JPH0370698A - 頭部回転式高性能飛行機 - Google Patents
頭部回転式高性能飛行機Info
- Publication number
- JPH0370698A JPH0370698A JP20888689A JP20888689A JPH0370698A JP H0370698 A JPH0370698 A JP H0370698A JP 20888689 A JP20888689 A JP 20888689A JP 20888689 A JP20888689 A JP 20888689A JP H0370698 A JPH0370698 A JP H0370698A
- Authority
- JP
- Japan
- Prior art keywords
- high speed
- fins
- fin
- fuselage
- airplane
- 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
- 239000003381 stabilizer Substances 0.000 abstract 3
- 230000000694 effects Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
Landscapes
- Toys (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
め要約のデータは記録されません。
Description
【発明の詳細な説明】
（産業上の利用分野）
飛行機産業
（従来の技術）
請求項（１）ジェット機、プロペラ機等であった（２）
従来は縦翼は飛行機の後部に ついていた． （発明が解決しようとする課題） 高性能飛行機の作製を計る （課題を解決するための手段） 飛行機の胴体の前頭部にフィンを設けてその前頭部を高
回転させることにより、フィンが高回転し推進力を得る
ことが出来る．フィンは空気を強制に後方に流す様に曲
線にしフィン自体は回転方向に対して空気を受ける方向
に斜め向きに取り付けフィンの内側は湾曲にする．また
、縦翼を胴体の前部に設けてフィンの風圧をも受けるこ
とにより小回転が可能となる様にする （発明の効果・作用） ・高速で飛行飛行出来る様になる ・小回転が出来る様になる ・安全性の向上 ・軽量化 （実施例）
従来は縦翼は飛行機の後部に ついていた． （発明が解決しようとする課題） 高性能飛行機の作製を計る （課題を解決するための手段） 飛行機の胴体の前頭部にフィンを設けてその前頭部を高
回転させることにより、フィンが高回転し推進力を得る
ことが出来る．フィンは空気を強制に後方に流す様に曲
線にしフィン自体は回転方向に対して空気を受ける方向
に斜め向きに取り付けフィンの内側は湾曲にする．また
、縦翼を胴体の前部に設けてフィンの風圧をも受けるこ
とにより小回転が可能となる様にする （発明の効果・作用） ・高速で飛行飛行出来る様になる ・小回転が出来る様になる ・安全性の向上 ・軽量化 （実施例）
簡単な図面で説明致します
第１図は高回転フィン部と縦翼の位置を表した図である
Claims (1)
- 【特許請求の範囲】 請求項 （１）飛行機の胴体の前頭部にフィンを設けてそのフィ
ンのついた部分を高回転させて高速飛行出来る様にする （２）従来の後部の縦翼を飛行機の前部に設けてフィン
の風圧も利用してこまわりがきく様にする
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20888689A JPH0370698A (ja) | 1989-08-11 | 1989-08-11 | 頭部回転式高性能飛行機 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20888689A JPH0370698A (ja) | 1989-08-11 | 1989-08-11 | 頭部回転式高性能飛行機 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0370698A true JPH0370698A (ja) | 1991-03-26 |
Family
ID=16563750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP20888689A Pending JPH0370698A (ja) | 1989-08-11 | 1989-08-11 | 頭部回転式高性能飛行機 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0370698A (ja) |
Cited By (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100959982B1 (ko) * | 2004-05-19 | 2010-05-27 | 주식회사 엘지화학 | 전지용 안전 소자 및 이를 구비한 전지 |
| WO2011065444A1 (ja) | 2009-11-27 | 2011-06-03 | 学校法人東海大学 | 抗血栓剤 |
| JP2016501761A (ja) * | 2012-10-23 | 2016-01-21 | ゼネラル・エレクトリック・カンパニイ | アンダクテッド推力発生システムのアーキテクチャ |
| US11492918B1 (en) | 2021-09-03 | 2022-11-08 | General Electric Company | Gas turbine engine with third stream |
| US11680530B1 (en) | 2022-04-27 | 2023-06-20 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
| US11819482B2 (en) | 2017-08-29 | 2023-11-21 | Conrig Pharma Aps | Composition comprising suplatast tosilate |
| US11834995B2 (en) | 2022-03-29 | 2023-12-05 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
| US11834992B2 (en) | 2022-04-27 | 2023-12-05 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
| US11834954B2 (en) | 2022-04-11 | 2023-12-05 | General Electric Company | Gas turbine engine with third stream |
| US12031504B2 (en) | 2022-08-02 | 2024-07-09 | General Electric Company | Gas turbine engine with third stream |
