US3942376A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Diaphragm type angle of attack indicator
Assignee: Individual
•
Filing: 1974-08-14
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Granted: 1976-03-09
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Expires: 1994-08-14
Abstract
Abstract An angle of attack indicator for use as a cockpit instrument including movable variable-area diaphragms which respond to the differences in pressure at selected points on the aircraft. The pressure points may include the total pressure sensed by the aircraft pitot tube and two other pressures at least one of which varies strongly with the angle of attack. The mechanism divides the difference between total pressure and one of the other two pressures by the difference between the total pressure and the other of the other two pressures obtaining a pressure coefficient which depends only on the shape and angle of attack of the aircraft. The use of the variable diaphragm as the sensitive element of a low level pressure sensor as in an aircraft airspeed indicator is described.
Inventors
- 👤 Roger W. Gallington
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 23:21
CPC Classifications
B; B64; B64D; B64D43/00; B64D43/02
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
278 words
A diaphragm type angle of attack indicator for use as an aircraft instrument comprising, means for sensing three pressures on the aircraft, at least one of said three pressures varying strongly with angle of attack, another of said three pressures being greater than the other two pressures, tubing means for transmitting the pressures to a central area, and means at the central area for dividing the difference between the greatest pressure and one of the two lesser pressures by the difference between the greatest pressure and the other of the two lesser pressures, said dividing means including an enclosure having three operatively connected sections, pressure from a different point on the aircraft being transferred to each of the sections in said enclosure, the first of the sections being operatively connected to one of the two lesser pressures, the second of the sections being operatively connected to the other of the two lesser pressures, the third of the sections being operatively connected to the greatest pressure, a pair of rigid, members shaped as surfaces of revolution, one each being positioned in each of the first and second sections and having their apexes fixedly attached to each other, a pair of flexible plastic diaphragms positioned in the third section one each being in contact with the back surface of each of said rigid members, said flexible diaphragms effectively separating the third section from the first and second sections, such that changes in pressure in the first and second sections produces a lateral movement in said pair of rigid members, said movement corresponding to the difference in pressures at pressure points on the aircraft and to the angle of attack thereof.
Claim 2
Dependent Claim
278 words
A diaphragm type angle of attack indicator for use as an aircraft instrument comprising, means for sensing three pressures on the aircraft, at least one of said three pressures varying strongly with angle of attack, another of said three pressures being greater than the other two pressures, tubing means for transmitting the pressures to a central area, and means at the central area for dividing the difference between the greatest pressure and one of the two lesser pressures by the difference between the greatest pressure and the other of the two lesser pressures, said dividing means including an enclosure having three operatively connected sections, pressure from a different point on the aircraft being transferred to each of the sections in said enclosure, the first of the sections being operatively connected to one of the two lesser pressures, the second of the sections being operatively connected to the other of the two lesser pressures, the third of the sections being operatively connected to the greatest pressure, a pair of rigid, members shaped as surfaces of revolution, one each being positioned in each of the first and second sections and having their apexes fixedly attached to each other, a pair of flexible plastic diaphragms positioned in the third section one each being in contact with the back surface of each of said rigid members, said flexible diaphragms effectively separating the third section from the first and second sections, such that changes in pressure in the first and second sections produces a lateral movement in said pair of rigid members, said movement corresponding to the difference in pressures at pressure points on the aircraft and to the angle of attack thereof.
Claim 3
Dependent Claim
26 words
The diaphragm type angle of attack indicator defined in claim 1 wherein said pair of flexible plastic diaphragms are formed of high strength clear plastic film.
Claim 4
Dependent Claim
70 words
The diaphragm type angle of attack indicator defined in claim 2 wherein the pressure in the third section causes said clear plastic film to be pressed against said rigid members and roll therewith as the rigid members move laterally in response to pressure changes in the second section to expose varying areas of the rigid members to the pressure differences between the sections thereby maintaining the rigid members in equilibrium.
Claim 5
Dependent Claim
68 words
The diaphragm type angle of attack indicator defined in claim 3 wherein a connecting rod is connected to one of said rigid members for lateral movement therewith, a crank mechanism pivotably connected to the outer end of said connecting rod, and an indicator needle attached to said crank mechanism for movement therewith to convert the linear movement of the rigid members to rotary motion of the indicating needle.
Claim 6
Dependent Claim
57 words
The diaphragm type angle of attack indicator defined in claim 3 wherein the rigid members are joined at their apexes by a string wrapped around a shaft and an indicating needle attached to said shaft for movement therewith such that lateral movement of said rigid members produces a corresponding rotary motion of said shaft and indicating needle.
References Cited (Backward Citations)
US2948149A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-03-09 | 1979-09-08 | 1980-03-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-03-09 | 1983-09-08 | 1984-03-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-03-09 | 1987-09-08 | 1988-03-09 | $7700.00 | Window Closed / Lapsed |