JPH02131741U - - Google Patents
Info
- Publication number
- JPH02131741U JPH02131741U JP3795589U JP3795589U JPH02131741U JP H02131741 U JPH02131741 U JP H02131741U JP 3795589 U JP3795589 U JP 3795589U JP 3795589 U JP3795589 U JP 3795589U JP H02131741 U JPH02131741 U JP H02131741U
- Authority
- JP
- Japan
- Prior art keywords
- camera
- photographing
- strobe
- light
- aerial
- 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.)
- Pending
Links
- 230000011514 reflex Effects 0.000 claims description 5
- 238000001514 detection method Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 238000012544 monitoring process Methods 0.000 claims description 3
- 239000013307 optical fiber Substances 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- 239000011888 foil Substances 0.000 claims 1
- 230000003287 optical effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Landscapes
- Details Of Cameras Including Film Mechanisms (AREA)
Description
図面は本考案に係る無人ヘリコプタの航空撮影
装置の実施例を示したもであつて、第１図は本考
案装置を装着したヘリコプタの一部切欠した側面
図、第２図は同上の一部切欠した下面図、第３図
は同上正面図、第４図は同上に於ける撮影手段の
載架台の機体への吊支状態を示した正面図、第５
図は同上側面図、第６図は撮影手段の第一実施例
の構成図、第７図は撮影手段の第二実施例の構成
図、第８図は撮影手段の第三実施例の一部切欠し
た構成図、第９図は同上に於ける一部拡大断面側
面図、第１０図は第５図に於ける閃光検知手段の
一部拡大断面側面図である。
１はヘリコプタ機本体、２は着陸装置、３は制
御手段、４はレンズシヤツター、５はスイツチケ
ーブル、６は光フアイバケーブル、７はサーボ装
置、８は緩衝手段、９は載架台、１０は撮影手段
、１１は撮影用カメラ、１１′は一眼レフカメラ
、１２はモニター用テレビカメラ、１３は確認用
ストロボ、１４はストロボスイツチケーブル、１
５はテレビカメラのレンズ、１６は光通過空間、
１７はカメラフアインダー接眼部、１８は小型反
射鏡、１９は光フアイバーケーブル（一眼レフカ
メラの場合）、２０は発光スイツチ手段、２１は
閃光検知手段、２２は反射膜体、２３は側壁、２
４は半球椀状透明体、２５，２５′は角部、２６
は機体フレーム、２７はスキツド、２８は上部緩
衝材、２９は下部緩衝材、３０は着陸装置廻動軸
、３１はシヨツクアブソーバー、３２はギヤー、
３３は出力ピニオン、３４は下部フレーム、３５
はサーボモータ、３６はスラストメタル、３７は
チルト用ギヤー、３８は出力ギヤー、３９は下部
機体フレーム、４０は電気式シヤツタースイツチ
用ケーブル。
The drawings show an embodiment of the aerial photographing device for an unmanned helicopter according to the present invention, in which Fig. 1 is a partially cutaway side view of a helicopter equipped with the device of the present invention, and Fig. 2 is a partially cutaway side view of the helicopter equipped with the device of the present invention. A cutaway bottom view, FIG. 3 is a front view of the same as above, FIG.
The figure is a side view of the same as above, FIG. 6 is a block diagram of the first embodiment of the photographing means, FIG. 7 is a block diagram of the second embodiment of the photographing means, and FIG. 8 is a part of the third embodiment of the photographing means. FIG. 9 is a partially enlarged cross-sectional side view of the same as above, and FIG. 10 is a partially enlarged cross-sectional side view of the flash detection means in FIG. 5. 1 is a helicopter body, 2 is a landing gear, 3 is a control means, 4 is a lens shutter, 5 is a switch cable, 6 is an optical fiber cable, 7 is a servo device, 8 is a buffer means, 9 is a mounting stand, 10 is Photographing means, 11 is a camera for photographing, 11' is a single-lens reflex camera, 12 is a television camera for monitoring, 13 is a strobe for confirmation, 14 is a strobe switch cable, 1
5 is a TV camera lens, 16 is a light passage space,
17 is a camera viewfinder eyepiece, 18 is a small reflector, 19 is an optical fiber cable (for a single-lens reflex camera), 20 is a light emitting switch means, 21 is a flash detection means, 22 is a reflective film body, 23 is a side wall, 2
4 is a hemispherical bowl-shaped transparent body, 25 and 25' are corner parts, 26
is the fuselage frame, 27 is the skid, 28 is the upper cushioning material, 29 is the lower cushioning material, 30 is the landing gear rotation axis, 31 is the shock absorber, 32 is the gear,
33 is the output pinion, 34 is the lower frame, 35
is the servo motor, 36 is the thrust metal, 37 is the tilt gear, 38 is the output gear, 39 is the lower fuselage frame, and 40 is the cable for the electric shutter switch.
