FR2254481A1 - Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged - Google Patents
Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arrangedInfo
- Publication number
- FR2254481A1 FR2254481A1 FR7440848A FR7440848A FR2254481A1 FR 2254481 A1 FR2254481 A1 FR 2254481A1 FR 7440848 A FR7440848 A FR 7440848A FR 7440848 A FR7440848 A FR 7440848A FR 2254481 A1 FR2254481 A1 FR 2254481A1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- canards
- dihedrally
- fins
- anhedrally
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Mechanical Control Devices (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19732361888 DE2361888C3 (de) | 1973-12-13 | Steuer- und Stabilisierungseinrichtung für ein Flugzeug künstlicher Stabilität |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2254481A1 true FR2254481A1 (en) | 1975-07-11 |
Family
ID=5900576
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7440848A Withdrawn FR2254481A1 (en) | 1973-12-13 | 1974-12-11 | Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2254481A1 (enrdf_load_stackoverflow) |
SE (1) | SE7414920L (enrdf_load_stackoverflow) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0084686A3 (en) * | 1982-01-25 | 1984-05-30 | Piaggio Rinaldo Ind Aeronaut | Improved aircraft |
EP0193442A1 (en) * | 1985-02-15 | 1986-09-03 | Grumman Aerospace Corporation | Automatic camber control |
CN109598025A (zh) * | 2018-11-02 | 2019-04-09 | 中国航空工业集团公司西安飞机设计研究所 | 一种v形尾翼倾角与面积优化设计方法 |
CN110395389A (zh) * | 2019-06-28 | 2019-11-01 | 中国航天空气动力技术研究院 | 一种改善高超声速飞行器横侧向耦合特性的气动布局 |
-
1974
- 1974-11-28 SE SE7414920A patent/SE7414920L/xx unknown
- 1974-12-11 FR FR7440848A patent/FR2254481A1/fr not_active Withdrawn
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0084686A3 (en) * | 1982-01-25 | 1984-05-30 | Piaggio Rinaldo Ind Aeronaut | Improved aircraft |
EP0193442A1 (en) * | 1985-02-15 | 1986-09-03 | Grumman Aerospace Corporation | Automatic camber control |
CN109598025A (zh) * | 2018-11-02 | 2019-04-09 | 中国航空工业集团公司西安飞机设计研究所 | 一种v形尾翼倾角与面积优化设计方法 |
CN110395389A (zh) * | 2019-06-28 | 2019-11-01 | 中国航天空气动力技术研究院 | 一种改善高超声速飞行器横侧向耦合特性的气动布局 |
Also Published As
Publication number | Publication date |
---|---|
DE2361888B2 (de) | 1976-06-10 |
DE2361888A1 (de) | 1975-06-19 |
SE7414920L (enrdf_load_stackoverflow) | 1975-06-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4466586A (en) | Directional control device for aircraft | |
US3883094A (en) | Foldable canard assembly | |
NO145314C (no) | Mateanordning for roer eller liknende, saerlig en roerstreng som skal inn eller ut av en broenn | |
GB1153747A (en) | Toy Airplane with Folding Wings | |
FR2254481A1 (en) | Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged | |
GB1080322A (en) | Tailless kite | |
GB1024103A (en) | Aircraft with flexible wings | |
GB1086044A (en) | Kites | |
GB1112924A (en) | Improvements in or relating to aircraft | |
GB582206A (en) | Improvements in tailless airplanes | |
US1767966A (en) | Wing system with stabilizing vanes for aircraft | |
GB987792A (en) | Improvements in and relating to aircraft wings | |
Spearman et al. | Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3 | |
GB1220055A (en) | Fixed wing aeroplanes | |
GB595464A (en) | Improvements in aeroplanes | |
GB628684A (en) | Improvements in aircraft control surfaces | |
CN207129132U (zh) | 旋翼机稳定舵半水滴状机构 | |
GB741720A (en) | Improvements in aeroplanes | |
US1405890A (en) | Aerofoil arrangement for aircraft | |
GB1169880A (en) | Aircraft having Means to Counteract Displacement of the Aerodynamic Centre | |
Staudacher et al. | Aerodynamic characteristics of a fighter-type configuration during and beyond stall | |
SPENCER | Canard aircraft with split flaps ahead of the wing trailing edge and flaps on the leading and trailing edges of the canard control at low speed | |
GB1417653A (en) | Aircraft | |
CZARNECKI | Spanwise loadings and aerodynamic characteristics for a series of trailing- edge controls on a 40 deg sweptback wing at Mach numbers of 1. 61 and 2. 01(Spanwise loadings and aerodynamic characteristics for trailing-edge controls on 40 deg sweptback wing at Mach numbers 1. 61 and 2. 01) | |
FR2272893A1 (en) | Powered aircraft with small front wing - has freely rotating tabs on front wing forming elevators |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |