ITMO20100281A1 - CARTER A BOCCHE DI LUPO - Google Patents
CARTER A BOCCHE DI LUPO Download PDFInfo
- Publication number
- ITMO20100281A1 ITMO20100281A1 IT000281A ITMO20100281A ITMO20100281A1 IT MO20100281 A1 ITMO20100281 A1 IT MO20100281A1 IT 000281 A IT000281 A IT 000281A IT MO20100281 A ITMO20100281 A IT MO20100281A IT MO20100281 A1 ITMO20100281 A1 IT MO20100281A1
- Authority
- IT
- Italy
- Prior art keywords
- dis
- carter
- wolf
- wheel
- mouths
- Prior art date
Links
- 241000282461 Canis lupus Species 0.000 claims description 8
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/40—Alighting gear characterised by elements which contact the ground or similar surface the elements being rotated before touch-down
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Preparation Of Compounds By Using Micro-Organisms (AREA)
Description
Brevetto di invenzione industriale avente per titolo: Industrial invention patent entitled:
“CARTER A BOCCHE DI LUPO” (T apparecchiatura viene montata sulle ruote dei carrelli degli aerei per metterle in rotazione nel momento delTatterraggio). "WOLF MOUTH CARTER" (The equipment is mounted on the wheels of aircraft trolleys to make them rotate when landing).
DESCRIZIONE DESCRIPTION
Per ottenere questo vantaggio II Carter a bocca di lupo viene montato sulle ruote dei carrelli (vedi dis. A). Il Carter comprende due bocche di lupo (dis. BB), collegate alle due sacche (dis. CC) e terminante nei diffusori (dis. DD). I cerchi delle ruote sono costruiti con raggi ad elica. To obtain this advantage, the L-shaped carter is mounted on the wheels of the trolleys (see dis. A). The Carter includes two wolf mouths (dis. BB), connected to the two pockets (dis. CC) and ending in the diffusers (dis. DD). The wheel rims are constructed with helical spokes.
Funzionamento del sistema: all’apertura dei carrelli, fase di atterraggio, l’aereo possiede ancora una notevole velocità le ruote dei carrelli quindi vengono investite dal flusso dell’ aria. Il Carter a bocca di lupo convoglia l’aria e la fa affluire tramite i diffusori sulle eliche dei cerchi, obbligando le ruote ad entrare in rotazione nel senso indicato dalla freccia del disegno. System operation: when the trolleys are opened, landing phase, the plane still has a considerable speed, the trolley wheels are therefore hit by the flow of air. The Lark Carter conveys the air and makes it flow through the diffusers on the propellers of the rims, forcing the wheels to rotate in the direction indicated by the arrow in the drawing.
La rotazione delle ruote deve essere regolata elettronicamente, affinché lo sviluppo della circonferenza per il numero di giri non superi la velocità dell’atterraggio del velivolo. The rotation of the wheels must be electronically adjusted, so that the development of the circumference for the number of revolutions does not exceed the landing speed of the aircraft.
L’atterraggio sulla pista avverrà con un contatto dolce e senza sussulti. The landing on the runway will take place with a gentle contact and without jolts.
Ulteriori caratteristiche e vantaggi dell’invenzione risulteranno evidenziati dal disegno allegato che illustra la collocazione del Carter a bocche di lupo e la funzionalità nel momento dell’atterraggio dell’aereo. Further features and advantages of the invention will be highlighted by the attached drawing which illustrates the location of the wolf mouth cover and its functionality when the plane lands.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000281A ITMO20100281A1 (en) | 2010-10-08 | 2010-10-08 | CARTER A BOCCHE DI LUPO |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000281A ITMO20100281A1 (en) | 2010-10-08 | 2010-10-08 | CARTER A BOCCHE DI LUPO |
Publications (1)
Publication Number | Publication Date |
---|---|
ITMO20100281A1 true ITMO20100281A1 (en) | 2012-04-09 |
Family
ID=43738159
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT000281A ITMO20100281A1 (en) | 2010-10-08 | 2010-10-08 | CARTER A BOCCHE DI LUPO |
Country Status (1)
Country | Link |
---|---|
IT (1) | ITMO20100281A1 (en) |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2777651A (en) * | 1955-05-24 | 1957-01-15 | Edward C Gates | Aircraft landing wheel rotating means |
US4061294A (en) * | 1977-01-21 | 1977-12-06 | Hawkins St Elmo | Aircraft wheel rotator |
BE865732A (en) * | 1978-04-06 | 1978-10-06 | Verbinnen Paul | IMPROVEMENTS TO AIRCRAFT LANDING GEARS |
GB1527880A (en) * | 1975-12-24 | 1978-10-11 | Stern M | Aircraft landing wheel |
US4385739A (en) * | 1980-04-28 | 1983-05-31 | Soderberg John V | System for enhancing airborne safety of airborne vehicles as well as reducing tire wear thereof |
US5104063A (en) * | 1990-04-27 | 1992-04-14 | Hartley James M | Aircraft landing gear prerotation system |
DE4407126A1 (en) * | 1994-02-18 | 1995-08-24 | Walter Georg Steiner | Aircraft undercarriage wheel rotating and braking system |
US6032900A (en) * | 1998-07-02 | 2000-03-07 | Smith; Robert Alfred | Aircraft wheel rotating device |
DE20003286U1 (en) * | 2000-02-23 | 2000-08-03 | Koehl Stephan | Device for accelerating aircraft wheels to a certain speed using compressed air before contact with the ground |
-
2010
- 2010-10-08 IT IT000281A patent/ITMO20100281A1/en unknown
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2777651A (en) * | 1955-05-24 | 1957-01-15 | Edward C Gates | Aircraft landing wheel rotating means |
GB1527880A (en) * | 1975-12-24 | 1978-10-11 | Stern M | Aircraft landing wheel |
US4061294A (en) * | 1977-01-21 | 1977-12-06 | Hawkins St Elmo | Aircraft wheel rotator |
BE865732A (en) * | 1978-04-06 | 1978-10-06 | Verbinnen Paul | IMPROVEMENTS TO AIRCRAFT LANDING GEARS |
US4385739A (en) * | 1980-04-28 | 1983-05-31 | Soderberg John V | System for enhancing airborne safety of airborne vehicles as well as reducing tire wear thereof |
US5104063A (en) * | 1990-04-27 | 1992-04-14 | Hartley James M | Aircraft landing gear prerotation system |
DE4407126A1 (en) * | 1994-02-18 | 1995-08-24 | Walter Georg Steiner | Aircraft undercarriage wheel rotating and braking system |
US6032900A (en) * | 1998-07-02 | 2000-03-07 | Smith; Robert Alfred | Aircraft wheel rotating device |
DE20003286U1 (en) * | 2000-02-23 | 2000-08-03 | Koehl Stephan | Device for accelerating aircraft wheels to a certain speed using compressed air before contact with the ground |
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