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)
• Toys (AREA)
• Professional, Industrial, Or Sporting Protective Garments (AREA)
• Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
• Compounds Of Unknown Constitution (AREA)
• Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
• Feedback Control In General (AREA)

Priority Applications (1)

Applications Claiming Priority (2)

Publications (1)

Family

ID=20792279

Family Applications (1)

Country Status (9)

Cited By (1)

Families Citing this family (4)

Citations (4)

• 1978
  • 1978-11-02 SU SU782681352A patent/SU764275A1/ru active
• 1979
  • 1979-09-28 WO PCT/SU1979/000097 patent/WO1980000949A1/ru unknown
  • 1979-09-28 AT AT0904379A patent/AT370690B/de not_active IP Right Cessation
  • 1979-09-28 GB GB8022037A patent/GB2048182B/en not_active Expired
  • 1979-10-24 CS CS797271A patent/CS217151B1/cs unknown
  • 1979-10-31 FR FR7927053A patent/FR2440872A1/fr active Granted
  • 1979-11-01 DD DD79216654A patent/DD148454A3/de not_active IP Right Cessation
  • 1979-11-02 IT IT7927025A patent/IT7927025A0/it unknown
  • 1979-11-08 AU AU52621/79A patent/AU529644B2/en not_active Ceased

Patent Citations (4)

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