TR2021022099A2 - ELECTRIC FAN MOTORIZED AIR TO LAND NAVIGATION MISSILE - Google Patents
ELECTRIC FAN MOTORIZED AIR TO LAND NAVIGATION MISSILEInfo
- Publication number
- TR2021022099A2 TR2021022099A2 TR2021/022099A TR2021022099A TR2021022099A2 TR 2021022099 A2 TR2021022099 A2 TR 2021022099A2 TR 2021/022099 A TR2021/022099 A TR 2021/022099A TR 2021022099 A TR2021022099 A TR 2021022099A TR 2021022099 A2 TR2021022099 A2 TR 2021022099A2
- Authority
- TR
- Turkey
- Prior art keywords
- rocket
- engine
- block
- radio receiver
- power
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/10—Missiles having a trajectory only in the air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Bu buluş, hava araçlarında kullanılabilen kara veya denizdeki hedefleri vurmaya yönelik Elektrik Fan Motorlu Havadan Karaya Seyir Füzesi ile ilgili olup, özelliği; roketin arka kısmını oluşturan ve motorları içerisinde barındıran motor bloğu (10), bataryaları ve motor sürücüsünü içerisinde barındıran güç bloğu (2), iki adet anahtar ve bu anahtarların yataklarının bulunduğu kontrol bloğu (3), faydalı yük taşımak için ve hava sürtünmesini azaltan faydalı yük bloğu (4), motor bloğunun (1) etrafına 4 adet ve 90 dereceli açılar ile yerleştirilen roketin yönünü ayarlayabilen yönlendirici finler (5), motorun miline bağlı pervanenin yüksek devirlerde dönmesi ile rokete itki kuvveti veren elektrikli fan motoru, roket içerisindeki bileşenlere güç sağlayan Li-Po bataryalar, aldığı komutları motora göndererek roket motorunun çalışmasını kontrol altına alan motor sürücüsü, sistemin gücünü açmaya veya kapatmaya yarayan ana güç anahtarı, dışarıdan sisteme gönderilen verileri 2.4Ghz bandındaki radyo sinyalleri ile almaya yarayan radyo alıcısı, radyo alıcısından gelen sinyal verilerini ve kendi devresinde bulunan 3 adet gyro?dan gelen verileri analiz eden uçuş kontrolcüsü, uçuş kontrolcüsünün analiz edip ilettiği veriler doğrultusunda roketin yönünü ayarlayabilmek için 180 derece sağa veya sola yatarak yönlendirici finleri (5) hareket ettirebilen servo motorlar, radyo alıcısına giden gücü açmaya veya kapamaya yarayan elektronik sistem anahtarı ve radyo alıcısına güç veren elektronik sistem bataryasına sahip olmasıdır.This invention relates to the Electric Fan Motor Air-to-Land Cruise Missile, which can be used in aircraft, for hitting targets on land or at sea, and its feature is; The engine block (10) that forms the rear of the rocket and contains the engines, the power block (2) that contains the batteries and the engine driver, the two keys and the control block (3) where the bearings of these keys are located, the payload that reduces the air friction and carries the payload. block (4), 4 pieces around the engine block (1) and guiding fins (5) that can adjust the direction of the rocket placed at 90-degree angles, electric fan motor that gives thrust to the rocket with the rotation of the propeller connected to the shaft of the engine at high speeds, Li, which provides power to the components in the rocket. -Po batteries, the motor driver that controls the operation of the rocket engine by sending the commands it receives to the engine, the main power switch to turn the power of the system on or off, the radio receiver to receive the data sent to the system from the outside with radio signals in the 2.4Ghz band, the signal data coming from the radio receiver and its own circuit. flight controller that analyzes data from 3 gyro It has servo motors whose controller can move the guiding fins (5) by tilting to the right or left 180 degrees in order to adjust the direction of the rocket in line with the data analyzed and transmitted by the flight controller, an electronic system switch for turning on or off the power to the radio receiver, and an electronic system battery powering the radio receiver. .
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TR2021/022099A TR2021022099A2 (en) | 2021-12-31 | 2021-12-31 | ELECTRIC FAN MOTORIZED AIR TO LAND NAVIGATION MISSILE |
| DE112022006273.8T DE112022006273T5 (en) | 2021-12-31 | 2022-06-24 | AIR-TO-LAND CRUISE MISSILE WITH ELECTRIC FAN MOTOR |
| PCT/TR2022/050659 WO2023128961A1 (en) | 2021-12-31 | 2022-06-24 | Air-to-land cruise missile with electric fan engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TR2021/022099A TR2021022099A2 (en) | 2021-12-31 | 2021-12-31 | ELECTRIC FAN MOTORIZED AIR TO LAND NAVIGATION MISSILE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| TR2021022099A2 true TR2021022099A2 (en) | 2022-02-21 |
Family
ID=85117771
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TR2021/022099A TR2021022099A2 (en) | 2021-12-31 | 2021-12-31 | ELECTRIC FAN MOTORIZED AIR TO LAND NAVIGATION MISSILE |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE112022006273T5 (en) |
| TR (1) | TR2021022099A2 (en) |
| WO (1) | WO2023128961A1 (en) |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2628984Y (en) | 2003-07-08 | 2004-07-28 | 邢球痕 | Air-to-surface missile |
| AU2012277568A1 (en) | 2011-06-28 | 2014-01-23 | Mbda Uk Limited | A bomb for deployment from an air vehicle |
-
2021
- 2021-12-31 TR TR2021/022099A patent/TR2021022099A2/en unknown
-
2022
- 2022-06-24 DE DE112022006273.8T patent/DE112022006273T5/en active Pending
- 2022-06-24 WO PCT/TR2022/050659 patent/WO2023128961A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| DE112022006273T5 (en) | 2025-01-16 |
| WO2023128961A1 (en) | 2023-07-06 |
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