frame 10 and include the plane definition of circumference point tangent line be the section at the point, each circumferential direction sensor 25 is in its section Projection tilts (or deflection) setting to same direction (clockwise or counter-clockwise), and angle of inclination is identical, wherein tilting Angle is the folder of two projection line of the central axis of circumferential sensor 25 with the vertical line perpendicular to fixed frame 10 on section Angle.
Compared with being taken the photograph with the boat of configuration, several circumferential sensors 25 that the utility model is laid by screw type and in The specific laying form of the central sensor 21 of heart setting, can make full use of space, effectively reduce entire structure for pod Volume, structure are compacter;First, the gondola is small, light-weight.Simultaneously by way of this kind of laying, multiple sensor groups It is more accurate to close the information such as acquired figure.
Wherein, sensor is the camera of information used to capture images.Inclination angle alpha value range is 30 degree to 75 degree.More It is 40-50 degree for preferably angle of inclination.
In the present embodiment, the quantity of circumferential sensor 25 is 4.In practical application, the particular number of circumferential sensor 25 It can be arranged according to the actual application, it is therefore preferable to 3-10.
The present embodiment further includes centralized positioning frame 22;Central sensor 21 is removably relatively solid by centralized positioning frame 22 Surely it is connected on fixed frame 10;The positioning positioned for centralized positioning frame 22 is provided between centralized positioning frame 22 and fixed frame 10 Structure.With reference to shown in Fig. 7, centralized positioning frame quantity is two, for repeating precise positioning central sensor.
The present embodiment further includes circumferentially positioned frame 26;With reference to shown in Fig. 6 and Fig. 8, circumferentially positioned frame 26 is to be arranged in circumferential direction The holder of the entirety setting triangular in shape of sensor both sides.
Circumferential sensor 25 is removably relatively fixed by circumferentially positioned frame 26 and is connected on fixed frame 10;It is circumferentially positioned The location structure positioned for circumferentially positioned frame 26 is provided between frame 26 and fixed frame 10.
Wherein, there are many location structure form, and the repetition for being mainly used for locating rack in locating rack disassembly process is accurately positioned, example Locating rack and the positioning pin and locating slot on fixed frame 10 is such as respectively set;
Alternatively, the positioning groove on fixed frame 10 is arranged, bottom and the positioning groove of locating rack match, and locating rack is inserted It is stuck in positioning groove;
Alternatively, be provided with limiting stand on fixed frame 10, locating rack is provided with positioning end face, when installation, the positioning of locating rack End face acts against on limiting stand.
Aerial survey gondola further includes POS modules 30;In the embodiment of the present application, POS modules are inertial nevigation apparatus.
The position limiting structure for limiting 30 position of POS modules is provided on fixed frame 10.Wherein position limiting structure can be fixed The forms such as position slot, positioning protrusion or positioning surface are mainly used for realizing the positioning of POS modules 30.
Location structure and position limiting structure can guarantee that in the gondola course of work, the relative position between sensor is kept not Become and the relative position between sensor and POS modules 30 remains unchanged.
In the prior art, POS modules 30 and sensor are fixed position when mounted, and in the gondola course of work, Relative position between POS modules 30 and sensor can change, in this way, subsequently in the location data based on POS modules 30 (data are the position datas of each sensor determined relative to the relative position of POS modules 30 according to each sensor) When handling the data of sensor acquisition, since the relative position between POS modules 30 and sensor can change, because This, data processing precision will produce deviation, and in the utility model, the relative position between POS modules 30 and sensor is solid Fixed, therefore, data processing precision is high.
In the above-mentioned technical solutions, it is preferable that be provided on centralized positioning frame 22 for limiting 21 position of central sensor Location structure;And the location structure for limiting 25 position of circumferential sensor is provided on circumferentially positioned frame 26.
Referring to Fig.1, shown in 2 and Fig. 9, fixed frame 10 includes top plate 12, bottom plate 11 and connecting pole 13, top plate 12 and bottom plate 11 interval settings, are fixedly connected by several connecting poles 13 between the two;
The accommodation space for accommodating central sensor 21 and circumferential sensor 25 is formed between top plate 12 and bottom plate 11;
