PROBLEM TO BE SOLVED: To provide a new aircraft with one or more air intakes having reduced engine installation losses.SOLUTION: The present invention is related to an aircraft 1 with a fuselage 2 that accommodates at least one air breathing propulsion engine 8a. The fuselage 2 has a maximum fuselage width determined in the region of the at least one air breathing propulsion engine 8a and comprises at least one front fuselage cowling and at least one rear fuselage cowling that are each covering the at least one air breathing propulsion engine 8a at least partly. The at least one front and rear fuselage cowlings are spaced apart from each other in a direction transverse to a longitudinal axis of the at least one air breathing propulsion engine 8a by a predetermined cowling offset to define a dynamic air intake 9 through which an intake air stream is supplied to the at least one air breathing propulsion engine 8a in operation.SELECTED DRAWING: Figure 1
【課題】エンジン取り付け損失が低減された1つ以上の空気取入口を備えた新しい航空機を提供する。【解決手段】本発明は、少なくとも1つの空気吸入推進エンジン8aを収容する胴体2を備えた航空機1に関する。胴体2は、少なくとも1つの空気吸入推進エンジン8aの領域内で決定された最大胴体幅を有し、それぞれが少なくとも部分的に少なくとも1つの空気吸入推進エンジン8aを覆っている少なくとも1つの前部胴体カウリングと少なくとも1つの後部胴体カウリングとを含む。少なくとも1つの前部及び後部胴体カウリングは、それを通って吸気流が作動中の少なくとも1つの空気吸入推進エンジン8aに供給される動的空気取入口9を規定するために、少なくとも1つの空気吸入推進エンジン8aの縦軸に対して横向きの方向に所定のカウリング・オフセット分だけ互いに間隔をおいて配置される。【選択図】図1
AIRCRAFT WITH AIR INTAKE FOR AIR BREATHING PROPULSION ENGINE
空気吸入推進エンジン用の空気取入口を備えた航空機
2016-04-25
Patent
Electronic Resource
Japanese
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