US4604526A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Position detector
Assignee: Micro Control Technology Ltd
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Filing: 1983-11-09
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Granted: 1986-08-05
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Expires: 2003-11-09
Abstract
Abstract A detector for checking the symmetry of a helicopter rotor while it is rotating has a scanner (11) which scans vertically a field of view (15) and the view is interrupted by a vertical strip on the blade tip (16). A slot (18) in the strip gives a characteristic signal as at (L2). The position of the signal (L2) in a scanning cycle gives an indication of the height of the blade tip and also the circumferential spacing between blades.
Inventors
- 👤 Christopher I. Moir
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 04:24
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/008; G; G01; G01B; G01B11/00; G01B11/16; G01M; G01M5/00
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
110 words
A position detector comprising means defining an elongate field of view, for viewing a target which is arranged to cross the field of view in any of a range of positions along the length of the field of view and having a reference part, a sensor in the form of a line of sensitive elements extending parallel with the field of view and positioned to receive an image of the field of view, and electronic means for repeatedly scanning the elements in scanning cycles and for detecting the particular sensitive element which receives the image of the reference part of the target as the target crosses the field of view.
Claim 2
Dependent Claim
110 words
A position detector comprising means defining an elongate field of view, for viewing a target which is arranged to cross the field of view in any of a range of positions along the length of the field of view and having a reference part, a sensor in the form of a line of sensitive elements extending parallel with the field of view and positioned to receive an image of the field of view, and electronic means for repeatedly scanning the elements in scanning cycles and for detecting the particular sensitive element which receives the image of the reference part of the target as the target crosses the field of view.
Claim 3
Dependent Claim
23 words
A detector as claimed in claim 1, in which the target is fixed to a rotor blade, whose position is to be detected.
Claim 4
Dependent Claim
28 words
A detector as claimed in claim 1, in which the target comprises a blade of a helicopter rotor and the reference part is the edge of the blade.
Claim 5
Dependent Claim
27 words
A detector as claimed in claim 1, in which the reference part is a slot extending perpendicularly to the length of elongation of the field of view.
Claim 6
Dependent Claim
43 words
A detector as claimed in claim 4, in which said reference part is a reflecting line and further including a source of radiation to which the sensor is sensitive for illuminating the reflecting line when the target is in the field of view.
Claim 7
Dependent Claim
21 words
A detector as claimed in claim 1, in which the means defining the elongate field of view comprises an elongate lens.
Claim 8
Dependent Claim
35 words
A detector as claimed in claim 1, further including computer means connected to receive the output from the sensor and including means for computing the position of the reference part in the field of view.
Claim 9
Dependent Claim
48 words
A detector as claimed in claim 7 in combination with a helicopter rotor and having means for generating a reference signal once per rotor revolution, and in which the computer means includes means for computing the circumferential position of each rotor blade in relation to the reference signal.
Claim 10
Independent Claim
74 words
A method of testing a helicopter rotor having blades in which a thin, generally vertical elongate field of view is defined, the rotor is rotated so that the blades in turn cross the vertical field of view, a multi-element sensor extending parallel with the field of view is repeatedly scanned in scanning cycles, and the position of the various blades in the field of view are computed from signals derived during the scanning cycles.
Claim 11
Independent Claim
74 words
A method of testing a helicopter rotor having blades in which a thin, generally vertical elongate field of view is defined, the rotor is rotated so that the blades in turn cross the vertical field of view, a multi-element sensor extending parallel with the field of view is repeatedly scanned in scanning cycles, and the position of the various blades in the field of view are computed from signals derived during the scanning cycles.
Claim 12
Dependent Claim
29 words
A method as claimed in claim 9, in which the scanning cycle is fast in relation to the time taken for a blade to cross the field of view.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-08-04 | 1990-02-03 | 1990-08-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-08-04 | 1994-02-03 | 1994-08-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-08-04 | 1998-02-03 | 1998-08-05 | $7700.00 | Window Closed / Lapsed |