| US12060829B2 (en) | 2022-04-27 | 2024-08-13 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
| US12065989B2 (en) | 2022-04-11 | 2024-08-20 | General Electric Company | Gas turbine engine with third stream |
| US12071896B2 (en) | 2022-03-29 | 2024-08-27 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
| US12366204B2 (en) | 2022-04-27 | 2025-07-22 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
| US12410763B2 (en) | 2022-08-02 | 2025-09-09 | General Electric Company | Gas turbine engine with third stream |
| US12421917B2 (en) | 2022-08-02 | 2025-09-23 | General Electric Company | Gas turbine engine with third stream |
| US12486817B2 (en) | 2022-08-02 | 2025-12-02 | General Electric Company | Gas turbine engine with third stream |
| US12516647B2 (en) | 2022-08-02 | 2026-01-06 | General Electric Company | Gas turbine engine with third stream |
| US12560132B2 (en) | 2022-08-02 | 2026-02-24 | General Electric Company | Gas turbine engine with third stream |
| US12565866B2 (en) | 2022-08-02 | 2026-03-03 | General Electric Company | Gas turbine engine with third stream |
| US12571358B2 (en) | 2022-08-02 | 2026-03-10 | General Electric Company | Gas turbine engine with third stream |
| US12571360B2 (en) | 2021-04-14 | 2026-03-10 | General Electric Deutschland Holding Gmbh | Three-stream gas turbine engine with embedded electric machine |
| US12577925B2 (en) | 2022-08-02 | 2026-03-17 | General Electric Company | Gas turbine engine with third stream |
| US12577926B2 (en) | 2022-08-02 | 2026-03-17 | General Electric Company | Gas turbine engine |
| US12618384B2 (en) | 2025-01-10 | 2026-05-05 | General Electric Company | Gas turbine engine having a bypass passage, a fan duct, and a core duct |
-
1989
- 1989-08-11 JP JP20888689A patent/JPH0370698A/ja active Pending
Cited By (29)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100959982B1 (ko) * | 2004-05-19 | 2010-05-27 | 주식회사 엘지화학 | 전지용 안전 소자 및 이를 구비한 전지 |
| WO2011065444A1 (ja) | 2009-11-27 | 2011-06-03 | 学校法人東海大学 | 抗血栓剤 |
| US11988099B2 (en) | 2012-10-23 | 2024-05-21 | General Electric Company | Unducted thrust producing system architecture |
| JP2016501761A (ja) * | 2012-10-23 | 2016-01-21 | ゼネラル・エレクトリック・カンパニイ | アンダクテッド推力発生システムのアーキテクチャ |
| US10704410B2 (en) | 2012-10-23 | 2020-07-07 | General Electric Company | Unducted thrust producing system architecture |
| US11819482B2 (en) | 2017-08-29 | 2023-11-21 | Conrig Pharma Aps | Composition comprising suplatast tosilate |
| US12571360B2 (en) | 2021-04-14 | 2026-03-10 | General Electric Deutschland Holding Gmbh | Three-stream gas turbine engine with embedded electric machine |
| US11492918B1 (en) | 2021-09-03 | 2022-11-08 | General Electric Company | Gas turbine engine with third stream |
| US11859516B2 (en) | 2021-09-03 | 2024-01-02 | General Electric Company | Gas turbine engine with third stream |
| US11834995B2 (en) | 2022-03-29 | 2023-12-05 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
| US12071896B2 (en) | 2022-03-29 | 2024-08-27 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
| US12065989B2 (en) | 2022-04-11 | 2024-08-20 | General Electric Company | Gas turbine engine with third stream |
