Patent US5362205A successfully refreshed from Google Patents.
US5362205A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method and apparatus for synchronizing the speed and phase of plural propellers of an aircraft
Assignee: GE Aviation UK
•
Filing: 1991-08-09
•
Granted: 1994-11-08
•
Expires: 2011-08-09
Abstract
Abstract A propeller control system (1) includes a propeller controller (6) the gain of which is set by a look up table (2) in response to airspeed data supplied by an airspeed detector (4). By varying the gain of the propeller controller (6) an overall system gain can be maintained as the gain of a propeller (7) varies with airspeed.
Inventors
- 👤 Gilbert A. Turner
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 20:23
CPC Classifications
B; B64; B64C; B64C11/00; B64C11/46; B64C11/50
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
112 words
A propeller control system for use with an aircraft having at least two propellers comprising a propeller controller comprising means for producing a first control signal corresponding to the motion of said propellers, said controller further comprising means that processes said first control signal using a variable gain to produce a second control signal suitable for adjusting the movement of at least one of the propellers, and an air speed sensor to sense the forward air speed of said aircraft and produce a forward air speed signal, said controller being responsive to said forward air speed signal to vary the gain of the controller in accordance with said forward air speed signal.
Claim 2
Dependent Claim
112 words
A propeller control system for use with an aircraft having at least two propellers comprising a propeller controller comprising means for producing a first control signal corresponding to the motion of said propellers, said controller further comprising means that processes said first control signal using a variable gain to produce a second control signal suitable for adjusting the movement of at least one of the propellers, and an air speed sensor to sense the forward air speed of said aircraft and produce a forward air speed signal, said controller being responsive to said forward air speed signal to vary the gain of the controller in accordance with said forward air speed signal.
Claim 3
Dependent Claim
54 words
Apparatus as claimed in claim 1, which includes a store containing values of gain against values of forward air speed in the form of a look-up table, the controller selecting gain values from the store in accordance with values of the forward air speed signal and using these to process said first control signal.
Claim 4
Dependent Claim
29 words
Apparatus as claimed in claim 1, in which the controller selects a default gain from the store in the event of the absence of the forward air speed signal.
Claim 5
Dependent Claim
13 words
Apparatus as claimed in claim 1, which controls the phase of the propellers.
Claim 6
Dependent Claim
13 words
Apparatus as claimed in claim 1, which controls the speed of the propellers.
References Cited (Backward Citations)
US4569021A
Cited
EP0008584A1
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1997-11-07 | 1998-05-09 | 1998-11-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2001-11-07 | 2002-05-09 | 2002-11-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2005-11-07 | 2006-05-09 | 2006-11-08 | $7700.00 | Window Closed / Lapsed |