JPH0810963Y2 - Aerial line lifting device - Google Patents
Aerial line lifting deviceInfo
- Publication number
- JPH0810963Y2 JPH0810963Y2 JP2668190U JP2668190U JPH0810963Y2 JP H0810963 Y2 JPH0810963 Y2 JP H0810963Y2 JP 2668190 U JP2668190 U JP 2668190U JP 2668190 U JP2668190 U JP 2668190U JP H0810963 Y2 JPH0810963 Y2 JP H0810963Y2
- Authority
- JP
- Japan
- Prior art keywords
- antenna
- inner cylinder
- lifting device
- cylinder
- handle
- 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 - Lifetime
Links
Landscapes
- Details Of Aerials (AREA)
- Support Of Aerials (AREA)
Description
【考案の詳細な説明】 〔産業上の利用分野〕 本考案は航空機に搭載する空中線の取付構造に関し、
特にヘリコプタに搭載するマイクロ波帯の昇降式の空中
線の昇降装置に関する。[Detailed Description of the Invention] [Industrial field of application] The present invention relates to a structure for mounting an antenna mounted on an aircraft,
In particular, the present invention relates to a microwave band lifting type antenna elevating device mounted on a helicopter.
従来、この種の空中線の昇降装置は、第５図の様な構
造となっていた。即ち、内筒24の下端には空中線22が空
中線フランジ部23を介して固定されており、この内筒24
はフランジ部25の軸受け21,26に軸支され、手動により
軸方向に移動し昇降する。ロック機構27をロックすると
内筒24は固定され、一方、ロックをゆるめると内筒24と
共に空中線22が昇降可能となる。なお、空中線22は無指
向性空中線であり、指向制御が不要なため、空中線制御
接栓等の取付構造を具備していない。Conventionally, this type of antenna lifting device has a structure as shown in FIG. That is, the antenna 22 is fixed to the lower end of the inner cylinder 24 via the antenna flange portion 23.
Is rotatably supported by bearings 21 and 26 of the flange portion 25, and is manually moved in the axial direction to move up and down. When the lock mechanism 27 is locked, the inner cylinder 24 is fixed, while when the lock is loosened, the antenna 22 can be moved up and down together with the inner cylinder 24. Since the antenna 22 is an omnidirectional antenna and does not require directivity control, it is not equipped with a mounting structure such as an antenna control connector.
上述した従来の空中線の昇降装置は、次のような欠点
を有していた。The above-described conventional antenna lifting device has the following drawbacks.
（１）手で持ち上下させる構造であるため、重量のある
大形空中線の場合は重く、また不用意に落下させる場合
もあり危険である。(1) Since it is a structure that it is held up and down by hand, a large antenna with a large weight is heavy and may be dropped accidentally, which is dangerous.
（２）軸受け部も外筒の中間部及び下部となっているた
め、大形の重量のある空中線の場合、下降時に飛行によ
る風圧により強度上不安が残る。(2) Since the bearings are also located in the middle and lower part of the outer cylinder, in the case of a large and heavy antenna, there is a concern about the strength due to the wind pressure during flight when descending.
（３）空中線の取付けに空中線導波管フランジのみに頼
っており、大形重量空中線の場合不適当である。(3) Only the antenna waveguide flange is used for mounting the antenna, and it is not suitable for a large weight antenna.
（４）空中線制御接栓を取付けできる構造ではない。(4) It is not a structure that can attach the antenna control connector.
本考案の空中線の昇降装置は、筒状をなし下端部に空
中線を取付け固定し該空中線の接続導波管及び接続ケー
ブルを内部に貫通させ且つ外面の軸方向にラック歯車を
設けてなる内筒と、筒状をなし内面の上部及び下部に軸
受けを設けて前記内筒を嵌挿させ且つ外面の中間部に取
付フランジを設けてなる外筒と、該外筒の上部に設けら
れ前記ラック歯車に噛み合うギヤ及びそのハンドルを有
し該ハンドルを回すことにより前記内筒を上下移動させ
るギヤ機構と、前記内筒の上部に嵌合し該内筒の上下移
動を固定するクランプ機構とを備えてある。The antenna lifting device according to the present invention is an inner cylinder having a tubular shape and having an antenna attached and fixed to the lower end thereof to allow the connecting waveguide and connecting cable of the antenna to penetrate therethrough and to provide a rack gear in the axial direction of the outer surface. An outer cylinder having a cylindrical shape and bearings provided on the upper and lower portions of the inner surface to fit and insert the inner cylinder and a mounting flange at the intermediate portion of the outer surface; and the rack gear provided on the upper portion of the outer cylinder. A gear mechanism that has a gear meshing with and a handle for moving the inner cylinder up and down by turning the handle; and a clamp mechanism that fits on the upper portion of the inner cylinder and fixes the vertical movement of the inner cylinder. is there.