Claims (1)
との間に、該着陸装置２と一緒に左右に回動し得
るように、撮影用カメラ１１及び該撮影用カメラ
１１の撮影する影像のモニター用のテレビカメラ
１２等を含む撮影手段１０の載架台９を着陸装置
２に緩衝手段８を介して装着したことを特徴とす
る無人ヘリコプタの航空撮影装置。 ２ 前記撮影用カメラ１１のシヤツタ作動時に該
作動の確認用ストロボ１３を発光せしめる発光ス
イツチ手段２０を設け、而かも前記ストロボ１３
の閃光を地上で検知する閃光検知手段２１を有す
ることを特徴とする請求項１記載の航空撮影装置
。 ３ 前記発光スイツチ手段２０が、地上からの指
令を受信して前記撮影用カメラ１１の操作をする
制御手段３から該撮影用カメラ１１へのシヤツタ
作動の指令と同時にストロボ１３への発光用電流
を送るようにストロボスイツチケーブル１４を設
けたものであることを特徴とする請求項１記載の
航空撮影装置。 ４ 前記撮影用カメラ１１が一眼レフカメラ１１
′であつて、該一眼レフカメラ１１′にモニター
用のテレビカメラ１２を設けたことを特徴とする
請求項１記載の航空撮影装置。 ５ 前記一眼レフカメラ１１′のカメラフアイン
ダー接眼部１７とテレビカメラ１２のレンズ１５
との間の光通過空間１６の光軸に対し４５゜に傾
斜した小型反射鏡１８を配設し、該小型反射鏡１
８に対し４５゜の傾斜角で前記ストロボ１３から
の閃光を当てるように該ストロボ１３からの光フ
アイバーケーブル１９を光通過空間１６の側壁２
３に配置し、ストロボ１３の閃光をテレビカメラ
１２の撮影素子に映し出させるようにしたことを
特徴とする請求項４記載の航空撮影装置。 ６ 前記ストロボ１３の閃光の地上からの視察の
ために、ストロボ１３の発光の方向の所要位置に
半球椀状透明体２４を配設し、該半球椀状透明体
２４の内面にアルミ箔の如き反射膜体２２を所要
の隙間を置いて貼着せしめたことを特徴とする請
求項２記載の航空撮影装置。[Scope of claims for utility model registration] 1. Helicopter body 1 and its lower landing gear 2
A photographing means 10 including a photographing camera 11 and a television camera 12 for monitoring images photographed by the photographing camera 11 is mounted between the landing gear 2 and the landing gear 2 so as to be able to rotate left and right together. An aerial photography device for an unmanned helicopter, characterized in that a mount 9 is attached to a landing gear 2 via a buffer means 8. 2. A light emitting switch means 20 is provided for causing the strobe 13 for confirming the operation to emit light when the shutter of the photographing camera 11 is operated, and the strobe 13
2. The aerial photographing apparatus according to claim 1, further comprising flash detection means (21) for detecting the flash of light on the ground. 3 The light emitting switch means 20 receives a command from the ground to operate the photographing camera 11, and at the same time receives a shutter operation command to the photographing camera 11 from the control means 3 which controls the photographing camera 11. 2. The aerial photographing apparatus according to claim 1, further comprising a strobe switch cable (14) for transmitting the strobe light. 4 The photographing camera 11 is a single-lens reflex camera 11
2. An aerial photographing apparatus according to claim 1, wherein said single-lens reflex camera 11' is provided with a television camera 12 for monitoring. 5 Camera viewfinder eyepiece 17 of the single-lens reflex camera 11' and lens 15 of the television camera 12
A small reflecting mirror 18 is arranged at an angle of 45° to the optical axis of the light passing space 16 between the small reflecting mirror 1.
The optical fiber cable 19 from the strobe 13 is connected to the side wall 2 of the light passage space 16 so that the flash from the strobe 13 is directed at an angle of 45° relative to the
5. The aerial photographing apparatus according to claim 4, wherein the aerial photographing device is arranged at a position of 3, and the flash of the strobe 13 is reflected on a photographing element of the television camera 12. 6. In order to observe the flash of the strobe 13 from the ground, a hemispherical bowl-shaped transparent body 24 is arranged at a predetermined position in the direction of light emission of the strobe 13, and the inner surface of the hemispherical bowl-shaped transparent body 24 is coated with a material such as aluminum foil. 3. The aerial photographing apparatus according to claim 2, wherein the reflective film body 22 is attached with a required gap.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3795589U JPH02131741U (en) | 1989-04-03 | 1989-04-03 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3795589U JPH02131741U (en) | 1989-04-03 | 1989-04-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02131741U true JPH02131741U (en) | 1990-11-01 |
Family
ID=31545531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3795589U Pending JPH02131741U (en) | 1989-04-03 | 1989-04-03 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02131741U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20010103221A (en) * | 2000-05-08 | 2001-11-23 | 사태형 | landing skid structure of wireless movie camera system |
| KR20010104564A (en) * | 2000-05-15 | 2001-11-26 | 사태형 | vibration absorbation structure of wireless movie camera system |
| WO2016059877A1 (en) * | 2014-10-17 | 2016-04-21 | ソニー株式会社 | Controller, control method, and flight vehicle device |
| JP6024074B1 (en) * | 2016-04-19 | 2016-11-09 | 株式会社ニチギ | Unmanned moving body for photography |
| WO2018088028A1 (en) * | 2016-11-09 | 2018-05-17 | 積水ポリマテック株式会社 | Vibration control device and unmanned aircraft |
-
1989
- 1989-04-03 JP JP3795589U patent/JPH02131741U/ja active Pending
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20010103221A (en) * | 2000-05-08 | 2001-11-23 | 사태형 | landing skid structure of wireless movie camera system |
| KR20010104564A (en) * | 2000-05-15 | 2001-11-26 | 사태형 | vibration absorbation structure of wireless movie camera system |
| WO2016059877A1 (en) * | 2014-10-17 | 2016-04-21 | ソニー株式会社 | Controller, control method, and flight vehicle device |
| JPWO2016059877A1 (en) * | 2014-10-17 | 2017-07-27 | ソニー株式会社 | Control apparatus, control method, and air vehicle device |
| US10011371B2 (en) | 2014-10-17 | 2018-07-03 | Sony Corporation | Control device, control method, and flight vehicle device |
| JP6024074B1 (en) * | 2016-04-19 | 2016-11-09 | 株式会社ニチギ | Unmanned moving body for photography |
| WO2018088028A1 (en) * | 2016-11-09 | 2018-05-17 | 積水ポリマテック株式会社 | Vibration control device and unmanned aircraft |
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