US4955561A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Cogwheel drive mechanism for aircraft
Assignee: Individual
•
Filing: 1987-08-31
•
Granted: 1990-09-11
•
Expires: 2007-08-31
Abstract
Abstract A cogwheel drive mechanism for driving at least one aircraft propeller or helicopter rotor through two transmissions, with two axially displaced transmission-connection shafts and at least one output shaft in the form of a propeller shaft or rotor shaft. The object is to ensure that at least one driven section will remain fully functional between one of the transmissions and one propeller or the other during any conceivable type of malfunction. There are two spatially separated individual drive mechanisms, each of which is accommodated in a separated housing that accommodates sections of one or both of the output shafts and each of which has one of the two connecting shafts.
Inventors
- 👤 U. C. Seefluth
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 09:06
CPC Classifications
B; B64; B64D; B64D35/00; B64D35/08; Y; Y10; Y10T; Y10T74/00; Y10T74/19; Y10T74/19023; Y10T74/19051; Y10T74/19056; Y10T74/19074; Y10T74/19121
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
118 words
A gear drive arrangement for driving one aircraft propeller or helicopter rotor comprising: two transmissions with two laterally displaced drive shafts and at least one driven shaft connected to a propeller shaft or rotor shaft; said two transmissions comprising two spatially separated individual drive mechanisms; a separate housing for each of said drive mechanisms and housing sections of said driven shaft; each of said drive mechanisms having one of said two drive shafts so that the propeller or rotor is assuredly always driven by one of said drive shafts, all said shafts having longitudinal axes, said two driven shafts and said propeller or rotor shaft being arranged one behind the other in predetermined sequence along said longitudinal axes.
Claim 2
Dependent Claim
118 words
A gear drive arrangement for driving one aircraft propeller or helicopter rotor comprising: two transmissions with two laterally displaced drive shafts and at least one driven shaft connected to a propeller shaft or rotor shaft; said two transmissions comprising two spatially separated individual drive mechanisms; a separate housing for each of said drive mechanisms and housing sections of said driven shaft; each of said drive mechanisms having one of said two drive shafts so that the propeller or rotor is assuredly always driven by one of said drive shafts, all said shafts having longitudinal axes, said two driven shafts and said propeller or rotor shaft being arranged one behind the other in predetermined sequence along said longitudinal axes.
Claim 3
Dependent Claim
19 words
A drive arrangement as defined in claim 1, wherein each housing is separately sealed for preventing loss of lubricant.
Claim 4
Dependent Claim
23 words
A drive arrangement as defined in claim 1, including an idling gear in each individual drive mechanism for preventing rotation in one direction.
Claim 5
Dependent Claim
41 words
A drive arrangement as defined in claim 1, wherein said individual drive mechanisms are adjacent to a propeller, one drive mechanism having a hollow driven shaft, and the other drive mechanism having a driven shaft extending coaxially through said hollow shaft.
Claim 6
Dependent Claim
45 words
A drive arrangement as defined in claim 1, wherein said housings are separated by a substantially narrow space, each housing having a wall bordering said space and facing the other drive mechanism, said two drive mechanisms having their own separate housing wall facing all directions.
Claim 7
Dependent Claim
22 words
A drive arrangement as defined in claim 1, including connecting elements for connecting said separate two housings, said connecting elements being removable.
Claim 8
Dependent Claim
29 words
A drive arrangement as defined in claim 1, wherein said housings have walls facing each other and separated from one another; and impact-absorbing material between said facing housing walls.
Claim 9
Dependent Claim
34 words
A drive arrangement as defined in claim 4, wherein said hollow driven shaft and said coaxial driven shaft of said other drive mechanism are each secured to a propeller shaft by separate fastening means.
Claim 10
Dependent Claim
35 words
A drive arrangement as defined in claim 1, wherein each said housing comprises a sealed subassembly comprised of a single piece of material of a casting; and a housing wall joining said two separate housings.
Claim 11
Dependent Claim
30 words
A drive arrangement as defined in claim 4, including two separately rotating axially displaced propellers driven by said coaxial driven shafts, each driven shaft driving one of said two propellers.
Claim 12
Dependent Claim
34 words
A drive arrangement as defined in claim 4, wherein said hollow driven shaft has journal bearings in the individual drive mechanism adjacent to the propeller and positioned only outside and toward the respective housing.
Claim 13
Dependent Claim
30 words
A drive arrangement as defined in claim 1, wherein said housing comprises two deep-drawn metal halves, said halves being separated by a plane extending at right-angle to the driven shaft.
Claim 14
Dependent Claim
39 words
A drive arrangement as defined in claim 1, wherein each said separate housing also encloses the respective drive mechanism accommodated by the housing, each of said drive shafts extending as an entering shaft through a wall of the housing.
Claim 15
Dependent Claim
32 words
A drive arrangement as defined in claim 1, including a torque-transmitting linkage between one driven shaft and propeller shaft and having individually and spatially separate rotating parts independent of another torque-transmitting means.
Claim 16
Dependent Claim
35 words
A driven arrangement as defined in claim 4, including bearings for supporting each of said coaxial driven shafts with a space between said bearings, each bearing being independent of dynamic actions of the other bearings.
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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) | 1993-09-10 | 1994-03-12 | 1994-09-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-09-10 | 1998-03-12 | 1998-09-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-09-10 | 2002-03-12 | 2002-09-11 | $7700.00 | Window Closed / Lapsed |