CN106275479A - A kind of double aerial surveying camera helicopter platform mechanism - Google Patents
A kind of double aerial surveying camera helicopter platform mechanism Download PDFInfo
- Publication number
- CN106275479A CN106275479A CN201610865046.9A CN201610865046A CN106275479A CN 106275479 A CN106275479 A CN 106275479A CN 201610865046 A CN201610865046 A CN 201610865046A CN 106275479 A CN106275479 A CN 106275479A
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- CN
- China
- Prior art keywords
- helicopter
- aerial surveying
- surveying camera
- sled
- cross bar
- Prior art date
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- Pending
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- 239000000725 suspension Substances 0.000 claims abstract description 30
- 229910001095 light aluminium alloy Inorganic materials 0.000 claims description 3
- 238000007493 shaping process Methods 0.000 claims description 2
- 238000009434 installation Methods 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 210000001015 abdomen Anatomy 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Accessories Of Cameras (AREA)
Abstract
The invention discloses a kind of double aerial surveying camera helicopter platform mechanism, including two helicopter front portion sled hanging points, two helicopter rear portion ventral hanging points, two instruments lifting cross bar, aerial surveying camera mounting suspension one box aerial surveying camera mounting suspensions two；Wherein an instrument lifting cross bar is arranged between two helicopter front portion sled hanging points, and another root instrument lifting cross bar is arranged between two helicopter rear portion ventral hanging points, and two instrument lifting cross bars be arranged in parallel relative to before and after helicopter direction of advance；Aerial surveying camera mounting suspension one and aerial surveying camera mounting suspension two are arranged between two instrument lifting cross bars, and aerial surveying camera mounting suspension one is fixedly installed in the side of instrument lifting cross bar, and aerial surveying camera mounting suspension two is fixedly installed in the opposite side of instrument lifting cross bar.By above-mentioned helicopter platform mechanism, two aerial surveying cameras can be carried simultaneously, and be easy for installation and removal.
Description
Technical field
The present invention relates to aerial surveying camera field, be specifically related to a kind of double aerial surveying camera helicopter platform mechanism.
Background technology
In today that airborne laser radar is progressively popularized, the carrying platform of aerial surveying camera the most still relies on fixed wing airplane,
As transported 5, fortune 12, PC-6 etc..And helicopter is much larger than fixed wing airplane in the occupation rate that China opens the navigation or air flight, additionally helicopter is motor-driven
Property, selection etc. ageing, landing site better than can only rest in the fixed wing airplane within airport.Therefore, selection is gone straight up to
Machine as the carrying platform of aerial surveying camera more for advantage.
It is all to be arranged on the floor reserved in advance within fixed wing airplane by transition plate that traditional aerial surveying camera is installed
In peephole, and general helicopter is limited by structure, and engine room inside does not has this observation port, and the installation of aerial surveying camera can only
It is mounted to nacelle exterior.But existing platform mechanism, can only carry an aerial surveying camera, and take the photograph after task terminates in boat, need
Aerial surveying camera is dismantled from aircraft, and after dismantling, is difficult to recover original state of aircraft.
Summary of the invention
For the deficiencies in the prior art, the invention aims to provide a kind of double aerial surveying camera helicopter platform mechanism, can
To carry two aerial surveying cameras simultaneously, and it is easy for installation and removal.
For reaching above-mentioned purpose, the technical solution used in the present invention is as follows:
A kind of double aerial surveying camera helicopter platform mechanism, including two helicopter front portion sled hanging points, two helicopter rear portions
Ventral hanging point, two instruments lifting cross bar, aerial surveying camera mounting suspension one box aerial surveying camera mounting suspensions two；Described helicopter front portion is avenged
Sledge hanging point is removably installed in the anterior ventral position of helicopter, is divided into the both sides of helicopter；Described helicopter rear portion machine
Abdomen hanging point is removably installed in the ventral position, rear portion of helicopter, is divided into the both sides of helicopter, anterior with described helicopter
Sled hanging point is corresponding；Wherein an instrument lifting cross bar is arranged between two described helicopter front portion sled hanging points, another root
Instrument lifting cross bar is arranged between two described helicopter rear portion ventral hanging points, and two instrument lifting cross bars are relative to helicopter
It is arranged in parallel before and after direction of advance；Described aerial surveying camera mounting suspension one and aerial surveying camera mounting suspension two are arranged on two instrument liftings
Between cross bar, described aerial surveying camera mounting suspension one is fixedly installed in the side of instrument lifting cross bar, described aerial surveying camera mounting suspension
Two opposite sides being fixedly installed in instrument lifting cross bar.
