Internal spur gear drive
View Patent ↗An internal spur gear drive has a mounting base including one or more sets of motor mounting lugs extending therefrom, for attaching a corresponding number of drive motors thereto. A drive shaft housing containing a rotary drive shaft extends from the mounting base. A drive bell is affixed to the drive shaft distal end, and rotates therewith. The opposite end of the drive bell has an internally toothed ring gear extending therefrom. Each motor drives a pinion gear which engages the internal teeth of the drive bell ring gear to rotate the drive bell and thus rotate the drive shaft as well. The motor mounting lugs are slotted, allowing the motors to be adjusted radially relative to the drive shaft and drive bell ring gear. This provides adjustment for gear lash, as well as permitting different sizes of pinion gears to be installed on the motors for different gear ratios.
1. An internal spur gear drive, comprising:
an elongate drive shaft housing having a first end and a second end opposite said first end;
a generally planar mounting base extending from the second end of said drive shaft housing, formed integrally therewith and substantially normal thereto;
at least one set of motor mounting lugs extending from said mounting base, substantially coplanar with said mounting base;
said mounting base having at least a pair of structure attachment passages formed therethrough, disposed substantially parallel to said drive shaft housing;
a rotary drive shaft having a first end and a second end opposite the first end, the drive shaft being rotatably mounted within said drive shaft housing with the first end of said drive shaft extending from the first end of said drive shaft housing;
a rotary drive bell having a first end and a second end opposite the first end, the first end of said drive bell being immovably affixed to the first end of said drive shaft in order to rotate with said drive shaft;
an internally toothed ring gear extending from the second end of said drive bell, and circumferentially surrounding said drive shaft housing of said mounting base;
at least one motor immovably affixed to said at least one set of motor mounting lugs of said mounting base, and extending substantially opposite said drive shaft housing;
a motor drive shaft extending from said at least one motor, substantially parallel to said drive shaft housing; and
an externally toothed pinion gear disposed upon said motor drive shaft, and rotationally engaging said internally toothed ring gear of said drive bell for driving said drive bell.
2. The internal spur gear drive according to claim 1 , wherein:
said at least one set of motor mounting lugs comprises a pair of elongate, parallel arms, each of said arms having an elongate motor position adjusting slot formed therethrough;
whereby said at least one motor is radially adjustable positionally relative to said drive shaft housing and said internally toothed ring gear of said drive bell for adjusting gear lash and changing gear ratios as desired.
3. The internal spur gear drive according to claim 1 , wherein said at least one set of motor mounting lugs comprises a plurality of sets selected from the group consisting of two, three, and four sets of motor mounting lugs; and
said at least one motor comprises a separate motor adjustably secured to each of the sets of lugs.
4. The internal spur gear drive according to claim 1 , further including:
an elongate mounting bolt removably disposed through each of said structure attachment passages of said mounting base, and extending generally opposite said drive shaft housing;
an elongate, tubular standoff removably disposed over each said mounting bolt;
each said standoff having a first end adjacent said mounting base, and a second end opposite said first end; and
a standoff pad removably disposed over each said mounting bolt, adjacent the second end of each said standoff.
5. The internal spur gear drive according to claim 1 , further including:
a first bearing installed within the first end of said drive shaft housing and generally medially about said drive shaft;
a second bearing installed within the second end of said drive shaft housing and about the second end of said drive shaft;
a first retaining clip secured about said drive shaft, adjacent said first bearing; and
a second retaining clip secured about said drive shaft, adjacent said second bearing.
6. The internal spur gear drive according to claim 1 , further including means for immovably securing said drive bell to said drive shaft.
7. A model aircraft powerplant assembly, comprising:
an elongate propeller drive shaft housing having a first end and a second end opposite the first end;
a generally planar mounting base extending from the second end of said propeller drive shaft housing, formed integrally therewith and substantially normal thereto;
at least one set of motor mounting lugs extending from said mounting base, substantially coplanar with said mounting base;
said mounting base having at least a pair of structure attachment passages formed therethrough, disposed substantially parallel to said propeller drive shaft housing;
a rotary propeller drive shaft having a first end and a second end opposite the first end, the drive shaft being rotatably mounted within said propeller drive shaft housing with the first end of said drive shaft extending from the first end of said propeller drive shaft housing;
a propeller secured to the first end of said propeller drive shaft;
a rotary drive bell having a first end and a second end opposite said first end, with the first end of said drive bell immovably affixed to the first end of said propeller drive shaft in order to rotate with said drive shaft;
an internally toothed ring gear extending from the second end of said drive bell, and circumferentially surrounding said propeller drive shaft housing of said mounting base;
at least one motor immovably affixed to said at least one set of motor mounting lugs of said mounting base, and extending substantially opposite said propeller drive shaft housing;
a motor drive shaft extending from said at least one motor, substantially parallel to said propeller drive shaft housing; and
an externally toothed pinion gear disposed upon said motor drive shaft, and rotationally engaging said internally toothed ring gear of said drive bell for driving said drive bell.
