Patent US3629861A successfully refreshed from Google Patents.
Patent US4886224A successfully refreshed from Google Patents.
US4886224A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft lift mechanism
Assignee: Individual
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Filing: 1988-09-15
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Granted: 1989-12-12
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Expires: 2008-09-15
Abstract
Abstract An apparatus for producing lift in a flying vehicle comprising a top deck of a flying vehicle having a cylindrical well formed thereinto, a discoidal member positioned within the cylindrical well, an air intake system formed in the center of the discoidal member for drawing air through the discoidal member for use elsewhere in the flying vehicle, and a labyrinth member formed on the periphery of the discoidal member for restricting the clearance between the discoidal member and the wall of the cylindrical well. The discoidal member is adapted and powered for rotating within the well. The top deck has a generally flat exterior surface. A fluid passageway extends through the interior of the flying vehicle for passing air from the air intake system. The discoidal member has a flat top surface generally parallel to the top deck of the flying vehicle. The top surface of the discoidal member is positioned within the well below the upper surface of the top deck. A second discoidal member is positioned within the fluid passageway at a location adjacent the bottom of the well. The second discoidal member is coaxial with the first discoidal member and connected by a common spindle. The common spindle is rotatably powered by the prime mover means. The labyrinth comprises of plurality of rimmed cavities positioned so as to be in close proximity with the wall of the well for the first discoidal member and the wall of the fluid passageway for the second discoidal member.
Inventors
- 👤 Mario G. Joy
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 19:31
CPC Classifications
B; B64; B64C; B64C29/00; B64C29/0008; B64C29/0016; B64C29/0025; B64C11/00; B64C11/007
Claims Analysis
Total Claims: 23
Claim 1
Independent Claim
98 words
An apparatus for producing lift for a flying vehicle comprising: a top deck of a flying vehicle having a cylindrical well formed thereinto; a discoidal member positioned within said cylindrical well, said discoidal member adapted and powered for rotating within said well; air intake means formed in the center of said discoidal member, said air intake means for drawing air through said discoidal member for use elsewhere in said flying vehicle; and a labyrinth member formed on the periphery of said discoidal member for restricting the clearance between said discoidal member and the wall of said cylindrical well.
Claim 2
Independent Claim
98 words
An apparatus for producing lift for a flying vehicle comprising: a top deck of a flying vehicle having a cylindrical well formed thereinto; a discoidal member positioned within said cylindrical well, said discoidal member adapted and powered for rotating within said well; air intake means formed in the center of said discoidal member, said air intake means for drawing air through said discoidal member for use elsewhere in said flying vehicle; and a labyrinth member formed on the periphery of said discoidal member for restricting the clearance between said discoidal member and the wall of said cylindrical well.
Claim 3
Dependent Claim
25 words
The apparatus of claim 1, said top deck having a generally flat exterior surface, said cylindrical well formed in the area of said flat surface.
Claim 4
Dependent Claim
37 words
The apparatus of claim 1, further comprising: a fluid passageway extending through the interior of said flying vehicle for passing said air from said air intake means, said fluid passageway opening at the bottom of said well.
Claim 5
Dependent Claim
36 words
The apparatus of claim 3, said fluid passageway arranged within said flying vehicle so as to transmit said air to a turbine said turbine positioned at the end of said fluid passageway opposite said cylindrical well.
Claim 6
Dependent Claim
31 words
The apparatus of claim 4, said turbine positioned for providing forward thrust to said flying vehicle, said turbine having an axis offset by ninety degrees from the axis of said well.
Claim 7
Dependent Claim
28 words
The apparatus of claim 4, said turbine positioned for providing upward thrust to said flying vehicle, said turbine having an axis aligned with the axis of said well.
Claim 8
Dependent Claim
42 words
The apparatus of claim 1, said discoidal member having a flat top surface generally parallel to said top deck of said flying vehicle, said top surface of said discoidal member positioned within said well below the upper surface of said top deck.
Claim 9
Dependent Claim
43 words
The apparatus of claim 1, said discoidal member having a nether surface within said well fitted with a blade adjacent the rim of said disc adapted to produce an accentuated reduction of pressure between said nether surface and the floor of said well.
Claim 10
Dependent Claim
39 words
The apparatus of claim 8, said labyrinth member positioned on the end of said blade at the rim of said discoidal member, said labyrinth member for sealing the area between said nether surface and the floor of said well.