Further, described helicopter front portion sled hanging point includes front sled clamping ring and extension, described front sled
Clamping ring is clamped on the front sled of helicopter, and described extension is provided with a cirque structure, is used for the lifting cross bar that installs instruments.
Further, described helicopter front portion sled hanging point be provided with several ventrals hanging screw, for by described directly
Rise machine front portion sled hanging point and be removably mounted on the anterior ventral position of helicopter.
Further, described helicopter rear portion ventral hanging point is provided with several ventrals hanging screw, for by after described
Portion's ventral hanging point is removably mounted on the ventral position, rear portion of helicopter.
Further, described helicopter front portion sled hanging point and helicopter rear portion ventral hanging point use 7075 aircraft aluminum to lead to
Cross CNC gang tool and be integrally machined shaping.
Further, described aerial surveying camera mounting suspension one and aerial surveying camera mounting suspension two can be on described instrument lifting cross bars
Laterally adjust mounting distance.
Relative to prior art, the present invention achieves useful technique effect:
(1) " anterior sled hanging point ", " rear portion ventral hanging point " all use 7075 aircraft aluminum by CNC gang tool one
Shape, there is the advantage that the big precision of intensity is high；Its design has also continued the technology requirement of aircraft genuine part, whole in guarantee
The weight that part is overall is alleviated as much as possible on the premise of body intensity.
(2) aerial surveying camera mounting suspension can laterally adjust mounting distance, to adapt to various model on instrument lifting cross bar
Aerial surveying camera；Mounting distance can also be adjusted according to the weight of two aerial surveying cameras, to adjust center of gravity, make helicopter reach equilibrium-like
State, it is ensured that safer efficient flight.
(3) two aerial surveying cameras can be carried simultaneously, and mount and dismount conveniently.
Accompanying drawing explanation
Fig. 1 is the front view of helicopter front portion disclosed by the invention sled hanging point；
Fig. 2 is the top view of helicopter front portion disclosed by the invention sled hanging point；
Fig. 3 is the front view of helicopter rear portion disclosed by the invention ventral hanging point；
Fig. 4 is the top view of helicopter rear portion disclosed by the invention ventral hanging point；
Fig. 5 is the schematic diagram of instrument disclosed by the invention lifting cross bar.
Detailed description of the invention
In order to make the purpose of the present invention, technical scheme and advantage clearer, below in conjunction with embodiment to the present invention
It is further elaborated, but the scope of protection of present invention is not limited to following specific embodiment.
A kind of double aerial surveying camera helicopter platform mechanism, including 1, two helicopter rear portions of two helicopter front portion sled hanging points
Ventral hanging point 5, two instruments lifting cross bar 7, aerial surveying camera mounting suspension one box aerial surveying camera mounting suspensions two.As it is shown in figure 1, go straight up to
Machine front portion sled hanging point 1 includes that front sled clamping ring 2 and extension 3, front sled clamping ring 2 are arranged in the front sled of helicopter
On, and fixed by screw-clamped.Extension 3 is provided with a cirque structure, is used for the lifting cross bar that installs instruments.The size of annulus
Be suitable to instrument lifting cross bar 7 insert.As in figure 2 it is shown, the upper end of helicopter front portion sled hanging point 1 is provided with 4 ventral hanging spiral shells
Hole 4, it coordinates with screw, and helicopter front portion sled hanging point 1 is arranged on ventral position, helicopter front portion.
As it is shown on figure 3, be helicopter rear portion disclosed by the invention ventral hanging point 5.Helicopter rear portion ventral hanging point 5 is provided with one
Cirque structure, annulus is identical with the annulus size of extension 3.As shown in Figure 4, the upper end of helicopter rear portion ventral hanging point 5
Being provided with 4 ventral hanging screws 6, it coordinates with screw, and helicopter rear portion ventral hanging point 5 is arranged on ventral position, helicopter rear portion
Put.
