CN102921175B - Model helicopter for aerial photography - Google Patents

Model helicopter for aerial photography Download PDF

Info

Publication number
CN102921175B
CN102921175B CN201210502292.XA CN201210502292A CN102921175B CN 102921175 B CN102921175 B CN 102921175B CN 201210502292 A CN201210502292 A CN 201210502292A CN 102921175 B CN102921175 B CN 102921175B
Authority
CN
China
Prior art keywords
helicopter
model
head frame
tripod head
plane
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
CN201210502292.XA
Other languages
Chinese (zh)
Other versions
CN102921175A (en
Inventor
龙吟
王家云
龙宇
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.)
Guizhou Dadi chart Technology Co. Ltd.
Original Assignee
GUIZHOU XINSHIJIE AERIAL PHOTO 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 GUIZHOU XINSHIJIE AERIAL PHOTO TECHNOLOGY Co Ltd filed Critical GUIZHOU XINSHIJIE AERIAL PHOTO TECHNOLOGY Co Ltd
Priority to CN201210502292.XA priority Critical patent/CN102921175B/en
Publication of CN102921175A publication Critical patent/CN102921175A/en
Application granted granted Critical
Publication of CN102921175B publication Critical patent/CN102921175B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention discloses a model helicopter for aerial photography. The model helicopter comprises a helicopter model (1), a cradle head (2) and remote control equipment, wherein cradle head frames (3) are arranged on the two sides of the helicopter model (1); the tail ends of the cradle head frames (3) are mounted at the tail part of the helicopter model (1); and the cradle head (2) is mounted at the front end of the helicopter model (1) through the cradle head frames (3). According to the invention, the fulcrum of the cradle head frame is located at the tail part of the helicopter, thus the vibration generated by the working engine is first transferred to the fulcrum of the cradle head frame at the tail part and then transferred to the cradle head through a bracket, the distance for vibration transfer is greatly increased, and the final vibration influence is remarkably reduced.

