КОМПОЗИТНАЯ ПАНЕЛЬ В СБОРЕ ДЛЯ САМОЛЕТА И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ: Fid-Bau Portal

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КОМПОЗИТНАЯ ПАНЕЛЬ В СБОРЕ ДЛЯ САМОЛЕТА И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ

The invention refers to an aircraft composite panel assembly (10) comprising a first panel (1) having upper and lower faces, the lower face having a recess (7) on a first side (1a) of the panel (1); a second panel (2) having upper and lower faces, the lower face having an outward projection (8) at a first side (2a) of the panel (2), the outward projection (8) received on the recess (7) forming a lower continuous face; and a forward stack of plies (5) of composite material bonded to the upper face of the first panel (1), the forward stack of plies (5) having an edge (5a) aligned with the first side (1 a) of the first panel (1), and the number of plies of the forward stack of plies (5) decreasing away from the first side (1a) of the first panel (1).

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КОМПОЗИТНАЯ ПАНЕЛЬ В СБОРЕ ДЛЯ САМОЛЕТА И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ

The invention refers to an aircraft composite panel assembly (10) comprising a first panel (1) having upper and lower faces, the lower face having a recess (7) on a first side (1a) of the panel (1); a second panel (2) having upper and lower faces, the lower face having an outward projection (8) at a first side (2a) of the panel (2), the outward projection (8) received on the recess (7) forming a lower continuous face; and a forward stack of plies (5) of composite material bonded to the upper face of the first panel (1), the forward stack of plies (5) having an edge (5a) aligned with the first side (1 a) of the first panel (1), and the number of plies of the forward stack of plies (5) decreasing away from the first side (1a) of the first panel (1).

КОМПОЗИТНАЯ ПАНЕЛЬ В СБОРЕ ДЛЯ САМОЛЕТА И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ

The invention refers to an aircraft composite panel assembly (10) comprising a first panel (1) having upper and lower faces, the lower face having a recess (7) on a first side (1a) of the panel (1); a second panel (2) having upper and lower faces, the lower face having an outward projection (8) at a first side (2a) of the panel (2), the outward projection (8) received on the recess (7) forming a lower continuous face; and a forward stack of plies (5) of composite material bonded to the upper face of the first panel (1), the forward stack of plies (5) having an edge (5a) aligned with the first side (1 a) of the first panel (1), and the number of plies of the forward stack of plies (5) decreasing away from the first side (1a) of the first panel (1).

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Titel:

КОМПОЗИТНАЯ ПАНЕЛЬ В СБОРЕ ДЛЯ САМОЛЕТА И СПОСОБ ЕЕ ИЗГОТОВЛЕНИЯ

Erscheinungsdatum:

28.05.2019

Medientyp:

Patent

Format:

Elektronische Ressource

Sprache:

Russisch

Klassifikation:

IPC: E04C STRUCTURAL ELEMENTS , Bauelemente

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