GB2048182A - Sports aeroplane - Google Patents

Sports aeroplane

Info

Publication number
GB2048182A
GB2048182A GB8022037A GB8022037A GB2048182A GB 2048182 A GB2048182 A GB 2048182A GB 8022037 A GB8022037 A GB 8022037A GB 8022037 A GB8022037 A GB 8022037A GB 2048182 A GB2048182 A GB 2048182A
Authority
GB
United Kingdom
Prior art keywords
wing
fuselage
per cent
plane
aeroplane
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.)
Granted
Application number
GB8022037A
Other versions
GB2048182B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kondratiev V P
Viryachev J N
Yakolev A A
Original Assignee
Kondratiev V P
Viryachev J N
Yakolev A A
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.)
Filing date
Publication date
Application filed by Kondratiev V P, Viryachev J N, Yakolev A A filed Critical Kondratiev V P
Publication of GB2048182A publication Critical patent/GB2048182A/en
Application granted granted Critical
Publication of GB2048182B publication Critical patent/GB2048182B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Compounds Of Unknown Constitution (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Toys (AREA)
  • Professional, Industrial, Or Sporting Protective Garments (AREA)
  • Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
  • Feedback Control In General (AREA)

Abstract

A sports aeroplane, comprising a fuselage (1) with a propulsion system (3), an uncambered wing (5), horizontal (8) and vertical (12) tails. Wing chords (B) and chords (C) of the horizontal tails (8), as well as the thrust vector of the propulsion system (3) are situated in a plane coming through the fuselage centre line 0-0, whereas the fin of the vertical tail (12) is extended beyond the lower outline of the fuselage at a distance h2 from the plane 0-0 equal to 25-50 per cent of the height h1 of the vertical tail (12) above that plane 0-0, so that a ventral fin is formed. The symmetrical wing section has its nose radius equal to 3-5 per cent of the local wing chord (B) and its relative wing thickness equal to 15-20 per cent of the local chord (B) of the wing (5).
GB8022037A 1978-11-02 1979-09-28 Sports aeroplane Expired GB2048182B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU782681352A SU764275A1 (en) 1978-11-02 1978-11-02 Sportive airplane

Publications (2)

Publication Number Publication Date
GB2048182A true GB2048182A (en) 1980-12-10
GB2048182B GB2048182B (en) 1983-03-30

Family

ID=20792279

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8022037A Expired GB2048182B (en) 1978-11-02 1979-09-28 Sports aeroplane

Country Status (9)

Country Link
AT (1) AT370690B (en)
AU (1) AU529644B2 (en)
CS (1) CS217151B1 (en)
DD (1) DD148454A3 (en)
FR (1) FR2440872A1 (en)
GB (1) GB2048182B (en)
IT (1) IT7927025A0 (en)
SU (1) SU764275A1 (en)
WO (1) WO1980000949A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101516726B (en) * 2006-09-15 2011-11-09 波音公司 Trapezoidal panel pin joint allowing free deflection between fuselage and wing

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2452424A1 (en) * 1979-03-27 1980-10-24 Gepal IMPROVEMENTS IN THE STRUCTURE AND LAYOUT OF A CELL, PARTICULARLY FOR THE PRODUCTION OF A TRAINING AIRCRAFT
US4565470A (en) * 1982-07-12 1986-01-21 William E. Mouzavires Apparatus for hand drilling
WO1994000345A1 (en) * 1992-06-30 1994-01-06 Aktsionernoe Obschestvo 'aviatika' Sport-piloting aeroplane
RU2005662C1 (en) * 1992-06-30 1994-01-15 Акционерное общество "Авиатика" Aerobatic plane

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1981700A (en) * 1933-09-18 1934-11-20 J L Younghusband Aircraft
GB507714A (en) * 1937-08-02 1939-06-20 Dornier Werke Gmbh Improvements in or relating to aircraft
US3926389A (en) * 1972-05-24 1975-12-16 Messerschmitt Boelkow Blohm Aircraft of a controllable stability
DE2254136A1 (en) * 1972-11-04 1974-05-16 Messerschmitt Boelkow Blohm FOLDING TAIL

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101516726B (en) * 2006-09-15 2011-11-09 波音公司 Trapezoidal panel pin joint allowing free deflection between fuselage and wing

Also Published As

Publication number Publication date
AT370690B (en) 1983-04-25
ATA904379A (en) 1982-09-15
AU5262179A (en) 1980-05-08
IT7927025A0 (en) 1979-11-02
FR2440872B1 (en) 1983-10-14
GB2048182B (en) 1983-03-30
FR2440872A1 (en) 1980-06-06
DD148454A3 (en) 1981-05-27
AU529644B2 (en) 1983-06-16
SU764275A1 (en) 1982-03-30
CS217151B1 (en) 1982-12-31
WO1980000949A1 (en) 1980-05-15

Similar Documents

Publication Publication Date Title
GB2048182A (en) Sports aeroplane
GB1152982A (en) Improvements in Anti-Drag Arrangements for Aerial Bodies, or Bodies intended for Movement partly in an Aerial Medium
US2898059A (en) Fuselage shaping to reduce the strength of the initial shock wave on lifting airplane wings
GB1260831A (en) A twin-hulled vessel (catamaran) with composite hulls
SU1580737A1 (en) Swept wing
GB1151577A (en) Aircraft
GB376634A (en) Elastic seaplane undercarriages
OTTENSOSER Parametric transonic evaluation of type A VSTOL nacelle drag[Final Report, Jan.- Aug. 1977]
Siddalingappa et al. An introduction to the aerodynamics of spoilers
GB373656A (en) Improvements in and relating to rudders
GB612666A (en) Improvements in or relating to aircraft
SU1001607A1 (en) DEVICE HANGING THE LOCK ON THE PLANE'S WING
SU687730A1 (en) Aircraft wing
JPS54131300A (en) Aerodynamic moment generating rudder of aircraft
FR2278569A1 (en) Aircraft with circular wing - has elevator formed by pivotal rear segment of wing
RAND Design and analysis of single cell balloons(stress analysis of high altitude balloons)
Roskam Forward swept wings and commuter airplanes
Herrouin et al. General survey of the studies and testing techniques that led to the definition of N 500 performance
SU1367343A1 (en) PLANE WITH POWER INSTALLATIONS ON THE WING
Haglund Potential for sonic boom reduction of the Boeing HSCT
SEREBRIISKII The ground effect on the aerodynamic characteristics of an aircraft(steady horizontal flight)
LUMMUS Study of aerodynamic technology for VSTOL fighter/attack aircraft, volume 1[Final Report, 1 Nov. 1977- 31 May 1978]
SE7901512L (en) RINGFUL WINGS
PUGSLEY The Engineering Development of Rigid Airships
Shaw Experimental investigation into forward swept wings for a light-weight combat aircraft

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee