WO1980000949A1 - Avion de sport - Google Patents

Avion de sport Download PDF

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Publication number
WO1980000949A1
WO1980000949A1 PCT/SU1979/000097 SU7900097W WO8000949A1 WO 1980000949 A1 WO1980000949 A1 WO 1980000949A1 SU 7900097 W SU7900097 W SU 7900097W WO 8000949 A1 WO8000949 A1 WO 8000949A1
Authority
WO
WIPO (PCT)
Prior art keywords
κρyla
fuselage
aircraft
plane
οκοlο
Prior art date
Application number
PCT/SU1979/000097
Other languages
English (en)
Russian (ru)
Inventor
Y Viryachev
A Yakovlev
B Frolischev
V Kondratev
Original Assignee
Y Viryachev
A Yakovlev
B Frolischev
V Kondratev
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 Y Viryachev, A Yakovlev, B Frolischev, V Kondratev filed Critical Y Viryachev
Priority to DE19792953301 priority Critical patent/DE2953301A1/de
Publication of WO1980000949A1 publication Critical patent/WO1980000949A1/fr

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

Definitions

  • a well-known and efficient aircraft also has a military vertical version.
  • the area of the apartment is 15 degrees higher than the surface of the drive, and the force of the vehicle does not result in any accident.
  • a well-known plane has a tradition that doesn’t squeeze a file with a yellowspan of a large thickness, which is 9-4 degrees with a small radius of 2, compared to 5%.
  • Tseles ⁇ b ⁇ azn ⁇ , ch ⁇ by simme ⁇ ichny ⁇ sh ⁇ ⁇ yla would have ⁇ adius za ⁇ ugleniya n ⁇ s ⁇ a, ⁇ avny ⁇ ⁇ l ⁇ 3 d ⁇ ⁇ l ⁇ 5% ⁇ lichzhny mes ⁇ n ⁇ y ⁇ dy ⁇ yla and 30 ⁇ n ⁇ si ⁇ el- hydrochloric ⁇ lschinu, ⁇ a ⁇ nuyu ⁇ ⁇ l ⁇ ⁇ 5 d ⁇ ⁇ l ⁇ 20% ⁇ elichiny mes ⁇ n ⁇ y ⁇ dy ⁇ yla.
  • a proprietary aircraft made according to a consensus invention, contains a fuselage I / Fig. ⁇ /. ⁇ n ⁇ s ⁇ - v ⁇ chas ⁇ i ⁇ yuzelyazha I ⁇ i ⁇ e ⁇ len ⁇ a ⁇ g ⁇ '2 ⁇ a ⁇ m sm ⁇ n ⁇ i ⁇ vana sil ⁇ vaya us ⁇ an ⁇ v ⁇ a 3 s ⁇ de ⁇ zhaschaya us ⁇ m in case ⁇ shnev ⁇ y dviga ⁇ el, ⁇ b ⁇ znachenny ⁇ y zh ⁇ ⁇ zi- tion 3 and zhmeyuschizh any zhzves ⁇ nuyu ⁇ d ⁇ dyaschuyu for e ⁇ y ts ⁇ li ⁇ yas ⁇ u ⁇ iyu, ⁇ aya here ⁇ isyvae ⁇ sy
  • Compressor unit 3 has an air screw 4 that is designed to generate traction power, mounted on a shaft / not in use / motor 3, which is not airborne. It coincides with a solid axis of 0-0 aircraft.
  • the plane also had the arm 5, intended for the creation of amperage.
  • the booster units 5 are equipped with a simplicity of a comfortable and spacious 0-0 aircraft.
  • the ele- ments 6 / Fig. 2/ are located; Chapter 5 has a ⁇ -shaped form in the plan, as shown in figure 2.
  • Arrow 5 has a zero angle and is set to a positive integral 0-0 plane and a zero angle V is a result of this, that is, all the costs of the installation are 5
  • the city center 8 has a special shape in the plan, as shown in figure 2, and is made up of a 9-inch, 10-height, 2-stage, 2-wheel drive
  • the external version 12 is from keel 13 / fig. the well-known constituency and the rule of the 14th.
  • the sympathetic design of the sprinkler 5 has a radius / figure 3/7 for pickling the nose, equal to 3 to 5, the value of the local area is 5.
  • the symmetrical range of the coil 5 has * a similarly large thickness, a significant difference of 15 to about 20% of the value of the local cycle 5.
  • Fig. 4 the dependency is shown .
  • the patient is £ -. ground power of the angle ⁇ of the attack.
  • ⁇ se e ⁇ is ⁇ lyuchae ⁇ v ⁇ znzh ⁇ n ⁇ venzhe in ⁇ yam ⁇ m and ⁇ e ⁇ eve ⁇ - nu ⁇ m ⁇ le ⁇ e, ⁇ i vy ⁇ lnenzhi ⁇ igu ⁇ * ⁇ yam ⁇ g ⁇ and ⁇ b ⁇ a ⁇ n ⁇ g ⁇ ⁇ il ⁇ azha, nesimm ⁇ ichny ⁇ ae ⁇ dinamichee ⁇ i ⁇ m ⁇ men ⁇ v, zhlzh m ⁇ men ⁇ v, s ⁇ zdavaemy ⁇ sil ⁇ y ⁇ yagzh sil ⁇ v ⁇ y us ⁇ an ⁇ v ⁇ i 3 ⁇ ebz ⁇ schi ⁇ nesimme ⁇ zhchn ⁇ g ⁇ ⁇ l ⁇ neniya ⁇ ulya 10 vys ⁇ y for zh ⁇ u ⁇ avya ⁇ veshzhvanzhya ⁇ zh vy ⁇ lnenzhzh ⁇ igu ⁇
  • FIG. 5 it is shown that an airplane made according to the present invention has a higher emi- tive power of 6, especially due to the fact that there is a lot of angle *.
  • a wide range of angles ⁇ _ ⁇ is not sufficient for a maneuverable, efficient aircraft.
  • FIG. 6 it is shown that the airplane made according to the invention has a higher er- • • ative pressure, especially at a safe time.
  • the non-existent coefficient of the problem of the traveling airport is 25 garbage, which constitutes a risk of the loss of peace, of the issue of the problem, of the problem, yz FIG. 6 that, in the case of the submitter, 30 are in accordance with the present invention, it is of a higher value, as compared with the well-known fact that it is generally accepted.
  • FIG. 8 This is shown in FIG. 8 for an airplane made with a vowel of the present invention, city 8, “0.” ⁇ g ⁇ ⁇ as ⁇ l ⁇ zheny in ' ⁇ dn ⁇ y ⁇ l ⁇ s ⁇ s ⁇ i 0 ⁇ with ⁇ dami ⁇ yla 5 on b ⁇ ly ⁇ i ⁇ ugla ⁇ ⁇ X a ⁇ a ⁇ i not ⁇ dae ⁇ in z ⁇ nu v ⁇ zdushn ⁇ g ⁇ ⁇ a, zavi ⁇ enn ⁇ g ⁇ ⁇ yl ⁇ m 5.
  • a fast-flying aircraft made according to the current winches presses a short-circuit with the radio
  • ⁇ nazhz ⁇ g ⁇ ammy s ⁇ v ⁇ emenny ⁇ s ⁇ evn ⁇ vanny ⁇ by higher mu ⁇ nl ⁇ azhu ⁇ azyvae ⁇ , ch ⁇ s ⁇ ivny sam ⁇ le ⁇ , vy ⁇ l- nenny s ⁇ glasn ⁇ nas ⁇ yaschemu nz ⁇ b ⁇ e ⁇ eyaigo, bude ⁇ 'ime ⁇ non-small ⁇ eimusches ⁇ va over sam ⁇ le ⁇ ash izves ⁇ ny ⁇ ae ⁇ dinash- ches ⁇ i ⁇ s ⁇ em.
  • the damnable invention may also be used in the 5th van and the use of other types of light aircraft, namely, passenger and rural vehicles.

