JPH0437837Y2 - - Google Patents
Info
- Publication number
- JPH0437837Y2 JPH0437837Y2 JP291287U JP291287U JPH0437837Y2 JP H0437837 Y2 JPH0437837 Y2 JP H0437837Y2 JP 291287 U JP291287 U JP 291287U JP 291287 U JP291287 U JP 291287U JP H0437837 Y2 JPH0437837 Y2 JP H0437837Y2
- Authority
- JP
- Japan
- Prior art keywords
- horizontal stabilizer
- flap
- movable member
- aircraft
- main wing
- 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
- 239000003381 stabilizer Substances 0.000 claims description 32
- 238000010586 diagram Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Landscapes
- Transmission Devices (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP291287U JPH0437837Y2 (enExample) | 1987-01-14 | 1987-01-14 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP291287U JPH0437837Y2 (enExample) | 1987-01-14 | 1987-01-14 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63111394U JPS63111394U (enExample) | 1988-07-18 |
| JPH0437837Y2 true JPH0437837Y2 (enExample) | 1992-09-04 |
Family
ID=30782193
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP291287U Expired JPH0437837Y2 (enExample) | 1987-01-14 | 1987-01-14 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0437837Y2 (enExample) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2017047898A (ja) * | 2016-08-31 | 2017-03-09 | 元延 深瀬 | エンジンの後方部に揚力板機構を設けたジェット飛行機。 |
-
1987
- 1987-01-14 JP JP291287U patent/JPH0437837Y2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63111394U (enExample) | 1988-07-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP3213752B2 (ja) | ティルト回転翼用フラッペロン・システム | |
| US2938680A (en) | Multiple position airfoil slat | |
| US3486720A (en) | Continuous slot forming leading edge slats for cranked wings | |
| US7992826B2 (en) | Leading edge flap method | |
| JPH04503495A (ja) | ティルト回転翼用フラッペロン・システム | |
| US4444368A (en) | Slotted variable camber flap | |
| RU2405715C2 (ru) | Поверхность управления задней кромкой крыла самолета | |
| CN107472511A (zh) | 基于扰流板和后缘舵面配合的飞翼布局飞机的气动舵面 | |
| WO1995011159A1 (en) | Aircraft flight control system | |
| CN106114847B (zh) | 一种垂直起降飞行器 | |
| CN110294102A (zh) | 一体式襟副翼的复合运动机构 | |
| JPH0437837Y2 (enExample) | ||
| US4890803A (en) | Airfoil with fixed and variable upper camber portions | |
| EP0052240B1 (en) | Actuation system for a control surface of an aircraft | |
| CN110422313B (zh) | 一种具有折叠机翼的飞行器 | |
| CN206265289U (zh) | 一种飞机俯仰、侧翻、偏航控制系统 | |
| RU2070144C1 (ru) | Высокоманевренный самолет | |
| GB1100376A (en) | Improvements in aircraft | |
| JP4623597B2 (ja) | 飛行機 | |
| US3260477A (en) | Flap assembly for aircraft | |
| JPH0338080Y2 (enExample) | ||
| US12371151B2 (en) | Flight control surface | |
| CN221234056U (zh) | 一种直升机的全动翼机构 | |
| CN219134487U (zh) | 一种可伸缩t型尾翼 | |
| JPH03118897U (enExample) |