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.)
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for DefencefiledCriticalUK Secretary of State for Defence
Publication of DE1556790A1publicationCriticalpatent/DE1556790A1/en
Application grantedgrantedCritical
Publication of DE1556790C3publicationCriticalpatent/DE1556790C3/en
B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
B64D27/02—Aircraft characterised by the type or position of power plants
B64D27/16—Aircraft characterised by the type or position of power plants of jet type
B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
B64D27/02—Aircraft characterised by the type or position of power plants
B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
Landscapes
Engineering & Computer Science
(AREA)
Aviation & Aerospace Engineering
(AREA)
Structures Of Non-Positive Displacement Pumps
(AREA)
Turbine Rotor Nozzle Sealing
(AREA)
Toys
(AREA)
Description
Hierzu 1 Blatt Zeichnungen1 sheet of drawings
Claims (1)
Patentanspruch:Claim:Flugzeug mit an den Tragflügeln montierten Triebwerken, dadurch gekennzeichnet,
daß zwischen den Triebwerken (19) und dem Flugzeugrumpf (12) Lärmblenden (32) auf den
Tragflügeln (14; 16) errichtet sind.Airplane with engines mounted on the wings, characterized in that
that between the engines (19) and the aircraft fuselage (12) noise screens (32) on the
Hydrofoils (14; 16) are erected.
DE1556790A1967-03-181968-03-18
Airplane with engines mounted on the wings
ExpiredDE1556790C3
(en)
The soviet Tu-144 civil supersonic transport(Soviet supersonic transport Tu 144, describing wing unit, fuselage, passenger accommodation, tail unit, landing gear, power unit engine nacelle and navigation)
The dynamic simulation of turbulence penetration(Jet transport aircraft accidents resulting from atmospheric turbulence, and dynamic simulation of turbulence penetration)
Laminar flow control and the x-21(Aerodynamic, propulsive, structural and maintenance aspects of laminar flow control, and application to x-21 a aircraft, noting wing design)
Qualification of a HFB-320 Hansa and a Piaggio P 149 D for inflight simulation for the approach of a combat aircraft with high wing loading(Inflight simulation with high wing loading fighter aircraft approach using HFB-320 and Piaggio aircraft)
The XV-4 B- New generation of VTOL(XV-4 B vertical lift aircraft with lift engines noting stability, control, structural design, flight control system, etc)
Sonic boom flight research- Some effects of airplane operations and the atmosphere on sonic boom signatures(Sonic boom flight research- effects of aircraft operations and atmosphere on sonic boom signatures)
The c-142 role in coin air mobile operations(C-142 high-wing aircraft with four turboshaft engines and tilt-wing deflected slipstream to attain V/STOL capability in COIN operations)
Summary of design considerations for airplane spin-recovery parachute systems(Design and development of spin-recovery parachute systems for military aircraft and compilation of design criteria)
Investigation of side forces on ogive-cylinder bodies at high angles of attack in the M equals 0. 5 to 1. 1 range(Side forces on ogive cylinder bodies at large incidence as function of Mach number, nose fineness and bluntness ratios for laminar and turbulent boundary layers)
Favorable interference effects on maximum lift-drag ratios of half-cone delta-wing configurations at mach 6. 86(Investigation of half-cone delta wing configurations under laminar boundary layer conditions at Mach 6. 86 to determine favorable interference effects on maximum lift-drag ratio)
STOL performance emphasized in aircraft design with special references to Japanese contribution(Improving STOL aircraft performance, examining Japanese experiments on modified SAAB Safir single-engined monoplane, experimental flying boat and lightweight turbojet engines)