PL445474A1 - UAV head retraction mechanism - Google Patents
UAV head retraction mechanismInfo
- Publication number
- PL445474A1 PL445474A1 PL445474A PL44547423A PL445474A1 PL 445474 A1 PL445474 A1 PL 445474A1 PL 445474 A PL445474 A PL 445474A PL 44547423 A PL44547423 A PL 44547423A PL 445474 A1 PL445474 A1 PL 445474A1
- Authority
- PL
- Poland
- Prior art keywords
- head
- frame
- attached
- retracting
- symmetry
- Prior art date
Links
- 230000005484 gravity Effects 0.000 abstract 1
- 230000003287 optical effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Accessories Of Cameras (AREA)
Abstract
Przedmiotem zgłoszenia przedstawionym na rysunku jest mechanizm chowania głowicy, szczególnie głowicy optycznej w latających pojazdach bezzałogowych. Mechanizm chowania głowicy bezzałogowej składający się z prostokątnej ramy, do której mocowany jest zaczep głowicy z jednej strony osi symetrii ramy, charakteryzuje się tym, że na przeciwległym rogu ramy mocowany jest siłownik liniowy elektryczny wsparty o ramę i głowicę, przy czym głowica osadzona jest obrotowo na ramie i mocowana jest do siłownika mocowanego obrotowo na szczycie głowicy, przy czym mocowanie głowicy do ramy jest przesunięte względem osi symetrii ramy tak, że głowica w położeniu pionowym i poziomym ma w tym samym miejscu środek ciężkości względem ramy. Przy czym mechanizm obrotu posiada blokadę mechaniczną w skrajnych położeniach obrotu głowicy realizacją poprzez występy.The subject of the application presented in the drawing is a mechanism for retracting a head, especially an optical head in unmanned flying vehicles. The mechanism for retracting an unmanned head consisting of a rectangular frame to which a head catch is attached on one side of the frame's axis of symmetry, is characterized in that an electric linear actuator supported by the frame and the head is attached to the opposite corner of the frame, wherein the head is mounted in a rotatable manner on the frame and is attached to an actuator mounted in a rotatable manner on the top of the head, wherein the attachment of the head to the frame is shifted relative to the frame's axis of symmetry so that the head in the vertical and horizontal position has the same center of gravity relative to the frame. Wherein the rotation mechanism has a mechanical lock in the extreme positions of head rotation implemented by means of protrusions.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL445474A PL445474A1 (en) | 2023-07-05 | 2023-07-05 | UAV head retraction mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL445474A PL445474A1 (en) | 2023-07-05 | 2023-07-05 | UAV head retraction mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL445474A1 true PL445474A1 (en) | 2025-01-07 |
Family
ID=94174451
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL445474A PL445474A1 (en) | 2023-07-05 | 2023-07-05 | UAV head retraction mechanism |
Country Status (1)
| Country | Link |
|---|---|
| PL (1) | PL445474A1 (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103640704A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Rotary extending-retracting mechanism of exposed device of aircraft |
| WO2017141154A1 (en) * | 2016-02-18 | 2017-08-24 | Ideaforge Technology Pvt. Ltd. | Retractable camera for fixed wing uav |
| US20170327243A1 (en) * | 2016-05-11 | 2017-11-16 | Dassault Aviation | Observation system for an aircraft, related aircraft and method |
| CN109573034A (en) * | 2018-12-30 | 2019-04-05 | 成都纵横大鹏无人机科技有限公司 | Jack and unmanned plane |
-
2023
- 2023-07-05 PL PL445474A patent/PL445474A1/en unknown
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103640704A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Rotary extending-retracting mechanism of exposed device of aircraft |
| WO2017141154A1 (en) * | 2016-02-18 | 2017-08-24 | Ideaforge Technology Pvt. Ltd. | Retractable camera for fixed wing uav |
| US20170327243A1 (en) * | 2016-05-11 | 2017-11-16 | Dassault Aviation | Observation system for an aircraft, related aircraft and method |
| CN109573034A (en) * | 2018-12-30 | 2019-04-05 | 成都纵横大鹏无人机科技有限公司 | Jack and unmanned plane |
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