次に、本考案について図面を参照して説明する。 Next, the present invention will be described with reference to the drawings.
第１図（ａ），（ｂ）は本考案の一実施例のヘリコプ
タへの搭載状況を示す部分断面を含む正面図、第２図及
び第３図は本実施例の縦断面図及び右側面図、第４図
（ａ）及び（ｂ）は第２図のＡ−Ａ線矢視図及びＢ−Ｂ
線断面図である。FIGS. 1 (a) and 1 (b) are front views including a partial cross section showing a mounting state of a helicopter according to an embodiment of the present invention, and FIGS. 2 and 3 are a longitudinal sectional view and a right side surface of the embodiment. FIGS. 4 (a) and 4 (b) are views taken along the line AA of FIG. 2 and BB.
It is a line sectional view.
本実施例は第１図に示すようにヘリコプタ16に搭載さ
れ、内筒２が外筒６内を上下して空中線１が昇降するよ
うになっている。詳しくは第２図ないし第４図に示すよ
うに、空中線１に接続ケーブル３及び接続導波管４が接
続されており、内筒２に空中線１が固定されている。外
筒６の上部と下部には十分な間隔を保って２個の軸受け
５があり、内筒２をガイドしている。外筒６の中間部に
は取付けフランジ７が設けらている。第３図に示すよう
に、内筒２の軸方向に取付けられたラック８と、外筒６
の上部に取付けられたギヤボックス９内のギヤとがかみ
あい、ギヤボックス９のハンドル11を回転させることに
より、内筒２を上下させることができる。さらに外筒６
上方の内筒２にはクランプ機構10が設けられ、第４図
（ａ）に示すように、クランプノブ12を回して締め付け
る事により、締め付けフランジ部13の２箇所の突起部14
の間隔15がつまり、内筒２を軸方向及び回転方向に固定
させることができる。In the present embodiment, as shown in FIG. 1, the helicopter 16 is mounted so that the inner cylinder 2 moves up and down in the outer cylinder 6 so that the antenna 1 moves up and down. More specifically, as shown in FIGS. 2 to 4, the connecting cable 3 and the connecting waveguide 4 are connected to the antenna 1, and the antenna 1 is fixed to the inner cylinder 2. Two bearings 5 are provided at an upper portion and a lower portion of the outer cylinder 6 with a sufficient space therebetween to guide the inner cylinder 2. A mounting flange 7 is provided at an intermediate portion of the outer cylinder 6. As shown in FIG. 3, the rack 8 mounted in the axial direction of the inner cylinder 2 and the outer cylinder 6
The inner cylinder 2 can be moved up and down by meshing with the gear in the gear box 9 attached to the upper part of the box and rotating the handle 11 of the gear box 9. Outer cylinder 6
The upper inner cylinder 2 is provided with a clamp mechanism 10, and as shown in FIG. 4 (a), the clamp knob 12 is rotated and tightened so that two protrusions 14 of the tightening flange 13 are formed.
That is, the inner cylinder 2 can be fixed in the axial direction and the rotation direction.
このような本実施例によれば、ラック８を有する内筒
２を、このラック８とかみ合うギヤボックス９のハンド
ル11の回転で上下させ、空中線１を昇降させることがで
きる。According to the present embodiment as described above, the inner cylinder 2 having the rack 8 can be moved up and down by the rotation of the handle 11 of the gear box 9 that meshes with the rack 8 to raise and lower the antenna 1.
