US4289027A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft fuel tester
Assignee: GLEAVES TOOL Corp
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Filing: 1979-12-20
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Granted: 1981-09-15
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Expires: 1999-12-20
Abstract
Abstract A device to measure both the fuel level in high wing aircraft fuel tanks and check for water and other impurities in the fuel tanks. This invention is used from the underside of the wing and is inserted from below into the fuel tank sump valve. The device measures both the height of the fuel within the tank to determine how full it is and at the same time drains fuel into the device for visual inspection of water and other impurities. The device can be used to determine both fuel level and impurities at the same time or separately.
Inventors
- 👤 Donald Gleaves
- 👤 Walter Green
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 01:46
CPC Classifications
G; G01; G01F; G01F23/00; G01F23/14; G01F23/16; G01F23/164
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
244 words
A guage to measure fuel level in the fuel tanks of high wing airplanes where the gauge used to measure fuel level has a mechanism which is activated by means of the fuel pressure against it and which in turn activates a pointer on a dial which indicates the level of fuel in the tank wherein the improvement comprises: (a) a hollow standpipe, with the upper end narrowing down to a perforated pin slightly smaller than the opening in the fuel tank sump valve, when the pin is pushed into the opening of the wing tank sump valve, and (b) which when pushed into the wing tank sump valve opens the valve sufficiently to allow fuel to flow into the opening in which the pin is inserted and through the perforations in the pin into the hollow standpipe while a collar fits tight against the opening in the valve preventing fluid from leaking out, and (c) and continues to flow down through the standpipe through the opening in the base where it presses against a pressure means mechanism with the full weight of the level of fuel in the fuel tank, and (d) which pressure means mechanism moves an indicator means registering the level of fuel in the wing tank, and (e) which measurement of the fuel level in the high wing fuel tanks is taken by inserting the device into the fuel tank sump valve while standing under the wing of the aircraft.
Claim 2
Dependent Claim
244 words
A guage to measure fuel level in the fuel tanks of high wing airplanes where the gauge used to measure fuel level has a mechanism which is activated by means of the fuel pressure against it and which in turn activates a pointer on a dial which indicates the level of fuel in the tank wherein the improvement comprises: (a) a hollow standpipe, with the upper end narrowing down to a perforated pin slightly smaller than the opening in the fuel tank sump valve, when the pin is pushed into the opening of the wing tank sump valve, and (b) which when pushed into the wing tank sump valve opens the valve sufficiently to allow fuel to flow into the opening in which the pin is inserted and through the perforations in the pin into the hollow standpipe while a collar fits tight against the opening in the valve preventing fluid from leaking out, and (c) and continues to flow down through the standpipe through the opening in the base where it presses against a pressure means mechanism with the full weight of the level of fuel in the fuel tank, and (d) which pressure means mechanism moves an indicator means registering the level of fuel in the wing tank, and (e) which measurement of the fuel level in the high wing fuel tanks is taken by inserting the device into the fuel tank sump valve while standing under the wing of the aircraft.
Claim 3
Dependent Claim
144 words
A gauge to measure fuel level in the fuel tanks of high wing airplanes where the gauge used to measure fuel level has a mechanism means activated by the fuel pressure against it and which has indicator means to register the level of fuel in the tank wherein the improvement comprises: (a) a hollow standpipe with the upper end narrowed and perforated to fit into the fuel tank sump valve, and (b) when pushed upward into the fuel tank sump valve opens the valve draining some of the fuel into the hollow standpipe and down to the base of the standpipe pressing against a pressure mechanism means which pressure mechanism means activates an indicator means registering the amount of fuel in the fuel tank, (c) while at the same time allowing visual inspection of the fluid in the standpipe for water and other pollutants.
Claim 4
Dependent Claim
144 words
A gauge to measure fuel level in the fuel tanks of high wing airplanes where the gauge used to measure fuel level has a mechanism means activated by the fuel pressure against it and which has indicator means to register the level of fuel in the tank wherein the improvement comprises: (a) a hollow standpipe with the upper end narrowed and perforated to fit into the fuel tank sump valve, and (b) when pushed upward into the fuel tank sump valve opens the valve draining some of the fuel into the hollow standpipe and down to the base of the standpipe pressing against a pressure mechanism means which pressure mechanism means activates an indicator means registering the amount of fuel in the fuel tank, (c) while at the same time allowing visual inspection of the fluid in the standpipe for water and other pollutants.
Claim 5
Independent Claim
142 words
A method of measuring the fuel level in the fuel tanks of high wing airplanes using a gauge activated by pressure mechanism means which in turn by indicator means registers the level of fuel in the wing tanks wherein the improvement comprises: (a) standing under the wing tanks of high wing airplanes underneath the fuel tank sump valve, and (b) inserting into the valve of the fuel tank sump a pin both perforated and narrower than the opening into which it is inserted, and (c) draining into the hollow standpipe fuel flowing from the fuel tank sump, and (d) pressing against a pressure mechanism means at the base of the standpipe, and (e) activating an indicator means which registers the fuel level in the tank on a dial means, and (f) inspecting the fuel in the standpipe for water and other pollutants.
Claim 6
Independent Claim
142 words
A method of measuring the fuel level in the fuel tanks of high wing airplanes using a gauge activated by pressure mechanism means which in turn by indicator means registers the level of fuel in the wing tanks wherein the improvement comprises: (a) standing under the wing tanks of high wing airplanes underneath the fuel tank sump valve, and (b) inserting into the valve of the fuel tank sump a pin both perforated and narrower than the opening into which it is inserted, and (c) draining into the hollow standpipe fuel flowing from the fuel tank sump, and (d) pressing against a pressure mechanism means at the base of the standpipe, and (e) activating an indicator means which registers the fuel level in the tank on a dial means, and (f) inspecting the fuel in the standpipe for water and other pollutants.
Claim 7
Dependent Claim
22 words
The claim as recited in claim 1 or claim 2 wherein the standpipe is encased in a transparent cylinder made from Lexan.
Claim 8
Dependent Claim
26 words
The claim as recited in claim 1 or claim 2 wherein the pressure means mechanism consists of a diaphragm which is made of a flexibile material.
Claim 9
Dependent Claim
45 words
The claim as recited in claim 1 or claim 2 wherein the indicator means consist of an arm resting against the diaphragm which when the arm moves turns a gear to which a pointer is attached which moves clockwise around the face of a dial.
Claim 10
Dependent Claim
19 words
The claim as recited in claim 1 or claim 2 wherein the hollow standpipe is made from transparent Lexan.
Claim 11
Dependent Claim
66 words
The claim as recited in claim 1 or claim 2 wherein the indicator means is made fail safe by causing the pointer to be moved clockwise around the face of a dial with the tension in the spring causing the pointer to be set at Empty and then moved by additional pressure on the spring to indicate some level of fuel in the wing fuel tank.
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) | 1984-09-14 | 1985-03-16 | 1985-09-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-09-14 | 1989-03-16 | 1989-09-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-09-14 | 1993-03-16 | 1993-09-15 | $7700.00 | Window Closed / Lapsed |