| US11834954B2 (en) | 2022-04-11 | 2023-12-05 | General Electric Company | Gas turbine engine with third stream |
| US11680530B1 (en) | 2022-04-27 | 2023-06-20 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
| US12060829B2 (en) | 2022-04-27 | 2024-08-13 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
| US11834992B2 (en) | 2022-04-27 | 2023-12-05 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
| US12366204B2 (en) | 2022-04-27 | 2025-07-22 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
| US12516647B2 (en) | 2022-08-02 | 2026-01-06 | General Electric Company | Gas turbine engine with third stream |
| US12421917B2 (en) | 2022-08-02 | 2025-09-23 | General Electric Company | Gas turbine engine with third stream |
| US12486817B2 (en) | 2022-08-02 | 2025-12-02 | General Electric Company | Gas turbine engine with third stream |
| US12031504B2 (en) | 2022-08-02 | 2024-07-09 | General Electric Company | Gas turbine engine with third stream |
| US12523188B2 (en) | 2022-08-02 | 2026-01-13 | General Electric Company | Gas turbine engine with third stream |
| US12560132B2 (en) | 2022-08-02 | 2026-02-24 | General Electric Company | Gas turbine engine with third stream |
| US12565866B2 (en) | 2022-08-02 | 2026-03-03 | General Electric Company | Gas turbine engine with third stream |
| US12571358B2 (en) | 2022-08-02 | 2026-03-10 | General Electric Company | Gas turbine engine with third stream |
| US12410763B2 (en) | 2022-08-02 | 2025-09-09 | General Electric Company | Gas turbine engine with third stream |
| US12577925B2 (en) | 2022-08-02 | 2026-03-17 | General Electric Company | Gas turbine engine with third stream |
| US12577926B2 (en) | 2022-08-02 | 2026-03-17 | General Electric Company | Gas turbine engine |
| US12618384B2 (en) | 2025-01-10 | 2026-05-05 | General Electric Company | Gas turbine engine having a bypass passage, a fan duct, and a core duct |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPH0370698A (ja) | 頭部回転式高性能飛行機 | |
| US11577827B2 (en) | YAW-enhancing attitude control system for VTOL fixed-wing aircraft | |
| US6669137B1 (en) | Air vehicle having rotor/scissors wing | |
| US7530787B2 (en) | Rotor hub fairing system for a counter-rotating, coaxial rotor system | |
| JP6158459B2 (ja) | マルチコプター | |
| US20030062442A1 (en) | VTOL personal aircraft | |
| CN108082466A (zh) | 一种倾转涵道连接翼布局垂直起降飞行器 | |
| GB1427802A (en) | Aircraft | |
| CN221294109U (zh) | 垂直起降飞行器 | |
| US3410506A (en) | Extensible rotor airplane | |
| CN108045572A (zh) | 一种横列式复合推力高速直升机 | |
| EP3914513B1 (en) | Aircraft | |
| US20210331792A1 (en) | Rotatable nacelle for centrifugal fan on aircraft | |
| US20230382521A1 (en) | Structural features of vertical take-off and landing (vtol) aerial vehicle | |
| CN109229360A (zh) | 剪刀式双旋翼跷跷板式自转旋翼机 | |
| CN216994842U (zh) | 一种垂直起降飞行器 | |
| US3820743A (en) | Vtol air and space craft | |
| US11858622B2 (en) | Aircraft | |
| CN216994843U (zh) | 一种垂直起降飞行器 | |
| CN207417148U (zh) | 一种基于倾转涵道的单升力涵道垂直起降飞机 | |
| JPH03292294A (ja) | 垂直離着陸航空機 | |
| US20120111997A1 (en) | Rotorcraft empennage | |
| US3343768A (en) | Aircraft | |
| CN111532426A (zh) | 一种v型尾翼多旋翼垂直起降布局的飞行器 | |
| JPH0382699A (ja) | 小形垂直離着陸航空機 |