Description

A kind of model helicopter for taking photo by plane
Technical field
The present invention relates to unmanned plane to take photo by plane.
Background technology
Unmanned plane photography of taking photo by plane is using UAV as aerial platform, with airborne sensory equipment, as high resolution CCD digital camera, light optical camera, infrared scanner, the obtaining information such as laser scanner, magnetic determining device, with computer, image information is processed, and be made into image according to certain required precision.
When the little scene in 20-200 rice low latitude makes dynamic, the static shooting of high definition and high-resolution photo, many uses RC Goblin model plane are as aerial platform, the vibration that current Problems existing produces when being helicopter engine work can cause the vibration of capture apparatus, have a strong impact on shooting quality, show as shooting picture more and produce ripple, tremble or photo fuzzy.Vibration be difficult to eliminate reason mainly The Cloud Terrace install fulcrum from vibration source (engine) too close to, and The Cloud Terrace photographs equipment is short relative to the arm of force of fulcrum, vibration can be relayed on The Cloud Terrace and capture apparatus very easily, even if pad adds vibration-absorptive material on The Cloud Terrace installing rack, be also difficult to the impact eliminating vibration.
Summary of the invention
The technical problem to be solved in the present invention: vibrate large problem for the existing model helicopter The Cloud Terrace that platform exists of taking photo by plane, provides and a kind ofly has the model helicopter lengthening tripod head frame structure.
Technical solution of the present invention: a kind of model helicopter for taking photo by plane, comprise helicopter model, The Cloud Terrace and remote control equipment, the both sides of helicopter model are erected with tripod head frame, and the tail end of tripod head frame is arranged on the afterbody of helicopter model, and The Cloud Terrace is arranged on the front end of helicopter model by tripod head frame.
The head both sides of helicopter model are provided with outstanding nail, and tripod head frame is suspended on nail below by elastic tape.
Tripod head frame front end is provided with installing plate, and be fixed on above tripod head frame by elastic tape, The Cloud Terrace is arranged on below installing plate.
Helicopter model is provided with automatic flight controller and controls flight attitude.
The contact position of tripod head frame and helicopter model body is lined with sponge or foamed material.
Tripod head frame adopts the material manufacture different with helicopter model.
Beneficial effect of the present invention:
1. the fulcrum of tripod head frame is positioned at the afterbody of helicopter, producing vibration during such engine operation is mainly first delivered on the The Cloud Terrace support fulcrum of afterbody, be delivered on The Cloud Terrace by support again, vibration transmission is required to be increased greatly through distance, and last vibration effect also can reduce a lot.
2. the front end of tripod head frame is suspended on helicopter by rubber ring, the effect of separating vibration can be produced between support front end and body, reduce the vibration being directly delivered to tripod head frame front end from helicopter body, and certain damping effect is also played to the vibration passed over from tripod head frame fulcrum.
3. the connection between tripod head frame and The Cloud Terrace adopts elastic tape, owing to not being rigidly connected, also can play certain effectiveness in vibration suppression.
4. automatically regulate its flight attitude by flight controller, reduce because of the unstable impact on camera of flying.
5. the making material of tripod head frame is different with helicopter, and the transmission effect vibrated between different materials can be poor.
accompanying drawing illustrates:
Fig. 1 is structural representation of the present invention;
Fig. 2 is the structural representation of tripod head frame of the present invention.
detailed description of the invention:
Helicopter model 1 is for opening up 700 type fuel oil helicopters in Asia, at its head, both sides are installed and 3 outstanding nails 6 are installed respectively, tripod head frame 3 is set up in body both sides, tripod head frame 3 is rectangular frame, tail end is arranged on the afterbody of helicopter model 1 by rope binding, front end is suspended on below outstanding nail 6 by rubber ring 5, and sponge on padding between tripod head frame 3 and helicopter model 1 body.Tripod head frame 3 front end is provided with installing plate 4, and be fixed on above tripod head frame 3 by elastic tape 5, The Cloud Terrace 2 is arranged on the downside of installing plate 4.
Helicopter model 1 is provided with automatic flight controller and controls flight attitude.
Tripod head frame 3 adopts aluminium alloy manufacture.

Claims (6)

1. the model helicopter for taking photo by plane, comprise helicopter model (1), The Cloud Terrace (2) and remote control equipment, it is characterized in that: the both sides of helicopter model (1) are erected with tripod head frame (3), the tail end of tripod head frame (3) is arranged on the afterbody of helicopter model (1), and The Cloud Terrace (2) is arranged on the front end of helicopter model (1) by tripod head frame (3).
2. the model helicopter according to claim 1 for taking photo by plane, is characterized in that: the head both sides of helicopter model (1) are provided with outstanding nail (6), and tripod head frame (3) is suspended on nail (6) below by elastic tape (5).
3. the model helicopter according to claim 1 for taking photo by plane, is characterized in that: tripod head frame (3) front end is provided with installing plate (4), is fixed on above tripod head frame (3) by elastic tape (5), and The Cloud Terrace (2) is arranged on installing plate (4) below.
4. the model helicopter according to claim 1 for taking photo by plane, is characterized in that: helicopter model (1) is provided with automatic flight controller and controls flight attitude.
5. the model helicopter according to claim 1 for taking photo by plane, is characterized in that: the contact position of tripod head frame (3) and helicopter model (1) body is lined with sponge or foamed material.
6. the model helicopter according to claim 1 for taking photo by plane, is characterized in that: tripod head frame (3) adopts the material manufacture different with helicopter model (1).
CN201210502292.XA 2012-11-30 2012-11-30 Model helicopter for aerial photography Expired - Fee Related CN102921175B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210502292.XA CN102921175B (en) 2012-11-30 2012-11-30 Model helicopter for aerial photography