8. The model aircraft powerplant assembly according to claim 7 , wherein:
said at least one set of motor mounting lugs comprises a pair of elongate, parallel arms; and
each of said arms further includes an elongate motor position adjusting slot formed therethrough, whereby said at least one motor is radially adjustable positionally relative to said drive shaft housing and said internally toothed ring gear of said drive bell for adjusting gear lash and changing gear ratios as desired.
9. The model aircraft powerplant assembly according to claim 7 , wherein said at least one set of motor mounting lugs comprises a plurality of sets selected from the group consisting of two, three, and four sets of motor mounting lugs; and
said at least one motor comprises a separate motor adjustably secured to each of the sets of lugs.
10. The model aircraft powerplant assembly according to claim 7 , further including:
an elongate mounting bolt removably disposed through each of said structure attachment passages of said mounting base, and extending generally opposite said drive shaft housing;
an elongate, tubular standoff removably disposed over each said mounting bolt;
each said standoff having a first end adjacent said mounting base, and a second end opposite said first end; and
a standoff pad removably disposed over each said mounting bolt, adjacent the second end of each said standoff.
11. The model aircraft powerplant assembly according to claim 7 , further including:
a first bearing installed within the first end of said drive shaft housing and generally medially about said drive shaft;
a second bearing installed within the second end of said drive shaft housing and about said second end of said drive shaft;
a first retaining clip secured about said drive shaft, adjacent said first bearing; and
a second retaining clip secured about said drive shaft, adjacent said second bearing.
12. The model aircraft powerplant assembly according to claim 7 , further including means for immovably securing said drive bell to said drive shaft.
13. A model aircraft and model aircraft powerplant assembly, comprising in combination:
a powered model aircraft airframe structure;
a model aircraft powerplant mounting assembly attached to said airframe structure and having an elongate propeller drive shaft housing with a first end and a second end opposite the first end;
a generally planar mounting base extending from the second end of said propeller drive shaft housing, formed integrally therewith and substantially normal thereto;
at least one set of motor mounting lugs extending from said mounting base, substantially coplanar with said mounting base;
said mounting base having at least a pair of structure attachment passages formed therethrough, disposed substantially parallel to said propeller drive shaft housing;
a rotary propeller drive shaft having a first end and a second end opposite the first end, the drive shaft within said propeller drive shaft housing with the first end of said drive shaft extending from the first end of said propeller drive shaft housing;
a propeller secured to the first end of said propeller drive shaft;
a rotary drive bell having a first end and a second end opposite the first end, the first end of said drive bell being immovably affixed to said first end of said propeller drive shaft in order to rotate with said drive shaft;
an internally toothed ring gear extending from the second end of said drive bell, and circumferentially surrounding said propeller drive shaft housing of said mounting base;
at least one motor immovably affixed to said at least one set of motor mounting lugs of said mounting base, and extending substantially opposite said propeller drive shaft housing;
a motor drive shaft extending from said at least one motor, substantially parallel to said propeller drive shaft housing; and
an externally toothed pinion gear disposed upon said motor drive shaft, and rotationally engaging said internally toothed ring gear of said drive bell for driving said drive bell.
14. The model aircraft and model aircraft powerplant assembly combination according to claim 13 , wherein:
said at least one set of motor mounting lugs comprises a pair of elongate, parallel arms; and
each of said arms has an elongate motor position adjusting slot formed therethrough, whereby said at least one motor is radially adjustable positionally relative to said drive shaft housing and said internally toothed ring gear of said drive bell for adjusting gear lash and changing gear ratios as desired.
15. The model aircraft and model aircraft powerplant assembly combination according to claim 13 , wherein said at least one set of motor mounting lugs comprises a plurality of sets selected from the group consisting of two, three, and four sets of motor mounting lugs; and
said at least one motor comprises a separate motor adjustably secured to each of the sets of lugs.
16. The model aircraft and model aircraft powerplant assembly combination according to claim 13 , further including:
an elongate mounting bolt removably disposed through each of said structure attachment passages of said mounting base, and extending generally opposite said drive shaft housing;
an elongate, tubular standoff removably disposed over each said mounting bolt;
each said standoff having a first end adjacent said mounting base, and a second end opposite said first end; and
a standoff pad removably disposed over each said mounting bolt, adjacent the second end of each said standoff.
17. The model aircraft and model aircraft powerplant assembly combination according to claim 13 , further including:
a first bearing installed within said first end of said drive shaft housing and generally medially about said drive shaft;
a second bearing installed within said second end of said drive shaft housing and about said second end of said drive shaft;
a first retaining clip secured about said drive shaft, adjacent said first bearing; and
a second retaining clip secured about said drive shaft, adjacent said second bearing.
18. The model aircraft and model aircraft powerplant assembly combination according to claim 13 , further including means for immovably securing said drive bell to said drive shaft.