RU2010106695A - AIRCRAFT CHASSIS - Google Patents
AIRCRAFT CHASSIS Download PDFInfo
- Publication number
- RU2010106695A RU2010106695A RU2010106695/11A RU2010106695A RU2010106695A RU 2010106695 A RU2010106695 A RU 2010106695A RU 2010106695/11 A RU2010106695/11 A RU 2010106695/11A RU 2010106695 A RU2010106695 A RU 2010106695A RU 2010106695 A RU2010106695 A RU 2010106695A
- Authority
- RU
- Russia
- Prior art keywords
- wheel
- aircraft
- pair
- landing gear
- electromagnetic coils
- Prior art date
Links
Landscapes
- Tires In General (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
Шасси самолета, имеющая колеса, состоящие из резиновых покрышек, дисков с ободами, отличающаяся тем, что внутри диска с ободом, размещены две пары электромагнитных катушек с железными сердечниками, закрепленными радиально на полую ось шасси, одна пара предназначена для раскручивания колеса, а другая пара для регулирования числа оборотов колеса и его торможения, причем линейная скорость вращения колеса определяется тахометром-датчиком, фиксирующим спидометром колеса, и все провода, идущие от электромагнитных катушек, через полую ось подключены к бортовому источнику электропитания самолета. Aircraft landing gear having wheels consisting of rubber tires, rim discs, characterized in that two pairs of electromagnetic coils with iron cores mounted radially on the hollow axis of the landing gear are located inside the rim disc, one pair is designed to spin the wheel, and the other pair to control the number of revolutions of the wheel and its braking, and the linear speed of the wheel is determined by the tachometer sensor, fixing the speedometer of the wheel, and all wires coming from the electromagnetic coils through the hollow axis They are connected to the onboard power supply of the aircraft.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2010106695/11A RU2433065C1 (en) | 2010-02-24 | 2010-02-24 | Aircraft landing gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2010106695/11A RU2433065C1 (en) | 2010-02-24 | 2010-02-24 | Aircraft landing gear |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2010106695A true RU2010106695A (en) | 2011-08-27 |
| RU2433065C1 RU2433065C1 (en) | 2011-11-10 |
Family
ID=44756361
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2010106695/11A RU2433065C1 (en) | 2010-02-24 | 2010-02-24 | Aircraft landing gear |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2433065C1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2581996C1 (en) * | 2015-03-11 | 2016-04-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Уфимский государственный авиационный технический университет" | Method for spin-braking of landing wheel |
-
2010
- 2010-02-24 RU RU2010106695/11A patent/RU2433065C1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2433065C1 (en) | 2011-11-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20130225 |