NO20003646L - Konstant turtall propeller for modellfly - Google Patents
Konstant turtall propeller for modellflyInfo
- Publication number
- NO20003646L NO20003646L NO20003646A NO20003646A NO20003646L NO 20003646 L NO20003646 L NO 20003646L NO 20003646 A NO20003646 A NO 20003646A NO 20003646 A NO20003646 A NO 20003646A NO 20003646 L NO20003646 L NO 20003646L
- Authority
- NO
- Norway
- Prior art keywords
- propeller
- aircraft
- model aircraft
- present
- model
- Prior art date
Links
- 230000007423 decrease Effects 0.000 abstract 1
- 230000003247 decreasing effect Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/34—Ultra-small engines, e.g. for driving models
-
- 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
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/44—Blade pitch-changing mechanisms electric
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/02—Model aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
Foreliggende oppfinnelse vedrører en elektronisk propellkontroller til bruk i modellfly. Motorens forgasserposisjon styres fortrinnsvis av operatøren, mens propellens angrepsvinkel styres av propellkontrolleren. Det er dog mulighet for automatisk justenng av forgasserposisjon av kontrollerenheten, selv om dette fortinnsvis vil bli utført manuelt før eller under flygning av operatørea Flyets hastighet er gitt av propellens skyvekraft og flyets aerodynamiske egenskaper. Propellens skyvekraft vil bli justert som følge av at forgasserposisjonen økes eller minskes. Dette medfører at propellangrepsvinkelen automatisk! økes eller minskes for å justere det forhåndsinnstilte motorturtall. Med modellfly skal forstås radiostyrte eller selvstyrte, ubemannede, ikke fullskala fly. Et mål med foreliggende oppfinnelse er å tilveiebringe en konstant turtall propellkontroller for bruk i modellfly som tillater anvendelse av fullskala propell og at modellmotoren samtidig kan operere på maksimal virkningsgrad uavhengig av flyets hastighet. Et annet mål med foreliggende oppfinnelse er å tilveiebringe en konstant turtall propellkontroller med en slik størrelse og vekt at den er praktisk anvendbar i et modellfly. Ytterligere et mål med foreliggende oppfinnelse er å tilveiebringe en konstant turtall propellkontroller som er vesentlig rimeligere i pris enn omtalt teknikk.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NO20003646A NO20003646L (no) | 2000-07-17 | 2000-07-17 | Konstant turtall propeller for modellfly |
| US09/908,454 US6638017B1 (en) | 2000-07-17 | 2001-07-16 | Constant rotational speed propeller for model aircrafts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NO20003646A NO20003646L (no) | 2000-07-17 | 2000-07-17 | Konstant turtall propeller for modellfly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| NO20003646D0 NO20003646D0 (no) | 2000-07-17 |
| NO20003646L true NO20003646L (no) | 2002-01-18 |
Family
ID=19911388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO20003646A NO20003646L (no) | 2000-07-17 | 2000-07-17 | Konstant turtall propeller for modellfly |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US6638017B1 (no) |
| NO (1) | NO20003646L (no) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080075597A1 (en) * | 2006-09-22 | 2008-03-27 | Charles Brocklehurst | Systems for powering remote-controlled aircraft |
| CN103914074A (zh) * | 2014-04-22 | 2014-07-09 | 西北工业大学 | 飞行器推力强耦合解耦方法 |
| US12077279B2 (en) * | 2021-04-27 | 2024-09-03 | Pratt & Whitney Canada Corp. | System and method for detecting and mitigating a propeller failure condition |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH631634A5 (en) | 1978-07-27 | 1982-08-31 | Landert Jakob | Adjustable pitch propeller, especially for model aircraft and ventilators. |
| US5222022A (en) * | 1986-12-01 | 1993-06-22 | Woodward Governor Company | Method and apparatus for iterated determinations of sensed speed and speed governing |
| EP0436231B1 (en) | 1989-12-30 | 1996-03-06 | Toyota Jidosha Kabushiki Kaisha | Pitch control apparatus for variable pitch propeller |
| NO170722C (no) * | 1990-10-12 | 1992-11-25 | Oddvard Johnsen | Fremgangsmaate og innretning for oppnaaelse av optimal utnyttelse av et fartoeys fremdriftsmaskineri |
| JPH0524585A (ja) | 1991-07-25 | 1993-02-02 | Toyota Motor Corp | 可変ピツチプロペラのピツチ制御装置 |
| US5451141A (en) * | 1993-12-23 | 1995-09-19 | United Technologies Corporation | Propeller pitch change machanism with inductive brake and motor |
-
2000
- 2000-07-17 NO NO20003646A patent/NO20003646L/no not_active Application Discontinuation
-
2001
- 2001-07-16 US US09/908,454 patent/US6638017B1/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US6638017B1 (en) | 2003-10-28 |
| NO20003646D0 (no) | 2000-07-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FC2A | Withdrawal, rejection or dismissal of laid open patent application |