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210502292.XA CN102921175B (en) 2012-11-30 2012-11-30 Model helicopter for aerial photography

Publications (2)

Publication Number Publication Date
CN102921175A CN102921175A (en) 2013-02-13
CN102921175B true CN102921175B (en) 2015-01-28

Family

ID=47636186

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210502292.XA Expired - Fee Related CN102921175B (en) 2012-11-30 2012-11-30 Model helicopter for aerial photography

Country Status (1)

Country Link
CN (1) CN102921175B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106178530A (en) * 2015-04-29 2016-12-07 张斌 Free flight model airplane

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2699263B2 (en) * 1994-07-22 1998-01-19 佐藤建設工業株式会社 Radio-controlled small aircraft
JP2002311498A (en) * 2001-04-19 2002-10-23 Swish Japan:Kk Photographic means for trick shooting and its supporting device
JP2007106267A (en) * 2005-10-13 2007-04-26 Yamaha Motor Co Ltd Unmanned helicopter
CN101298283B (en) * 2008-04-15 2010-09-08 孙卓 Airborne tripod head apparatus for collecting aerial information and use thereof
CN101604830B (en) * 2009-07-14 2011-08-10 山东电力研究院 Unmanned helicopter system for patrolling trolly wire route and tower and method thereof
CN201676524U (en) * 2010-03-22 2010-12-22 重庆市电力公司杨家坪供电局 Connector of wireless remote control model helicopter and vidicon holder

Also Published As

Publication number Publication date
CN102921175A (en) 2013-02-13

Similar Documents

Publication Publication Date Title
US10670183B2 (en) Systems and methods for payload stabilization
WO2021078270A1 (en) Detachable/replaceable gimbal camera, aerial vehicle, system, and gimbal detachment/replacement method
US10597169B2 (en) Method of aerial vehicle-based image projection, device and aerial vehicle
CN105398562A (en) Multifunctional folding type unmanned aerial vehicle
JP2019093868A (en) Control method of unmanned flight vehicle
CN109688323A (en) Unmanned plane Visual Tracking System and its control method
CN105933615A (en) Unmanned aerial vehicle based image acquisition system, image acquisition method and unmanned aerial vehicle
CN204287973U (en) flight camera
WO2018163571A1 (en) Information-processing device, information-processing method, and information-processing program
CN102921175B (en) Model helicopter for aerial photography
WO2017181930A1 (en) Method and device for displaying flight direction, and unmanned aerial vehicle
CN203567947U (en) Self stabilizing holder for unmanned plane
CN203211514U (en) Fixed-wing aircraft for aerial photographing
CN106357981A (en) Shooting system
CN205186546U (en) Unmanned aerial vehicle with anti -trembling function
WO2020244648A1 (en) Aerial vehicle control method and apparatus, and aerial vehicle
CN203208680U (en) Pan-tilt structure on model helicopter
KR102381007B1 (en) Double folding landing gear and Vibration-free gimbal device having it
CN205525020U (en) Aircraft frame
CN108860578A (en) A kind of unmanned plane surveying and mapping data acquisition device
WO2021093577A1 (en) High dynamic range image automatic exposure method and unmanned aerial vehicle
CN207491080U (en) A kind of six camera lens panorama camera arrangements
CN207956088U (en) A kind of pan-shot holder of taking photo by plane of self-stabilization
CN205191125U (en) Unmanned aerial vehicle is with three -axis pan -tilt who has anti -trembling function
CN218343729U (en) Unmanned aerial vehicle takes photo by plane

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20170825

Address after: 550000 B1314 room, Jinli building, Tuyun Road, Guiyang hi tech Industrial Development Zone, Guizhou, China

Patentee after: Guizhou Dadi chart Technology Co. Ltd.

Address before: 550022 building 315, building B, National High-tech Zone Industrial Park, Guizhou, Guiyang

Patentee before: Guizhou Xinshijie Aerial Photo 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: 20150128

Termination date: 20191130