US3709630A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Pneumatic motor for medical instruments
Assignee: Howmet International Inc
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Filing: 1970-08-07
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Granted: 1973-01-09
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Expires: 1990-08-07
Abstract
Abstract The invention relates to a small pneumatic motor for a rotating medical instrument, especially for drilling or milling instruments. A shaft with a turbine is supported in a housing with the gas inlet end of the turbine arranged towards the output end of the motor. The driving gas flows to the turbine inlet side via channels arranged longitudinally in the housing along the periphery of the turbine and then back to the input end of the housing. Discharge of driving gas at the output end of the housing toward the patient is avoided in this way.
Inventors
- 👤 F Pohl
- 👤 A Keller
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 20:06
CPC Classifications
A; A61; A61C; A61C1/00; A61C1/02; A61C1/05; A61B; A61B17/00; A61B17/16; A61B17/1613; A61B17/1628; F; F01; F01D; F01D15/00; F01D15/06; A61B17/1626; Y; Y10; Y10S; Y10S415/00; Y10S415/904
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
205 words
A pneumatic turbine powered surgical motor apparatus for rotating a medical instrument comprising, in combination, an elongated housing having a longitudinal axis, an input end and an output end, a shaft rotatably mounted in said housing concentric with said axis and projecting from said output end adapted to drive a cutting instrument, a pressurized gas connection and an exhaust gas connection defined on said housing at said input end, an axial flow turbine having a rotor rotatably mounted in said housing concentric thereto and drivingly connected to said shaft, said turbine having an inlet disposed toward said housing output end and an exit disposed toward said housing input end, first passage means longitudinally defined in said housing concentrically extending about the periphery of said turbine and communicating with said pressurized gas connection and said turbine inlet, and second passage means defined in said housing communicating with said exhaust gas connection and said turbine exit whereby pressurized gas entering said pressurized gas connection and first passage flows toward said housing output end to said turbine inlet, enters said turbine inlet and reverses its direction of flow to flow through said turbine toward said housing input end and from said turbine exit to said exhaust gas connection.
Claim 2
Dependent Claim
205 words
A pneumatic turbine powered surgical motor apparatus for rotating a medical instrument comprising, in combination, an elongated housing having a longitudinal axis, an input end and an output end, a shaft rotatably mounted in said housing concentric with said axis and projecting from said output end adapted to drive a cutting instrument, a pressurized gas connection and an exhaust gas connection defined on said housing at said input end, an axial flow turbine having a rotor rotatably mounted in said housing concentric thereto and drivingly connected to said shaft, said turbine having an inlet disposed toward said housing output end and an exit disposed toward said housing input end, first passage means longitudinally defined in said housing concentrically extending about the periphery of said turbine and communicating with said pressurized gas connection and said turbine inlet, and second passage means defined in said housing communicating with said exhaust gas connection and said turbine exit whereby pressurized gas entering said pressurized gas connection and first passage flows toward said housing output end to said turbine inlet, enters said turbine inlet and reverses its direction of flow to flow through said turbine toward said housing input end and from said turbine exit to said exhaust gas connection.
Claim 3
Dependent Claim
66 words
In a pneumatic turbine powered surgical motor apparatus as in claim 1, a nozzle member within said housing located adjacent said turbine inlet, nozzles defined in said nozzle member for directing pressurized gas into said turbine, said nozzle member including an annular bushing circumscribing said shaft and extending toward said turbine exit and being radially spaced from said shaft and turbine rotor by small running clearances.
Claim 4
Dependent Claim
51 words
In a pneumatic turbine powered surgical motor apparatus as in claim 1 wherein said first passage means comprises an annular chamber concentrically disposed about said turbine and said second passage means comprises a plurality of passages axially defined in said housing extending between said turbine exit and said exhaust gas connection.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1976-01-09 | 1976-07-10 | 1977-01-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1980-01-09 | 1980-07-10 | 1981-01-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1984-01-09 | 1984-07-10 | 1985-01-09 | $7700.00 | Window Closed / Lapsed |