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Application filed by 신호근, 이대성filedCritical신호근
Priority to KR1019900014122ApriorityCriticalpatent/KR920006203A/en
Publication of KR920006203ApublicationCriticalpatent/KR920006203A/en
Structures Of Non-Positive Displacement Pumps
(AREA)
Abstract
내용 없음No content
Description
고속 비행체의 홴(FAN)성능을 높이기 위한 유체유도 고정익(GUIDED SDATOR)GUIDED SDATOR for improving the FAN performance of high-speed aircraft
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음As this is a public information case, the full text was not included.
제1도는 본 발명을 설명하기 위한 측단면도.1 is a side cross-sectional view for explaining the present invention.
제2도는 제1도의 A-A선 절단면도.2 is a cross-sectional view taken along the line A-A of FIG.
제3도는 본 발명을 설명하기 위한 설명도.3 is an explanatory diagram for explaining the present invention.
Claims (1)
각도면에 표시하고 상술한 바와같이 고속 비행체의 홴 전면에 유체유도 고정익(도면1, 2, 3)을 설치하여 홴 전면에서 진입하는 공기(3)를 홴(2)의 추진각과 비슷하게 평행(平行)유도, 회전, 진압하도록 장치한 유체유도 고정익(1)으로 고속비행시 추력감소를 방지하는 목적에 사용하며 항공기, 고속선박등의 추진 장치에 사용하는 고속비행제의 홴 성능을 높이기 위한 유체유도 고정익.As shown above, the fluid-guided fixed blades (Figs. 1, 2, and 3) are installed on the front surface of the high-speed aircraft, and the air (3) entering from the front surface of the aircraft is parallel to the propulsion angle of the surface (2). Fluid guided fixed vane (1) designed to guide, rotate, and suppress the fluid guide to prevent thrust loss during high-speed flight and to improve the performance of high-speed aircraft used in propulsion systems such as aircraft and high-speed ships. Fixed wing.※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.※ Note: The disclosure is based on the initial application.
KR1019900014122A1990-09-071990-09-07
GUIDED SDATOR for improving the FAN performance of high-speed aircraft
KR920006203A
(en)
PROPELLER SHEETS AND PROCEDURES, SPECIFICALLY INTENDED FOR DRAINING MARINES, REVERSIBLE DEVICES FOR THE CONVERSION OF ROTARY MOVEMENT INTO RELIGIOUS AND SIMILAR DEVICES IN AND FOR MINIMIZATION OF CAVITATION AND