JPH045199U - - Google Patents
Info
- Publication number
- JPH045199U JPH045199U JP4560190U JP4560190U JPH045199U JP H045199 U JPH045199 U JP H045199U JP 4560190 U JP4560190 U JP 4560190U JP 4560190 U JP4560190 U JP 4560190U JP H045199 U JPH045199 U JP H045199U
- Authority
- JP
- Japan
- Prior art keywords
- pitch control
- blades
- control device
- rotary blades
- pitch
- 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
Landscapes
- Toys (AREA)
Description
第１，２図は第１実施例を示し、第１図は要部
の平面図、第２図は要部の断面図、第３図は第２
実施例の平面図、第４図は第２実施例の断面図、
第５図は第３実施例の平面図、第６図は第３実施
例の断面図である。
１……飛行体、２〜５……回転翼、７……ピツ
チコントロール装置、４１……ピツチコントロー
ル部材、４２……サーボ機構。
Figures 1 and 2 show the first embodiment, Figure 1 is a plan view of the main part, Figure 2 is a sectional view of the main part, and Figure 3 is the second embodiment.
A plan view of the embodiment, FIG. 4 is a sectional view of the second embodiment,
FIG. 5 is a plan view of the third embodiment, and FIG. 6 is a sectional view of the third embodiment. DESCRIPTION OF SYMBOLS 1... Flight object, 2-5... Rotor blade, 7... Pitch control device, 41... Pitch control member, 42... Servo mechanism.
Claims (1)
れる回転翼と、これら回転翼のブレードをフエザ
リング軸に対して、回動させるピツチコントロー
ル装置とを備えていて、 前記ピツチコントロール装置を、前記第１〜第
４回転翼のそれぞれの回転軸に昇降可能に取り付
けられていて、その昇降によりブレードのピツチ
を変化させるピツチコントロール部材と、これら
第１〜第４ピツチコントロール部材を昇降させる
サーボ機構とで構成したことを特徴とする垂直離
着陸可能な飛行体。[Claims for Utility Model Registration] The utility model is equipped with at least four or more rotary blades that are rotated at a constant ratio in a horizontal plane, and a pitch control device that rotates the blades of these rotary blades about a feathering axis, The pitch control device includes a pitch control member which is attached to the rotation shaft of each of the first to fourth rotary blades so as to be able to rise and fall, and which changes the pitch of the blades by moving the pitch control device up and down, and these first to fourth pitch control members. An aircraft capable of vertical take-off and landing, characterized by comprising a servo mechanism that raises and lowers the aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4560190U JPH045199U (en) | 1990-04-27 | 1990-04-27 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4560190U JPH045199U (en) | 1990-04-27 | 1990-04-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH045199U true JPH045199U (en) | 1992-01-17 |
Family
ID=31559929
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4560190U Pending JPH045199U (en) | 1990-04-27 | 1990-04-27 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH045199U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100812755B1 (en) * | 2006-11-13 | 2008-03-12 | 한국생산기술연구원 | Single-power controlled quadcopter |
| KR101129249B1 (en) * | 2011-11-22 | 2012-06-12 | 조금배 | A vertical takeoff and landing aircraft |
-
1990
- 1990-04-27 JP JP4560190U patent/JPH045199U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100812755B1 (en) * | 2006-11-13 | 2008-03-12 | 한국생산기술연구원 | Single-power controlled quadcopter |
| KR101129249B1 (en) * | 2011-11-22 | 2012-06-12 | 조금배 | A vertical takeoff and landing aircraft |
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