SE7414920L - - Google Patents

Info

Publication number: SE7414920L
Authority: SE; Sweden

Application number

SE7414920A

Inventor

A Mederer

Original Assignee

Messerschmitt Boelkow Blohm

Priority date (The priority date 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 date listed.)

1973-12-13

Filing date

1974-11-28

Publication date

1975-06-16

1973-12-13 Priority claimed from DE19732361888 external-priority patent/DE2361888C3/en

1974-11-28 Application filed by Messerschmitt Boelkow Blohm filed Critical Messerschmitt Boelkow Blohm

1975-06-16 Publication of SE7414920L publication Critical patent/SE7414920L/xx

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)

SE7414920A 1973-12-13 1974-11-28 SE7414920L (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
DE19732361888 DE2361888C3 (en)		1973-12-13	Control and stabilization device for an aircraft with artificial stability

Publications (1)

Publication Number	Publication Date
SE7414920L true SE7414920L (en)	1975-06-16

Family

ID=5900576

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
SE7414920A SE7414920L (en)	1973-12-13	1974-11-28

Country Status (2)

Country	Link
FR (1)	FR2254481A1 (en)
SE (1)	SE7414920L (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
IT1152763B (en) *	1982-01-25	1987-01-14	Ind Aeronautiche E Meccaniche	IMPROVED AIRCRAFT
US4723214A (en) *	1985-02-15	1988-02-02	Grumman Aerospace Corporation	Automatic camber control
CN109598025B (en) *	2018-11-02	2023-05-26	中国航空工业集团公司西安飞机设计研究所	Optimal design method for inclination angle and area of V-shaped tail wing
CN110395389A (en) *	2019-06-28	2019-11-01	中国航天空气动力技术研究院	A kind of aerodynamic arrangement improving the horizontal side-coupled characteristic of hypersonic aircraft

1974
- 1974-11-28 SE SE7414920A patent/SE7414920L/xx unknown
- 1974-12-11 FR FR7440848A patent/FR2254481A1/en not_active Withdrawn

Also Published As

Publication number	Publication date
FR2254481A1 (en)	1975-07-11
DE2361888B2 (en)	1976-06-10
DE2361888A1 (en)	1975-06-19

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