It is enclosed with shell 14 on the outside of accommodation space;Shell 14 is tubular, and top plate 12 and bottom plate 11 are separately positioned on cylindrical case In the upper and lower opening's edge of body 14;In the present embodiment, shell 14 has left shell half and right half-shell to be assemblied to form, so it is easy to process and Assembling and the maintenance work in later stage.
11 center of bottom plate is provided with center mounting hole and location structure for installation center sensor 21;
Several periphery mounting holes for installing circumferential sensor 25 are evenly arranged in the circumferential direction of center mounting hole And location structure;
Central sensor 21 and circumferential sensor 25 are arranged in accommodation space, central sensor 21 and circumferential sensor 25 Front end respectively by extending downwardly bottom plate 11 on center mounting hole and periphery mounting hole.Wherein, during location structure is for ensureing Heart sensor and circumferential sensor and fixed frame bottom plate relative position are constant.
Aerial survey gondola further includes several hanging plates 15, and hanging plate 15 is fixed on fixed frame 10;Hanging plate 15 Top plate 12 is stretched out on top upwards, for being connected with aircraft.
Hanging plate 15 is generally arranged at the both sides of fixed frame 10, is provided with threaded hole above, by two pieces of hanging plates 15, The lifting structure of the aerial survey gondola and fixed wing aircraft can be coordinated, be applied to large-scale fixed wing aircraft.
The lifting structure of fixed wing aircraft can have the lifting space of 380mm, coordinate with gondola, be fixed in aircraft cabin Bottom plate 11 on, then by lifting structure aerial survey gondola is hung on outside ventral, can avoid visual angle interference, improve reliability And safety.And the relative position of POS modules 30 and sensor constant also ensures the shadow in lifting structure in the aerial survey gondola The measurement accuracy of picture.
The extension section plate of the aerial survey gondola both sides can also coordinate damped platform, be mounted below helicopter ventral.Or cooperation Passive energy dissipation structure is hung below the ventral of similar mountains and rivers fixed wing aircraft.
Aerial survey gondola further includes for covering 21 head (mirror of 25 head of circumferential sensor (camera lens) and/or central sensor Head) lens case 40.
Lens case 40 includes sequentially connected fixed part, protection department and light shielding part;
Fixed part with the bottom of fixed frame 10 for connecting;
Protection department is tubular, and is sleeved on the outside for leaning out part that sensor front end stretches out bottom plate 11, is passed for protecting Sensor front end leans out part;
Light shielding part is in the front end of the axially projecting sensor of sensor.
Light shielding part prevents veiling glare from being had an impact to sensor shooting, such as prevent from producing in image for blocking veiling glare Hickie, to reduce the quality of image, and light shielding part can also play grease proofing dustproof effect.In flight operation, aircraft oil pipe generates Oil droplet can drift with the wind, light shielding part can effectively prevent oil droplet to be splashed on camera lens, avoid generating spot in image;Protection department Also oil droplet can be obstructed to be splashed on sensor fuselage, while bulky grain dust contaminant sensor (camera) can be effectively prevent.
Lens case 40 is fixed by screw in use, fixed part is contacted with 10 bottom of fixed frame (bottom plate 11).Sensor is logical Cross locating rack to be fixed on fixed frame 10, be placed in the gondola on 10 top of fixed frame to part camera body, partial denudation in In the air of 10 lower part of fixed frame, lens case 40 is added at this time, then exposed aerial sensor can be protected.
Several the circumferential sensors 25 and centrally disposed central sensor that the utility model is laid by screw type 21 specific laying form, can make full use of space, effectively reduce the volume of entire structure for pod, structure is compacter; First, the gondola is small, light-weight.Simultaneously by way of this kind of laying, the letters such as figure acquired in multiple sensor combinations Breath is more accurate.Finally the inclination aerial survey gondola is equipped with general-purpose interface, and operating mode is various, can be used for helicopter, small-sized fixation A variety of flight carriers such as the wing, large-scale fixed-wing.
Finally it should be noted that:The above various embodiments is only to illustrate the technical solution of the utility model, rather than limits it System;Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should Understand:It still can be with technical scheme described in the above embodiments is modified, either to which part or whole Technical characteristic carries out equivalent replacement;And these modifications or replacements, this practicality that it does not separate the essence of the corresponding technical solution are new The range of each embodiment technical solution of type.