During installation, two helicopter front portion sled hanging points 1 are removably mounted on the anterior ventral position of helicopter, set up separately
In the both sides of helicopter, mutually corresponding.The front sled clamping ring 2 of helicopter front portion sled hanging point 1 is clamped on front sled, extends
The most front sled clamping ring 2 of the circular ring structure in portion 3.Wherein an instrument lifting cross bar 7 is tied from the annular of two extensions 3
Pass at structure, be transversely mounted on ventral position, helicopter front portion.Two helicopter rear portion ventral hanging points 5 are removably mounted on directly
The ventral position, rear portion of the machine of liter, is divided into the both sides of helicopter, mutually corresponding.Another instrument lifting cross bar 7 is after helicopter
Pass at the cirque structure of portion's ventral hanging point, be transversely mounted on ventral position, helicopter rear portion.Two instrument lifting cross bar phases
The most parallel.Aerial surveying camera mounting suspension one and aerial surveying camera mounting suspension two are arranged between two instrument lifting cross bars, and aerial surveying camera is pacified
Dress suspension bracket one is fixedly mounted on the side of instrument lifting cross bar, and aerial surveying camera mounting suspension two is fixedly installed in instrument lifting cross bar
Opposite side.It is adjustable, to adapt to the aerial surveying camera of various model that aerial surveying camera mounting suspension lifts distance horizontal on cross bar at instrument.With
Time can also adjust mounting distance according to the weight of two aerial surveying cameras, to adjust center of gravity, make helicopter reach poised state, it is ensured that
Safer efficient flight.
The announcement of book and teaching according to the above description, those skilled in the art in the invention can also be to above-mentioned embodiment party
Formula changes and revises.Therefore, the invention is not limited in detailed description of the invention disclosed and described above, to invention
A little modifications and changes should also be as falling in the scope of the claims of the present invention.Although additionally, this specification employing
Some specific terms, but these terms are merely for convenience of description, and the present invention does not constitute any restriction.
Claims (6)
1. a double aerial surveying camera helicopter platform mechanism, it is characterised in that: include two helicopter front portion sled hanging points, two straight
Rise machine rear portion ventral hanging point, two instruments lifting cross bar, aerial surveying camera mounting suspension one box aerial surveying camera mounting suspensions two；Described go straight up to
Machine front portion sled hanging point is removably installed in the anterior ventral position of helicopter, is divided into the both sides of helicopter；Described go straight up to
Machine rear portion ventral hanging point is removably installed in the ventral position, rear portion of helicopter, is divided into the both sides of helicopter, with described directly
Rise machine front portion sled hanging point corresponding；Wherein instrument lifting cross bar be arranged on two described helicopter front portion sled hanging points it
Between, another root instrument lifting cross bar is arranged between two described helicopter rear portion ventral hanging points, two instrument lifting cross bar phases
For be arrangeding in parallel before and after helicopter direction of advance；Described aerial surveying camera mounting suspension one and aerial surveying camera mounting suspension two are arranged on two
Between root instrument lifting cross bar, described aerial surveying camera mounting suspension one is fixedly installed in the side of instrument lifting cross bar, and described boat is taken the photograph
Instrument mounting suspension two is fixedly installed in the opposite side of instrument lifting cross bar.
The most according to claim 1 pair of aerial surveying camera helicopter platform mechanism, it is characterised in that: described helicopter front portion sled
Hanging point includes that front sled clamping ring and extension, described front sled clamping ring are clamped on the front sled of helicopter, described in prolong
Extending portion is provided with a cirque structure, is used for the lifting cross bar that installs instruments.
The most according to claim 2 pair of aerial surveying camera helicopter platform mechanism, it is characterised in that: described helicopter front portion sled
Hanging point is provided with several ventrals hanging screw, for described helicopter front portion sled hanging point is removably mounted on helicopter
Anterior ventral position.
The most according to claim 1 pair of aerial surveying camera helicopter platform mechanism, it is characterised in that: described helicopter rear portion ventral
Hanging point is provided with several ventrals hanging screw, for described rear portion ventral hanging point is removably mounted on the rear portion of helicopter
Ventral position.
The most according to claim 1 pair of aerial surveying camera helicopter platform mechanism, it is characterised in that: described helicopter front portion sled
Hanging point and helicopter rear portion ventral hanging point use 7075 aircraft aluminum to be integrally machined shaping by CNC gang tool.
