Claims
- 1. A turbo tool comprising:a housing forming a hollow section, said housing comprising at least one air inlet and a nozzle opening spaced from said at least one air inlet; a brushroll rotatably mounted in said housing and within said nozzle opening; a turbine mounted in said housing and drivingly connected to said brushroll for rotating said brushroll, said turbine being driven by a first airflow through said at least one air inlet in said housing, wherein a longitudinal axis of said brushroll is parallel to a longitudinal axis of said turbine; and a first conduit located in said housing and connected at a first end to said nozzle opening, wherein a second airflow occurs through said first conduit and wherein said first and second airflows occur at the same time.
- 2. The turbo tool of claim 1 wherein said brushroll is mounted parallel to a longitudinal axis of said housing.
- 3. The turbo tool of claim 1 wherein said nozzle opening is oriented parallel to a longitudinal axis of said turbine.
- 4. The turbo tool of claim 1 further comprising a second conduit being fluidly connected to said first conduit.
- 5. The turbo tool of claim 4 further comprising a third conduit fluidly connected to said second conduit.
- 6. The turbo tool of claim 5 wherein said third conduit is fluidly connected to an associated vacuum source.
- 7. The turbo tool of claim 6 further comprising a swivel attachment connected to said third conduit, wherein said swivel attachment allows said housing to swivel between two positions approximately 180 degrees apart.
- 8. The turbo tool of claim 7 further comprising a locking member which serves to lock said swivel attachment into one of said two positions and selectively allows the swivel attachment to rotate.
- 9. The turbo tool of claim 8 wherein said locking member is made of a resilient material which acts as a spring when displaced.
- 10. The turbo tool of claim 4, wherein said second airflow from said first conduit and said first airflow from said at least one air inlet merge into said second conduit.
- 11. The turbo tool of claim 1 further comprising a brushroll housing located within said nozzle opening, said brushroll housing enclosing said brushroll.
- 12. The turbo tool of claim 1 wherein said turbine comprises a rotor, a pair of spiraled inlet channels for directing airflow directly to said turbine, and an exit channel.
- 13. A turbo tool comprising:a main housing forming a hollow section, said housing comprising at least one air inlet and a nozzle opening spaced from said at least one air inlet; a brushroll housing located in said main housing and communicating with said nozzle opening; a brushroll rotatably mounted in said brushroll housing; a turbine mounted in said main housing and drivingly connected to said brushroll for rotating said brushroll, said turbine being driven by a first airflow through said at least one air inlet in said main housing, said at least one air inlet comprising at least one spiraled inlet channel for directing airflow directly to said turbine; and a first conduit located in said main housing and connected at a first end to said brushroll housing, wherein a second airflow occurs through said first conduit.
- 14. The turbo tool of claim 13 further comprising:a second conduit held in said housing, said first conduit being fluidly connected at a second end to said second conduit; and a third conduit being fluidly connected to said second conduit.
- 15. The turbo tool of claim 14 further comprising a swivel attachment connected to said third conduit, wherein said swivel attachment allows said main housing to swivel between two positions approximately 180 degrees apart and can be locked into one of said two positions.
- 16. The turbo tool of claim 15, wherein said second airflow from said first conduit and said first airflow from said at least one air inlet merge into said second conduit.
- 17. The turbo tool of claim 13 wherein said brushroll is mounted parallel to a longitudinal axis of said brushroll housing.
- 18. The turbo tool of claim 13 wherein said turbine comprises a rotor, and an exit channel spaced from said motor.
- 19. A turbo tool comprising:a housing forming a hollow section, said housing comprising at least one air inlet and a nozzle opening spaced from said at least one air inlet; a brushroll rotatably mounted to said housing; a turbine mounted in said housing and drivingly connected to said brushroll for rotating said brushroll, said turbine being driven by a first airflow through said at least one air inlet in said housing; and a swivel attachment connected to said housing, wherein said swivel attachment allows said housing to swivel between two positions approximately 180 degrees apart; said swivel attachment comprises a locking member made of a resilient material which acts as a spring when displaced.
- 20. The turbo tool of claim 19 wherein said brushroll is mounted parallel to a longitudinal axis of said housing.
- 21. The turbo tool of claim 19 wherein said brushroll is mounted on an axis parallel to a longitudinal axis of said turbine.
- 22. The turbo tool of claim 19 further comprising a first conduit located in said housing and connected at a first end to said nozzle opening, wherein a second airflow occurs through said first conduit.
- 23. The turbo tool of claim 22 further comprising a second conduit being fluidly connected to said first conduit.
- 24. The turbo tool of claim 23 further comprising a third conduit fluidly connected to said second conduit.
- 25. The turbo tool of claim 23, wherein said second airflow from said first conduit and said first airflow from said at least one air inlet merge into said second conduit.
- 26. The turbo tool of claim 19, wherein said turbine comprises a rotor and a pair of spiraled inlet channels adjacent said rotor for directing airflow directly to such rotor.
Parent Case Info
This application claims priority from provisional application Ser. No. 60/176,122 filed on Jan. 14, 2000.
US Referenced Citations (15)
Foreign Referenced Citations (1)
Number |
Date |
Country |
2 105 413 |
Mar 1983 |
GB |
Provisional Applications (1)
|
Number |
Date |
Country |
|
60/176122 |
Jan 2000 |
US |