JPH0449518Y2 - - Google Patents
Info
- Publication number
- JPH0449518Y2 JPH0449518Y2 JP7864484U JP7864484U JPH0449518Y2 JP H0449518 Y2 JPH0449518 Y2 JP H0449518Y2 JP 7864484 U JP7864484 U JP 7864484U JP 7864484 U JP7864484 U JP 7864484U JP H0449518 Y2 JPH0449518 Y2 JP H0449518Y2
- Authority
- JP
- Japan
- Prior art keywords
- detector
- drive shaft
- wiring
- piping
- homing device
- 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
Links
- 238000005452 bending Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 230000008602 contraction Effects 0.000 description 1
- 239000000112 cooling gas Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
【考案の詳細な説明】
本考案は飛しよう体のホーミング装置に関す
る。[Detailed Description of the Invention] The present invention relates to a homing device for a flying object.
第１図及び第２図に従来の飛しよう体用ホーミ
ング装置の１例が示され、第１図は部分的に破断
して示す正面図、第２図は第１図の−線に沿
う横断面図である。 An example of a conventional homing device for a flying object is shown in FIGS. 1 and 2. FIG. 1 is a partially cutaway front view, and FIG. 2 is a cross-sectional view taken along the line - in FIG. 1. It is a front view.
第１図及び第２図において、１はドーム、２は
ドーム１内に配設されたフレーム、３はアウタジ
ンバルで、その軸４を軸受５を介してフレーム２
に軸支し、モータ６を正逆転することにより軸４
まわりに回動して所定の方位角を占める。７は目
標を検知するための検知装置で、その軸８を軸受
９を介してアウタジンバル３に軸支し、モータ１
０を正逆転することにより軸８まわりに回動して
所定の昇降角を占める。１１は検知装置３を冷却
するための冷却ガスを送給する配管、１２は検知
装置３からの信号を伝送し、またはモータ６及び
１０に電気を送給するための配線、１３はバルク
ヘツドである。 1 and 2, 1 is a dome, 2 is a frame disposed inside the dome 1, 3 is an outer gimbal, and the shaft 4 is connected to the frame via a bearing 5.
By rotating the motor 6 forward and backward, the shaft 4
It rotates around and occupies a predetermined azimuth angle. 7 is a detection device for detecting a target, the shaft 8 of which is supported on the outer gimbal 3 via a bearing 9, and the motor 1
0 in the forward and reverse directions, it rotates around the shaft 8 and occupies a predetermined elevation angle. 11 is a pipe for supplying cooling gas to cool the detection device 3; 12 is a wiring for transmitting a signal from the detection device 3 or for supplying electricity to the motors 6 and 10; and 13 is a bulkhead. .
上記従来の装置においては配管１１及び配線１
２が検知装置７の方位方向及び昇降方向への揺動
に伴つて引き摺られ又は伸縮するのでこれら配管
１１及び配線１２の摺動による摩擦力や、伸縮に
よる曲げ応力によつて検知装置７の方位方向及び
昇降方向への円滑な揺動が阻害されるとともに配
管１１や配線１２が摩耗し又は曲げ荷重により破
損するおそれがあつた。 In the conventional device described above, piping 11 and wiring 1
2 is dragged or expands and contracts as the detector 7 swings in the azimuth direction and the vertical direction, so the orientation of the detector 7 is affected by the frictional force caused by the sliding of these piping 11 and the wiring 12 and the bending stress caused by the expansion and contraction. Smooth rocking in the vertical and vertical directions was hindered, and there was a risk that the piping 11 and wiring 12 would be worn out or damaged by bending loads.
本考案は上記問題に対処するために提案された
ものであつて、その要旨とするところは、ドーム
内に配設されたフレームに駆動軸を介して軸支さ
れたアウタジンバルと、該アウタジンバルに駆動
軸を介して軸支された検知器を具えた飛しよう体
用ホーミング装置において、上記検知器に連結さ
れる配管を上記各駆動軸の軸芯を中心とするコイ
ル状に巻回し、上記検知器に連結される配線と共
に上記各駆動軸にその軸方向に穿設された穴を貫
通せしめたことを特徴とする飛しよう体用ホーミ
ング装置にある。 The present invention was proposed to address the above-mentioned problems, and its gist consists of an outer gimbal supported via a drive shaft on a frame disposed within a dome; In a homing device for a flying object, the piping connected to the detector is wound in a coil shape around the axis of each of the drive shafts. There is provided a homing device for a flying object, characterized in that a hole drilled in the axial direction of each of the drive shafts is passed through along with wiring connected to the detector.
本考案においては上記構成を具えているため、
検知器に連結された配管及び配線は検知器の方位
方向及び昇降方向への揺動によつて引き摺られ又
は伸縮することがないとともに配管は各駆動軸の
軸芯を中心とするコイル状に巻回されているの
で、検知器の揺動に伴なう捩り応力を緩和でき
る。かくして、配管及び配線の摩擦力や曲げ応力
及び捩り応力によつて検知器の円滑な揺動を阻害
することはなく、また、配管や配線が摩耗したり
これに負荷される応力によつて破損するおそれも
ない。 Since the present invention has the above configuration,
The piping and wiring connected to the detector will not be dragged or expanded or contracted by the swinging of the detector in the azimuth direction and the vertical direction, and the piping is wound in a coil shape around the axis of each drive shaft. Since the sensor is rotated, the torsional stress caused by the swinging of the detector can be alleviated. In this way, the frictional force, bending stress, and torsional stress of the piping and wiring will not impede the smooth swinging of the detector, and the piping and wiring will not be damaged due to wear or stress applied to them. There's no risk of it happening.