The most according to claim 1 pair of aerial surveying camera helicopter platform mechanism, it is characterised in that: described aerial surveying camera mounting suspension
One and aerial surveying camera mounting suspension two can described instrument lifting cross bar on laterally adjust mounting distance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610865046.9A CN106275479A (en) | 2016-09-29 | 2016-09-29 | A kind of double aerial surveying camera helicopter platform mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610865046.9A CN106275479A (en) | 2016-09-29 | 2016-09-29 | A kind of double aerial surveying camera helicopter platform mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106275479A true CN106275479A (en) | 2017-01-04 |
Family
ID=57715748
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610865046.9A Pending CN106275479A (en) | 2016-09-29 | 2016-09-29 | A kind of double aerial surveying camera helicopter platform mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106275479A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4270711A (en) * | 1979-01-29 | 1981-06-02 | Textron, Inc. | Helicopter landing gear with crosstube pivot |
| US5462242A (en) * | 1993-11-05 | 1995-10-31 | Bell Helicopter Textron Inc. | Helicopter landing gear assembly |
| JPH0943753A (en) * | 1995-07-31 | 1997-02-14 | Chiaki Ochiai | Aerial photographic method for remote controlled aircraft |
| CN1169936A (en) * | 1996-06-10 | 1998-01-14 | 法兰西欧洲科普特公司 | Helicopter landing gear with skids |
| CN101298283A (en) * | 2008-04-15 | 2008-11-05 | 孙卓 | Airborne tripod head apparatus for collecting aerial information and use thereof |
| CN104539905A (en) * | 2015-01-06 | 2015-04-22 | 山东鲁能智能技术有限公司 | Visible light accurate detection system for electric unmanned helicopter |
| KR101598411B1 (en) * | 2015-10-20 | 2016-02-29 | 제주대학교 산학협력단 | Air craft gimbal system for 3demensioins photographic survey |
| CN206087351U (en) * | 2016-09-29 | 2017-04-12 | 广州建通测绘地理信息技术股份有限公司 | Appearance helicopter platform mechanism is taken photograph to two boats |
-
2016
- 2016-09-29 CN CN201610865046.9A patent/CN106275479A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4270711A (en) * | 1979-01-29 | 1981-06-02 | Textron, Inc. | Helicopter landing gear with crosstube pivot |
| US5462242A (en) * | 1993-11-05 | 1995-10-31 | Bell Helicopter Textron Inc. | Helicopter landing gear assembly |
| JPH0943753A (en) * | 1995-07-31 | 1997-02-14 | Chiaki Ochiai | Aerial photographic method for remote controlled aircraft |
| CN1169936A (en) * | 1996-06-10 | 1998-01-14 | 法兰西欧洲科普特公司 | Helicopter landing gear with skids |
| CN101298283A (en) * | 2008-04-15 | 2008-11-05 | 孙卓 | Airborne tripod head apparatus for collecting aerial information and use thereof |
| CN104539905A (en) * | 2015-01-06 | 2015-04-22 | 山东鲁能智能技术有限公司 | Visible light accurate detection system for electric unmanned helicopter |
| KR101598411B1 (en) * | 2015-10-20 | 2016-02-29 | 제주대학교 산학협력단 | Air craft gimbal system for 3demensioins photographic survey |
| CN206087351U (en) * | 2016-09-29 | 2017-04-12 | 广州建通测绘地理信息技术股份有限公司 | Appearance helicopter platform mechanism is taken photograph to two boats |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information |
Address after: 511340 No. 2 Xiangshan Avenue, Yongning Street, Zengcheng District, Guangzhou, Guangdong Province (core zone of Zengcheng Economic and Technological Development Zone) Applicant after: GUANGZHOU JIANTONG MAPPING TECHNOLOGY DEVELOPMENT CO., LTD. Address before: 510000 Guangdong city of Guangzhou province Tianhe District high Cape Road No. 1027 building 6 floor D Applicant before: GUANGZHOU JIANTONG MAPPING TECHNOLOGY DEVELOPMENT CO., LTD. |
|
| CB02 | Change of applicant information | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170104 |
|
| RJ01 | Rejection of invention patent application after publication |