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US 12,617,550 B2Granted
Guidance system
AssigneeTusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi
InventorFatih Turk
Life of this patent
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Abstract
The present invention relates to a body (2) that is an aircraft, at least one engine (3) that is located on the body (2) and generates the power required for the flight of the aircraft, and at least one exhaust (4) that is located on the engine (3) and transmits the fluid (A) heated inside the engine (3) due to the operation of the engine (3) to the outside of the aircraft.
Claims10
A guidance system (1) comprising:
- a body (2) that is an aircraft,
- at least one engine (3) that is located on the body (2) that generates power required for flight of the aircraft, and
- at least one exhaust (4) that is located on the engine (3) that transmits fluid (A) heated inside the engine (3) due to operation of the engine (3) to an outside of the aircraft,
- wherein at least a guide (5) that is located on the body and/or on the exhaust (4),
- wherein in a way that the guide faces towards the exhaust (4) outlet, meets air flow (H) formed during the flight of the aircraft and takes in the air flow (H), directs the air flow (H) to an exhaust outlet and thus ensures that the fluid heated and coming out of the exhaust (4) is dispersed irregularly and/or an exhaust direction is changed,
- wherein at least one fan (501) is located inside the guide (5) that takes the air flow (H) into the guide (5) by rotating and transmitting the air flow to the exhaust outlet, and
- wherein at least one opening (6) that is located on the guide that allows the air flow (H) to enter the guide and thus allows air to be absorbed from an external environment.
4 more elements
Dependencies are inferred from the claim text.