以下本考案を第３図及び第４図に示す１実施例
を参照しながら具体的に説明する。 The present invention will be specifically explained below with reference to an embodiment shown in FIGS. 3 and 4.
第３図及び第４図に示すように、配管１１は駆
動軸４の軸芯を中心とするコイル状に巻回された
後駆動軸４にその軸方向に穿設された穴４ａを貫
通し、次いで駆動軸８の外端に導かれて駆動軸８
にその軸方向に穿設された穴８ａ内を駆動軸８の
軸芯を中心とするコイル状に巻回しながら貫通し
て検知器７に連結される。配線１２は駆動軸４の
穴４ａ及び駆動軸８の穴８ａ内をこの順に貫通し
て検知器７に連結される。他の構成は第１図及び
第２図に示す従来のものと同様であり、対応する
部材には同じ符号が付されている。 As shown in FIGS. 3 and 4, the pipe 11 is wound into a coil around the axis of the drive shaft 4, and then passes through a hole 4a drilled in the drive shaft 4 in the axial direction. , then guided to the outer end of the drive shaft 8
The drive shaft 8 is connected to the detector 7 by passing through the hole 8 a bored in the axial direction while being wound in a coil shape around the axis of the drive shaft 8 . The wiring 12 passes through the hole 4a of the drive shaft 4 and the hole 8a of the drive shaft 8 in this order, and is connected to the detector 7. The rest of the structure is similar to the conventional one shown in FIGS. 1 and 2, and corresponding members are given the same reference numerals.
しかして、配管１１及び配線１２は駆動軸４の
穴４ａ及び駆動軸８の穴８ａを貫通しているの
で、検知器７を方位方向及び昇降方向に指向させ
るため検知器７が軸８まわりに回動しかつ、アウ
タジンバル３が軸４まわりに回動しても配管１１
及び配線１２は引き摺られ又は伸縮することがな
い。そして配管１１は軸８及び軸４の軸芯を中心
とするコイル状に巻回されているので軸８及び軸
４の回動に伴う捩り応力を緩和できる。かくし
て、配管１１及び配線１２の摩擦力、曲げ応力及
び捩り応力によつて検知器の円滑な揺動を妨げる
ことはなく、また、配管及び配線が摩耗したり、
これに負荷される応力によつて破損することもな
い。 Since the piping 11 and the wiring 12 pass through the hole 4a of the drive shaft 4 and the hole 8a of the drive shaft 8, the detector 7 moves around the shaft 8 in order to orient the detector 7 in the azimuth direction and the vertical direction. Even if the outer gimbal 3 rotates around the axis 4, the piping 11
And the wiring 12 will not be dragged or expanded or contracted. Since the pipe 11 is wound in a coil shape around the axes of the shafts 8 and 4, torsional stress caused by rotation of the shafts 8 and 4 can be alleviated. In this way, the frictional force, bending stress, and torsional stress of the piping 11 and wiring 12 will not hinder the smooth swinging of the detector, and the piping and wiring will not be worn out.
It will not be damaged by stress applied to it.
第１図は従来の飛しよう体用ホーミング装置を
部分的に破断して示す正面図、第２図は第１図の
−線に沿う断面図、第３図は本考案の１実施
例を部分的に破断して示す正面図、第４図は第３
図の−線に沿う断面図である。
ドーム……１、フレーム……２、駆動軸……
４、アウタジンバル……３、駆動軸……８、検知
器……７、配管……１１、配線……１２、駆動軸
に穿設された穴……４ａ，８ａ。
Fig. 1 is a partially cutaway front view of a conventional homing device for flying objects, Fig. 2 is a sectional view taken along the - line in Fig. 1, and Fig. 3 is a partial view of an embodiment of the present invention. A front view cut away and shown in Fig. 3.
It is a sectional view taken along the - line in the figure. Dome...1, Frame...2, Drive shaft...
4, Outer gimbal...3, Drive shaft...8, Detector...7, Piping...11, Wiring...12, Hole drilled in the drive shaft...4a, 8a.
Claims (1)
て軸支されたアウタジンバルと、該アウタジンバ
ルに駆動軸を介して軸支された検知器を具えた飛
しよう体用ホーミング装置において、上記検知器
に連結される配管を上記各駆動軸の軸芯を中心と
するコイル状に巻回し、上記検知器に連結される
配線と共に上記各駆動軸にその軸方向に穿設され
た穴を貫通せしめたことを特徴とする飛しよう体
用ホーミング装置。 In the homing device for a flying object, the homing device includes an outer gimbal that is supported via a drive shaft on a frame disposed in a dome, and a detector that is supported via the drive shaft on the outer gimbal. The piping connected to the detector is wound into a coil around the axis of each of the drive shafts, and the wiring connected to the detector is passed through holes drilled in the axial direction of each of the drive shafts. A homing device for a flying body, which is characterized by:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7864484U JPS60191921U (en) | 1984-05-30 | 1984-05-30 | Homing device for flying objects |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7864484U JPS60191921U (en) | 1984-05-30 | 1984-05-30 | Homing device for flying objects |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS60191921U JPS60191921U (en) | 1985-12-19 |
| JPH0449518Y2 true JPH0449518Y2 (en) | 1992-11-20 |
Family
ID=30622807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7864484U Granted JPS60191921U (en) | 1984-05-30 | 1984-05-30 | Homing device for flying objects |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60191921U (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008139250A (en) * | 2006-12-05 | 2008-06-19 | Toshiba Corp | Gimbal device |
| US8205514B2 (en) * | 2008-01-18 | 2012-06-26 | Honeywell International Inc. | Control moment gyroscope |
-
1984
- 1984-05-30 JP JP7864484U patent/JPS60191921U/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS60191921U (en) | 1985-12-19 |
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