以上説明したように本考案は、空中線を固定した内筒
にラックを設け、これとかみ合うギヤボックスのハンド
ルを回転させることにより、重量のある大形空中線を確
実に昇降装置に取付け、強度上不安のない昇降装置を提
供でき、操作も安全に下降及び上昇を行わせることがで
きる効果がある。As described above, according to the present invention, the rack is provided on the inner cylinder to which the antenna is fixed, and the handle of the gear box that meshes with the rack is rotated to securely attach the heavy antenna to the lifting device. It is possible to provide an elevating device that does not have the effect of being able to safely lower and raise the operation.
第１図（ａ），（ｂ）は本考案の一実施例のヘリコプタ
への搭載状況を示す部分断面を含む正面図、第２図及び
第３図は本実施例の縦断面図及び右側面図、第４図
（ａ）及び（ｂ）は第２図のＡ−Ａ矢視図及びＢ−Ｂ線
断面図、第５図（ａ）及び（ｂ）は従来の昇降装置の一
例を示す断面図及び上面図である。 1,22……空中線、２……内筒、３……接続ケーブル、４
……接続導波管、５……軸受け、６……外筒、７……取
付けフランジ、８……ラック、９……ギヤボックス、10
……クランプ機構部、11……ハンドル、12……クランプ
ノブ、13……締め付けフランジ部、14……突起部、15…
…間隔、16……ヘリコプタ。FIGS. 1 (a) and 1 (b) are front views including a partial cross section showing a mounting state of a helicopter according to an embodiment of the present invention, and FIGS. 2 and 3 are a longitudinal sectional view and a right side surface of the embodiment. FIGS. 4 (a) and 4 (b) are sectional views taken along line AA and BB in FIG. 2, and FIGS. 5 (a) and 5 (b) show an example of a conventional lifting device. It is a sectional view and a top view. 1,22 …… Aerial line, 2 …… Inner tube, 3 …… Connection cable, 4
...... Connection waveguide, 5 ... Bearing, 6 ... Outer cylinder, 7 ... Mounting flange, 8 ... Rack, 9 ... Gear box, 10
…… Clamp mechanism, 11 …… Handle, 12 …… Clamp knob, 13 …… Tightening flange, 14 …… Protrusion, 15…
… Interval, 16 …… Helicopter.
Claims (1)
該空中線の接続導波管及び接続ケーブルを内部に貫通さ
せ且つ外面の軸方向にラック歯車を設けてなる内筒と、
筒状をなし内面の上部及び下部に軸受けを設けて前記内
筒を嵌挿させ且つ外面の中間部に取付フランジを設けて
なる外筒と、該外筒の上部に設けられ前記ラック歯車に
噛み合うギヤ及びそのハンドルを有し該ハンドルを回す
ことにより前記内筒を上下移動させるギヤ機構と、前記
内筒の上部に嵌合し該内筒の上下移動を固定するクラン
プ機構とを備えることを特徴とする空中線の昇降装置。1. An inner cylinder having a cylindrical shape and having an antenna attached and fixed to a lower end thereof, a connecting waveguide and a connecting cable of the antenna penetrating therethrough, and a rack gear provided axially on an outer surface thereof.
An outer cylinder, which is cylindrical and has bearings provided on the upper and lower portions of the inner surface to fit and insert the inner cylinder and a mounting flange at the intermediate portion of the outer surface, and meshes with the rack gear provided on the upper portion of the outer cylinder. A gear mechanism having a gear and its handle for moving the inner cylinder up and down by turning the handle; and a clamp mechanism that fits on the upper part of the inner cylinder and fixes the vertical movement of the inner cylinder. Lifting device for the antenna.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2668190U JPH0810963Y2 (en) | 1990-03-15 | 1990-03-15 | Aerial line lifting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2668190U JPH0810963Y2 (en) | 1990-03-15 | 1990-03-15 | Aerial line lifting device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH03117917U JPH03117917U (en) | 1991-12-05 |
| JPH0810963Y2 true JPH0810963Y2 (en) | 1996-03-29 |
Family
ID=31529561
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2668190U Expired - Lifetime JPH0810963Y2 (en) | 1990-03-15 | 1990-03-15 | Aerial line lifting device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0810963Y2 (en) |
-
1990
- 1990-03-15 JP JP2668190U patent/JPH0810963Y2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH03117917U (en) | 1991-12-05 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EXPY | Cancellation because of completion of term |