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1. (WO1989000130) PROTECTIVE SYSTEM FOR REDUCING THE NOISE OF HIGH-VELOCITY JET STREAMS FROM INBUILT POWER UNITS IN AIRCRAFT
Latest bibliographic data on file with the International Bureau
Pub. No.: WO/1989/000130 International Application No.: PCT/DE1988/000409
Publication Date: 12.01.1989 International Filing Date: 01.07.1988
IPC:
B64F 1/26 (2006.01) ,E04B 1/82 (2006.01) ,E06B 3/01 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
F
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS
1
Ground or aircraft-carrier-deck installations
26
for reducing engine or jet noise; Protecting airports from jet erosion
E FIXED CONSTRUCTIONS
04
BUILDING
B
GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
1
Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
62
Insulation or other protection; Elements or use of specified material therefor
74
Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
82
specifically with respect to sound only
E FIXED CONSTRUCTIONS
06
DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS, IN GENERAL; LADDERS
B
FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES, OR LIKE ENCLOSURES, IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
3
Window sashes, door leaves, or like elements for closing openings; Layout of fixed or moving closures, e.g. windows; Features of rigidly-mounted outer frames relating to the mounting of wing frames
01
Removable or disappearing walls for hangars or other halls, e.g. for aircraft
Applicants:
RHEINHOLD & MAHLA GMBH [DE/DE]; Gneisenaustr. 15 D-8000 München, DE (AllExceptUS)
SCHAFHAUPT, Horst [DE/DE]; DE (UsOnly)
Inventors:
SCHAFHAUPT, Horst; DE
Agent:
SEIBERT, Rudolf; Tattenbachstr. 9 D-8000 München 22, DE
Priority Data:
P 37 22 112.403.07.1987DE
Title (EN) PROTECTIVE SYSTEM FOR REDUCING THE NOISE OF HIGH-VELOCITY JET STREAMS FROM INBUILT POWER UNITS IN AIRCRAFT
(FR) DISPOSITIF PROTECTEUR AMORTISSEUR DES BRUITS DE PROPULSEURS INCORPORES D'AVIONS PRODUISANT DES COURANTS DE GAZ DE HAUTE VITESSE
Abstract:
(EN) In a protective system for reducing the noise of high-velocity jet streams, in particular for aircraft power units, an inclined lattice-type conducting element is installed at a distance from the power units and an approximately horseshoe-shaped noise-absorbing wall whose height is approximately twice that of the conducting element is arranged behind the conducting element. To prevent the radiation of suction noise from the power unit towards the front, two swivelling door wings (16, 17) lined with sound-absorbing material (22, 23) are hinged to the outer front edges (14, 15) of the free sides (8, 9) of the horseshoe-shaped sound-absorbing wall. The door wings can swivel inwards through approximately 60° and their length is such that in the fully swivelled state they leave a gap (a) for the nose of an aircraft (1).
(FR) Un dispositif protecteur amortisseur du bruit produit par des courants de gaz s'écoulant à des vitesses élevées, notament pour propulseurs d'avions, comprend un élément de guidage incliné en forme de grille disposé à une certaine distance des propulseurs. Derrière cet élément de guidage est agencée une paroi d'insonorisation ayant approximativement la forme d'un fer-à-cheval et environ deux fois la hauteur de l'élément de guidage. Afin d'empêcher les bruits d'aspiration produits par les propulseurs de se propager vers l'avant, deux battants (16, 17) pivotables revêtus d'un matériau amortisseur des bruits (22, 23) sont reliés par des charnières aux bords frontaux antérieurs (14, 15) des côtés libres (8, 9) de la paroi d'insonorisation en forme de fer-à-cheval. Les battants (16, 17) peuvent pivoter de 60° environ vers l'intérieur et ont une longueur telle que lorsqu'ils sont à l'état complètement fermé ils laissent libre un écart (a) pour le nez de proue d'un avion (1).
Designated States: JP, US
European Patent Office (AT, BE, CH, DE, FR, GB, IT, LU, NL, SE)
Publication Language: German (DE)
Filing Language: German (DE)
Also published as:
EP0322433US4958700