PL443346A1 - Main rotor hub - Google Patents
Main rotor hubInfo
- Publication number
- PL443346A1 PL443346A1 PL443346A PL44334622A PL443346A1 PL 443346 A1 PL443346 A1 PL 443346A1 PL 443346 A PL443346 A PL 443346A PL 44334622 A PL44334622 A PL 44334622A PL 443346 A1 PL443346 A1 PL 443346A1
- Authority
- PL
- Poland
- Prior art keywords
- hub
- wedges
- main rotor
- rotor hub
- button
- Prior art date
Links
- 230000001154 acute effect Effects 0.000 abstract 1
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/02—Hub construction
- B64C11/04—Blade mountings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Permanent Magnet Type Synchronous Machine (AREA)
- Synchronous Machinery (AREA)
- Insulation, Fastening Of Motor, Generator Windings (AREA)
Abstract
Przedmiotem zgłoszenia jest piasta wirnika nośnego. Charakteryzuje się ona tym, że piasta (1) od strony przeciwnej do strony jej montażu posiada otwór (1.1), w którym znajduje się przycisk odblokowujący (2), posiadający od strony mocowania piasty (1) dwa kliny (2.1, 2.2) ułożone naprzeciwko siebie po dwóch stronach osi piasty (1) i posiadające powierzchnię pochyloną pod kątem ostrym do osi piasty (1) od wewnętrznej strony piasty (1). Każdy z klinów (2.1, 2.2) przycisku (2) zazębiony jest z jednym z klinów znajdującym się na sworzniu blokującym (3, 4) ułożonych współosiowo i umiejscowionych w otworach znajdujących się w jarzmie łopat. Pomiędzy sworzniami blokującymi (3, 4) znajduje się sprężyna naciskowa (6).The subject of the application is the hub of the main rotor. It is characterized by the fact that the hub (1) on the side opposite to its mounting side has a hole (1.1) in which the unlocking button (2) is located, with two wedges (2.1, 2.2) arranged opposite to the hub mounting side (1). each other on two sides of the hub axis (1) and having a surface inclined at an acute angle to the hub axis (1) on the inner side of the hub (1). Each of the wedges (2.1, 2.2) of the button (2) is meshed with one of the wedges located on the locking pin (3, 4) arranged coaxially and located in the holes located in the blade yoke. Between the locking pins (3, 4) there is a compression spring (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL443346A PL244047B1 (en) | 2022-12-30 | 2022-12-30 | Main rotor hub |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL443346A PL244047B1 (en) | 2022-12-30 | 2022-12-30 | Main rotor hub |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| PL443346A1 true PL443346A1 (en) | 2023-06-19 |
| PL244047B1 PL244047B1 (en) | 2023-11-20 |
Family
ID=86944937
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL443346A PL244047B1 (en) | 2022-12-30 | 2022-12-30 | Main rotor hub |
Country Status (1)
| Country | Link |
|---|---|
| PL (1) | PL244047B1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| PL446982A1 (en) * | 2023-12-05 | 2024-07-15 | Politechnika Lubelska | Hub with main rotor locking mechanism |
| PL446983A1 (en) * | 2023-12-05 | 2024-07-15 | Politechnika Lubelska | Hub with rotor removal mechanism |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204956919U (en) * | 2015-08-18 | 2016-01-13 | 王军 | Screw connection structure and unmanned aerial vehicle |
| CN205602090U (en) * | 2016-04-01 | 2016-09-28 | 深圳市大疆创新科技有限公司 | Screw, motor, power suit and unmanned vehicles |
| CN206664924U (en) * | 2016-12-14 | 2017-11-24 | 深圳市道通智能航空技术有限公司 | Aircraft and its propeller device for quickly disassembling, propeller, propeller mount component |
| CN109018308B (en) * | 2018-08-09 | 2021-09-21 | 上海歌尔泰克机器人有限公司 | Screw quick detach device and have its unmanned aerial vehicle |
| CN112119009A (en) * | 2019-08-01 | 2020-12-22 | 深圳市大疆创新科技有限公司 | Locking structures, propellers, powerplants, power packs and drones |
-
2022
- 2022-12-30 PL PL443346A patent/PL244047B1/en unknown
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| PL446982A1 (en) * | 2023-12-05 | 2024-07-15 | Politechnika Lubelska | Hub with main rotor locking mechanism |
| PL446983A1 (en) * | 2023-12-05 | 2024-07-15 | Politechnika Lubelska | Hub with rotor removal mechanism |
| PL247891B1 (en) * | 2023-12-05 | 2025-09-15 | Lubelska Polt | Hub with rotor removal mechanism |
| PL247890B1 (en) * | 2023-12-05 | 2025-09-15 | Lubelska Polt | Hub with main rotor locking mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| PL244047B1 (en) | 2023-11-20 |
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