Landscapes

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

Abstract

Un avion de sport comprend un fuselage (1) avec un systeme de propulsion (3), une aile a profil non cambre (5), des empennages horizontaux (8) et verticaux (12). Les profondeurs d'aile (B) et les lignes de corde des empennages horizontaux (8), ainsi que le vecteur de poussee du systeme de propulsion (3) sont situes dans un plan passant par la ligne mediane du fuselage (O-O), tandis que la derive de l'empennage vertical (12) s'etend au-dela du pourtour inferieur du fuselage a une distance H2 du plan (O-O) egal a 25-50% de la hauteur hl de l'empennage vertical (12) au-dessus du plan (O-O), formant ainsi une derive ventrale. La section d'aile symetrique possede un rayon de bord d'attaque r egal a 3-5% de la profondeur d'aile locale (B) et son epaisseur d'aile correspondante est egale a 15-20% de la profondeur locale (B) de l'aile (5).
PCT/SU1979/000097 1978-11-02 1979-09-28 Avion de sport WO1980000949A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19792953301 DE2953301A1 (de) 1978-11-02 1979-09-28 Sports aeroplane

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SU2681352 1978-11-02
SU782681352A SU764275A1 (en) 1978-11-02 1978-11-02 Sportive airplane

Publications (1)

Publication Number Publication Date
WO1980000949A1 true WO1980000949A1 (fr) 1980-05-15

Family

ID=20792279

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SU1979/000097 WO1980000949A1 (fr) 1978-11-02 1979-09-28 Avion de sport

Country Status (9)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4565470A (en) * 1982-07-12 1986-01-21 William E. Mouzavires Apparatus for hand drilling

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2452424A1 (fr) * 1979-03-27 1980-10-24 Gepal Perfectionnements apportes dans la structure et l'amenagement d'une cellule, notamment pour la realisation d'un avion d'entrainement
RU2005662C1 (ru) * 1992-06-30 1994-01-15 Акционерное общество "Авиатика" Спортивно-пилотажный самолет
WO1994000345A1 (fr) * 1992-06-30 1994-01-06 Aktsionernoe Obschestvo 'aviatika' Avion de pilotage sportif
US7546979B1 (en) * 2006-09-15 2009-06-16 The Boeing Company Trapezoidal panel pin joint allowing free deflection between fuselage and wing

Citations (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
DE2254136A1 (de) * 1972-11-04 1974-05-16 Messerschmitt Boelkow Blohm Klappleitwerk
US3926389A (en) * 1972-05-24 1975-12-16 Messerschmitt Boelkow Blohm Aircraft of a controllable stability

Patent Citations (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 (de) * 1972-11-04 1974-05-16 Messerschmitt Boelkow Blohm Klappleitwerk

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4565470A (en) * 1982-07-12 1986-01-21 William E. Mouzavires Apparatus for hand drilling

Also Published As

Publication number Publication date
DD148454A3 (de) 1981-05-27
ATA904379A (de) 1982-09-15
GB2048182B (en) 1983-03-30
GB2048182A (en) 1980-12-10
AU529644B2 (en) 1983-06-16
FR2440872A1 (fr) 1980-06-06
FR2440872B1 (fr) 1983-10-14
CS217151B1 (en) 1982-12-31
AT370690B (de) 1983-04-25
IT7927025A0 (it) 1979-11-02
SU764275A1 (en) 1982-03-30
AU5262179A (en) 1980-05-08

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