US4983153A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Gear unit, particularly for use in a helicopter
Assignee: DAF Special Products BV
•
Filing: 1989-01-09
•
Granted: 1991-01-08
•
Expires: 2009-01-09
Abstract
Abstract In a high-loaded, light-weight, compact, multi-stage gear transmission unit with at least one stage with non-parallel shafts, and a transmission ratio between approximately 70 and 150, like a helicopter transmission, said angle transmission generally forms the weakest link. By adoption of a face gear/cylindrical pinion-stage instead of the commonly used bevelled-stage, not only a more reliable drive is possible, but its efficiency is higher, due to less friction, its size is smaller, its adjustment is simpler such that straight forward replacement becomes possible, and--not in the least--the transmission ratio of said angle drive tends to high ratios in contrast to known bevelled-drives which tend to low ratios. In many cases one or even more stages less become possible, providing a further important reduction in weight and size.
Inventors
- 👤 Waltherus J. T. H. Luijten
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 11:58
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/04; B64C27/12; F; F16; F16H; F16H1/00; F16H1/02; F16H1/04; F16H1/12; Y; Y10; Y10T; Y10T74/00; Y10T74/19; Y10T74/19642; Y10T74/1966; Y10T74/21; Y10T74/2186
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
165 words
A gear unit having a plurality of reduction stages, for use in a helicopter, and intended for a relatively high output torque at an output shaft which carries and drives the main rotors of the helicopter with a relatively low speed of rotation and a total transmission ratio between about 70 and 150, comprising at least one reduction stage with non-parallel shafts, and including a face gear transmission used on the last or next to last reduction stage of the gear unit, said stage with non-parallel shafts comprising a rotor shaft, a gear box mounted around said rotor shaft, a face gear disposed in said gear unit positioned concentrically to said output shaft and cooperating with a cylindrical spur gear on said rotor shaft which transmits power to the output shaft, said cylindrical spur gear being removable from said gear unit through detachable cover means mounted to said gear box and/or by detaching said gear box procedures previously required to replace the cylindrical spur gear.
Claim 2
Dependent Claim
165 words
A gear unit having a plurality of reduction stages, for use in a helicopter, and intended for a relatively high output torque at an output shaft which carries and drives the main rotors of the helicopter with a relatively low speed of rotation and a total transmission ratio between about 70 and 150, comprising at least one reduction stage with non-parallel shafts, and including a face gear transmission used on the last or next to last reduction stage of the gear unit, said stage with non-parallel shafts comprising a rotor shaft, a gear box mounted around said rotor shaft, a face gear disposed in said gear unit positioned concentrically to said output shaft and cooperating with a cylindrical spur gear on said rotor shaft which transmits power to the output shaft, said cylindrical spur gear being removable from said gear unit through detachable cover means mounted to said gear box and/or by detaching said gear box procedures previously required to replace the cylindrical spur gear.
Claim 3
Dependent Claim
64 words
Gear unit according to claim 1, wherein a planetary transmission assembly comprising a sun gear, a ring gear, and a plurality of planets is provided in the power flow between the face gear and the output shaft, the face gear being constructed in the form of a ring gear with the planetary assembly planets and sun gear being disposed substantially within the ring gear.
Claim 4
Dependent Claim
56 words
Gear unit according to claim 1 wherein said gear unit housing has a substantially flattened cylindrical shape with a flat drum and said spur gear--face gear is a second stage of said plurality of reduction stages and a preceding reduction stage is also in the form of a face gear transmission with a cylindrical spur gear.
Claim 5
Dependent Claim
77 words
Gear unit according to claim 1, characterized in that there is a total of three reduction stages of the type comprising a face gear and a cylindrical (spur) gear, the first and third stages being a substantially right angled transmission and the middle stage being a gear transmission with an angle between the shafts in the range between about 10° and 45°, said middle stage transmitting the power to the third stage with or without power division.
Claim 6
Dependent Claim
147 words
A gear unit in combination with a helicopter having a plurality of transmission reduction stages, for use in said helicopter, and intended for a relatively high output torque at an output shaft which carries and drives the main rotor of the helicopter with a relatively low speed of rotation and a total transmission ratio between about 70 and 150, comprising a transmission reduction stage with non-parallel shafts after the initial transmission reduction stage, said transmission reduction stage with non-parallel shafts comprising a cylindrical pinion gear positioned on a shaft for transmission of power to a face gear positioned adjacent to said output shaft and cooperating with said cylindrical pinion gear, said shaft and pinion gear being encased by a gearbox with removable cover means, said cover means when removed allowing the shaft and associated cylindrical pinion gear to be removed from the transmission for repair or replacement.
Claim 7
Dependent Claim
147 words
A gear unit in combination with a helicopter having a plurality of transmission reduction stages, for use in said helicopter, and intended for a relatively high output torque at an output shaft which carries and drives the main rotor of the helicopter with a relatively low speed of rotation and a total transmission ratio between about 70 and 150, comprising a transmission reduction stage with non-parallel shafts after the initial transmission reduction stage, said transmission reduction stage with non-parallel shafts comprising a cylindrical pinion gear positioned on a shaft for transmission of power to a face gear positioned adjacent to said output shaft and cooperating with said cylindrical pinion gear, said shaft and pinion gear being encased by a gearbox with removable cover means, said cover means when removed allowing the shaft and associated cylindrical pinion gear to be removed from the transmission for repair or replacement.
References Cited (Backward Citations)
US11258A
Cited
US267440A
Cited
US2771143A
Cited
US2520887A
Cited
US2911851A
Cited
DE1042388B
Cited
US3129608A
Cited
GB1000430A
Cited
US3188884A
Cited
US3486832A
Cited
US3669564A
Cited
US3762669A
Cited
FR2354922A1
Cited
US4238970A
Cited
DE3144112A1
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1994-01-07 | 1994-07-09 | 1995-01-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-01-07 | 1998-07-09 | 1999-01-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-01-07 | 2002-07-09 | 2003-01-08 | $7700.00 | Window Closed / Lapsed |