US4490802A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Takeoff weight computer apparatus for aircraft
Assignee: Honeywell Inc
•
Filing: 1981-12-21
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Granted: 1984-12-25
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Expires: 2001-12-21
Abstract
Abstract The takeoff weight of an aircraft is computed from measures of the thrust of the engines and the forward acceleration of the aircraft detected over a time period when such acceleration is at a maximum following brake release on the runway. A major variable that must be considered is the coefficient of rolling friction of the landing gear of the particular aircraft involved and other factors inducing ground roll drag. The present invention calculated this variable as a function of engine thrust and manifest weight for each takeoff of the aircraft and updates weighted filter values thereof for use during subsequent takeoffs. For each takeoff, therefore, and average value of rolling friction is used to calculate takeoff weight, which average value becomes more nearly the actual value for the existing condition of the landing gear.
Inventors
- 👤 Harry Miller
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 22:28
CPC Classifications
G; G01; G01G; G01G19/00; G01G19/02; G01G19/07
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
101 words
Apparatus for providing a measure of actual takeoff weight of an aircraft, comprising: means for providing a measure of engine thrust of said aircraft, means for providing a measure of longitudinal acceleration of said aircraft, means for providing a measure of rolling friction of said aircraft, which measure is an average value of a plurality of rolling friction measures obtained over a plurality of prior aircraft takeoffs, and means responsive to said measures of thrust, acceleration and friction for providing an output measure of said takeoff weight of said aircraft as a predetermined function of said thrust, acceleration and friction measures.
Claim 2
Dependent Claim
101 words
Apparatus for providing a measure of actual takeoff weight of an aircraft, comprising: means for providing a measure of engine thrust of said aircraft, means for providing a measure of longitudinal acceleration of said aircraft, means for providing a measure of rolling friction of said aircraft, which measure is an average value of a plurality of rolling friction measures obtained over a plurality of prior aircraft takeoffs, and means responsive to said measures of thrust, acceleration and friction for providing an output measure of said takeoff weight of said aircraft as a predetermined function of said thrust, acceleration and friction measures.
Claim 3
Dependent Claim
54 words
The apparatus as set forth in claim 1 wherein said predetermined function is of the form ##EQU5## wherein: ______________________________________
W = actual aircraft takeoff weight
T = engine thrust imparted to said aircraft
a.sub.x =
longitudinal acceleration of said aircraft
g = gravity acceleration
μ.sub.AV =
average value of said aircraft rolling friction.
______________________________________
Claim 4
Dependent Claim
62 words
The apparatus as set forth in claim 1 wherein said rolling friction measure providing means comprises: means for providing a measure of the estimate takeoff weight of the aircraft for a present takeoff, and means responsive to said estimated aircraft weight measure for providing a measure of the present rolling friction as a function of said thrust, acceleration and estimated weight measures.
Claim 5
Dependent Claim
73 words
The apparatus as set forth in claim 3 wherein said predetermined function is of the form of ##EQU6## wherein: ______________________________________
μ = a measure of the value of the rolling friction
of said aircraft at a specific takeoff
W.sub.M =
the estimated weight of the aircraft at a
specific takeoff
T = the thrust imparted to the aircraft by the
engines
a.sub.x =
longitudinal acceleration of the aircraft
g = gravity acceleration.
______________________________________
Claim 6
Dependent Claim
18 words
The apparatus as set forth in claim 3 wherein said estimated aircraft takeoff weight is the manifest weight.
Claim 7
Dependent Claim
64 words
The apparatus as set forth in claim 5 wherein said value of rolling friction measure providing means further includes weighted filter means responsive to said present and a plurality of past rolling friction measures for providing a weighted average of said rolling friction measures wherein the values of said plurality of past measures are weighted more heavily than the values of said present measure.
Claim 8
Dependent Claim
43 words
The apparatus as set forth in claim 6 wherein said rolling friction measure providing means further includes comparator means responsive to said present rolling friction measure said weighted filter measure for rejecting predetermined values of said present measure from said weighted filter means.
Claim 9
Dependent Claim
20 words
The apparatus as set forth in claim 7 further comprising maintenance recorder means responsive to said rejected rolling friction measure.
References Cited (Backward Citations)
US4018111A
Cited
US4110605A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-12-25 | 1988-06-25 | 1988-12-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-12-25 | 1992-06-25 | 1992-12-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-12-25 | 1996-06-25 | 1996-12-25 | $7700.00 | Window Closed / Lapsed |