ME03099B - Longitudinally wing for airplanes - Google Patents

Longitudinally wing for airplanes

Info

Publication number
ME03099B
ME03099B MEP-2017-37A MEP201737A ME03099B ME 03099 B ME03099 B ME 03099B ME P201737 A MEP201737 A ME P201737A ME 03099 B ME03099 B ME 03099B
Authority
ME
Montenegro
Prior art keywords
wing
longitudinal
airplane
aircraft
jet engine
Prior art date
Application number
MEP-2017-37A
Other languages
Unknown language (me)
Inventor
Zoran M Ilinčić
Original Assignee
Ilincic Zoran M
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 Ilincic Zoran M filed Critical Ilincic Zoran M
Priority to MEP-2017-37A priority Critical patent/ME03099B/en
Publication of ME03099B publication Critical patent/ME03099B/en

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  • Tires In General (AREA)

Abstract

Uzdužno krilo za  avione Ako se iza Mlaznog motora (3)  aviona  postavi Uzdužna krilo za avione (1), može se iskoristiti veliki dio  kinetičke energije gasova  koji izlaze iz Mlaznog motora (3). Konstrukcione karakteristike  Uzdužnog krila  za avione (1)  su takve da su stvoreni uslovi da na Donjoj površini uzdužnog krila  za avione (8) bude  veći pritisak nego  na Gornjoj površini uzdužnog krila za avione (7), što  rezultira pojavom sile  uzgona. To se postiže tako što  se napravi Uzdužna krilo za avione (1)  slično polovini uzdužna po osi prerezane konusne cijevi, omotača valjka ili sl. Uzdužna krilo za avioine  (1)  treba  da se na pogodan način  pričvrsti za krilo ili trup aviona  i to  iza mlaznog  motora. Da bi se poboljšala efikasnost  Uzdužnog  krila  za avione (1)  korisno je  na njega postaviti jedno ili više  Dodatnih krila  (6).Longitudinal Airplane Wing If a Longitudinal Airplane Wing (1) is located behind the Jet Engine (3), much of the kinetic energy of the gases exiting the Jet Engine (3) can be utilized. The design characteristics of the Longitudinal Wing for Airplanes (1) are such that conditions are created for the pressure on the Lower surface of the Longitudinal Wing for aircraft (8) to be greater than on the Upper surface of the Longitudinal Wing for aircraft (7), which results in a buoyancy force. This is accomplished by making the longitudinal wing of the aircraft (1) similar to half longitudinally along the axis of the slit conical tube, roller sheath or the like. The longitudinal airplane wing (1) should be conveniently attached to the airplane wing or fuselage behind the jet engine. In order to improve the efficiency of the Airplane Longitudinal Wing (1), it is useful to place one or more Extra Wings (6) on it.

MEP-2017-37A 2017-02-08 2017-02-08 Longitudinally wing for airplanes ME03099B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
MEP-2017-37A ME03099B (en) 2017-02-08 2017-02-08 Longitudinally wing for airplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
MEP-2017-37A ME03099B (en) 2017-02-08 2017-02-08 Longitudinally wing for airplanes

Publications (1)

Publication Number Publication Date
ME03099B true ME03099B (en) 2019-01-20

Family

ID=65030259

Family Applications (1)

Application Number Title Priority Date Filing Date
MEP-2017-37A ME03099B (en) 2017-02-08 2017-02-08 Longitudinally wing for airplanes

Country Status (1)

Country Link
ME (1) ME03099B (en)

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