ME03099B - Longitudinally wing for airplanes - Google Patents
Longitudinally wing for airplanesInfo
- 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
Links
Landscapes
- Toys (AREA)
- 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.
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) |
-
2017
- 2017-02-08 ME MEP-2017-37A patent/ME03099B/en unknown
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112018009344A2 (en) | air vehicle with folding components | |
AR109035A1 (en) | AIRCRAFT AND AIRCRAFT WING | |
BR112015020484A2 (en) | aircraft | |
BR112016006370A2 (en) | Method for controlling the operation of an aircraft turboprop engine engine and turboprop engine control system | |
WO2009133217A8 (en) | Support-model assembly with minimum aerodynamic interference for tests in the transonic range in a wind tunnel | |
WO2017003542A3 (en) | Solar-powered aircraft | |
IL241201B (en) | Foldable wings for an unmanned air vehicle | |
ATE528705T1 (en) | IMPLEMENTATION OF CONTINUOUS LANDING APPROACHES FOR MAXIMUM AIRCRAFT PREDICTABILITY | |
BR112013020203A2 (en) | aircraft with improved aerodynamic performance | |
WO2015007259A3 (en) | Changeable wing profile | |
WO2014135948A3 (en) | Aft pylon fairing for aircraft | |
RU2014122331A (en) | SUSPENSION Pylon for gas turbine engine | |
WO2015162575A3 (en) | Aircraft galley configuration | |
WO2020003239A3 (en) | Tail sitter | |
ME03099B (en) | Longitudinally wing for airplanes | |
WO2016111715A3 (en) | Hand-launched, solar-powered aircraft | |
DE602007010125D1 (en) | AIRCRAFT WITH A DEVICE FOR REDUCING AIR RESISTANCE | |
EP3492374A3 (en) | Retrofit flight control surface | |
EA201500683A1 (en) | AERODYNAMIC DEVICE | |
PL424512A1 (en) | Multi-rotor plane, (copter) of which the movable arms and other planes create the aerodynamic lift | |
BR102018071840A8 (en) | NACELLE CONFIGURATION, METHOD TO CONTROL AIR FLOW FOR REVERSE THRUST IN A NACELLE AND AIRCRAFT ENGINE | |
RU2015149094A (en) | Application of a method of flight with asymmetric thrust for landing an aircraft in crosswind | |
ES2611024A1 (en) | Aircraft (Machine-translation by Google Translate, not legally binding) | |
RU2015135410A (en) | Helicopter vertical take-off | |
ES1271359Y (en) | AERODYNAMIC FLYING PROJECTILE |