Claims (10)

1. a kind of aerial survey gondola, which is characterized in that including:Fixed frame;
And a central sensor being arranged on the fixed frame and several circumferential sensors;
The central sensor is vertically set on the fixed frame;
Several described circumferential sensors are arranged on same circumference centered on by the central sensor;
Helically type is obliquely installed several described circumferential sensors, and angle of inclination is identical.
2. aerial survey gondola according to claim 1, which is characterized in that the angle of inclination is 30 degree to 75 degree.
3. aerial survey gondola according to claim 1, which is characterized in that the quantity of the circumferential direction sensor is 3-10.
4. aerial survey gondola according to claim 1, which is characterized in that further include centralized positioning frame;
The central sensor is removably relatively fixed by the centralized positioning frame and is connected on the fixed frame;
The location structure positioned for centralized positioning frame is provided between the centralized positioning frame and the fixed frame.
5. aerial survey gondola according to claim 4, which is characterized in that further include circumferentially positioned frame;
The circumferential direction sensor is removably relatively fixed by the circumferentially positioned frame to be connected on the fixed frame;
The location structure positioned for circumferentially positioned frame is provided between the circumferentially positioned frame and the fixed frame.
6. aerial survey gondola according to claim 1, which is characterized in that the aerial survey gondola further includes POS modules;It is described POS modules are for recording in operation process, the position of exposure point and posture.
7. aerial survey gondola according to claim 5, which is characterized in that in being provided on the centralized positioning frame for limiting The location structure of heart sensing station;
And/or the location structure for limiting circumferential sensing station is provided on the circumferentially positioned frame.
8. aerial survey gondola according to claim 1, which is characterized in that the fixed frame includes top plate and bottom plate and connection Column, top plate and the setting of bottom plate interval, are fixedly connected by several connecting poles between the two;
The accommodation space for accommodating the central sensor and circumferential sensor is formed between top plate and the bottom plate;The appearance It receives and is enclosed with shell on the outside of space;
The bottom plate center is provided with center mounting hole and location structure for installing the central sensor;
Several periphery installations for installing the circumferential sensor are evenly arranged in the circumferential direction of the center mounting hole Hole and location structure;
The central sensor and the circumferential sensor are arranged in the accommodation space, during the location structure is for ensureing Heart sensor and circumferential sensor and fixed frame bottom plate relative position are constant;The central sensor and the circumferential sensor Front end on the center mounting hole and periphery mounting hole respectively by extending downwardly the bottom plate.
9. aerial survey gondola according to claim 8, which is characterized in that the aerial survey gondola further includes several hanging plates, The hanging plate is fixed on the fixed frame;The top plate is stretched out on the top of hanging plate upwards, for being connected with aircraft.
10. aerial survey gondola according to claim 1, which is characterized in that the aerial survey gondola further includes described for covering The lens case on circumferential sensor head and/or central sensor head.
CN201820082397.7U 2018-01-17 2018-01-17 A kind of aerial survey gondola Expired - Fee Related CN207832183U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820082397.7U CN207832183U (en) 2018-01-17 2018-01-17 A kind of aerial survey gondola

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820082397.7U CN207832183U (en) 2018-01-17 2018-01-17 A kind of aerial survey gondola

Publications (1)

Publication Number Publication Date
CN207832183U true CN207832183U (en) 2018-09-07

Family

ID=63393537

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820082397.7U Expired - Fee Related CN207832183U (en) 2018-01-17 2018-01-17 A kind of aerial survey gondola

Country Status (1)

Country Link
CN (1) CN207832183U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108036775A (en) * 2018-01-17 2018-05-15 北京量子星光科技有限公司 A kind of aerial survey gondola

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108036775A (en) * 2018-01-17 2018-05-15 北京量子星光科技有限公司 A kind of aerial survey gondola

Similar Documents

Publication Publication Date Title
CN106289186B (en) The airborne visual detection of rotor wing unmanned aerial vehicle and multi-target positioning system and implementation method
CN204776013U (en) Six unmanned aerial vehicle
CN112504242B (en) Target correction system and target correction method for hoisting type head-up display
CN106628211A (en) Ground guiding type unmanned aerial vehicle flying landing system and method based on LED dot matrix
CN109739254A (en) Using the unmanned plane and its localization method of visual pattern positioning in a kind of electric inspection process
CN205675254U (en) A kind of aircraft for the video that pans
CN106428595A (en) Built-in image stabilization cradle head for miniature unmanned aerial vehicle
CN204137328U (en) A kind of Micro Aerial Vehicle takes the cradle head mechanism of compare rule orthogonal projection figure fast
CN207832183U (en) A kind of aerial survey gondola
CN205940552U (en) Many rotor unmanned aerial vehicle oblique photography system
CN107972881A (en) A kind of multifunction camera cover and its aerial survey gondola
CN206255209U (en) A kind of built-in steady picture head of SUAV
CN207826583U (en) A kind of multifunction camera cover and its aerial survey gondola
CN105323485B (en) One camera Oblique images capture device and acquisition method
CN114252057A (en) Oblique photography unmanned aerial vehicle surveying and mapping system and device
CN207460350U (en) A kind of unmanned plane
CN108036775A (en) A kind of aerial survey gondola
CN217935703U (en) Airborne large-format aerial photography system device
CN107481234A (en) One kind is used to examine unmanned plane cruising inspection system visual light imaging method for testing performance
CN213566528U (en) Special oblique photography camera of engineering survey and drawing carries on platform
CN105243639B (en) Image adjusting method, device and the system of the photoelectric nacelle of sleeping dress
CN204439995U (en) The five camera holder for aerial photographings that a kind of camera angle is fixing
CN207631514U (en) A kind of portable oblique photograph holder for UAV flight's oblique photograph camera
CN208075839U (en) A kind of swing oblique photograph measurement camera of 100,000,000 pixels
CN206020771U (en) The attitude-control device that many camera lens three-dimensional lives of unmanned plane shoot

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20210121

Address after: 100193 room 340, 3rd floor, building 11, Zhongguancun Software Park, Haidian District, Beijing

Patentee after: Beijing Xingguang Tongshi Technology Co.,Ltd.

Address before: C-1906, 16 / F, building 1, 18 Zhongguancun East Road, Haidian District, Beijing

Patentee before: BEIJING QUANTUM STARLIGHT 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: 20180907