Claim 11
Dependent Claim
36 words
The apparatus of claim 9, said labyrinth member comprising a plurality of rimmed cavities extending outwardly from the rim of said discoidal member so as to be in close proximity to said wall of said well.
Claim 12
Dependent Claim
41 words
The apparatus of claim 1, said air intake means comprising: a plurality of vent members extending across the center of said discoidal member so as to draw air through the center of said discoidal member during rotation of said discoidal member.
Claim 13
Dependent Claim
27 words
The apparatus of claim 11, said vent members extending radially outwardly from the center of said discoidal member, said vent members having a curved downwardly spiralling configuration.
Claim 14
Dependent Claim
49 words
The apparatus of claim 3, further comprising: prime mover means for providing powered rotation to said discoidal member, said prime mover means positioned within said fluid passageway and having a spindle connected to the center of said discoidal member, said spindle rotatable with respect to said prime mover means.
Claim 15
Dependent Claim
36 words
The apparatus of claim 3, further comprising: a second discoidal member positioned within said fluid passageway at a location adjacent the bottom of said well, said second discoidal member being coaxial with said first discoidal member.
Claim 16
Dependent Claim
36 words
The apparatus of claim 14, said second discoidal member having a labyrinth on the periphery of said second discoidal member for restricting the clearance between said second discoidal member and the wall of said fluid passageway.
Claim 17
Dependent Claim
48 words
The apparatus of claim 15, said labyrinth of said second discoidal member comprising a plurality of rimmed cavities extending outwardly from the rim of said second discoidal member so as to be in close proximity to the wall of said fluid passageway adjacent the bottom of said well.
Claim 18
Dependent Claim
35 words
The apparatus of claim 16, said labyrinth of said second discoidal member for sealing the area between a nether surface of said first discoidal member and the floor of said well from said fluid passageway.
Claim 19
Dependent Claim
51 words
The apparatus of claim 14, said second discoidal member having a plurality of vents formed therein for passing air to said fluid passageway, said second discoidal member having a smaller diameter than said first discoidal member, said second discoidal member and said first discoidal member powered by a primer mover means.
Claim 20
Dependent Claim
126 words
A flying vehicle comprising: a generally flat top deck connected to a body, said top deck forming the wings of said flying vehicle; a tail section connected to said top deck for stabilizing and controlling aircraft attitude; a discoidal member positioned in a cylindrical well formed in said top deck, said discoidal member adapted and powered for rotating within said well, said discoidal member rotating with restricted clearance from the wall of said cylindrical well; air intake means formed in the central portion of said discoidal member for drawing air into and through said discoidal member; and thruster means connected to said body for providing forward movement to said flying vehicle, said thruster means communicating with said air intake means by way of a fluid passageway.
Claim 21
Dependent Claim
126 words
A flying vehicle comprising: a generally flat top deck connected to a body, said top deck forming the wings of said flying vehicle; a tail section connected to said top deck for stabilizing and controlling aircraft attitude; a discoidal member positioned in a cylindrical well formed in said top deck, said discoidal member adapted and powered for rotating within said well, said discoidal member rotating with restricted clearance from the wall of said cylindrical well; air intake means formed in the central portion of said discoidal member for drawing air into and through said discoidal member; and thruster means connected to said body for providing forward movement to said flying vehicle, said thruster means communicating with said air intake means by way of a fluid passageway.
Claim 22
Dependent Claim
204 words
The vehicle of claim 19, said thruster means being a turbine having an inlet opening to the end of said fluid passageway opposite said air intake means, said discoidal member having a nether surface within said well fitted with a blade adjacent the rim of said discoidal member adapted to produce an accentuated reduction of pressure between said nether surface and the floor of said well, said air intake means comprising a plurality of vent members extending across the center of said discoidal member so as to draw air through the center of said discoidal member during rotation of said discoidal member, said flying vehicle further comprising: a second discoidal member positioned within said fluid passageway at a location adjacent the bottom of said well, said second discoidal member being coaxial with said first discoidal member, said first discoidal member and said second discoidal member connected by a common spindle, said second discoidal member having a plurality of vents formed therein for passing air to said fluid passageway, said second discoidal member having a smaller diameter than said first discoidal member, said spindle being powered for rotation by a prime mover means so as to impart rotation to said first and second discoidal members.
Claim 23
Dependent Claim
129 words
The flying vehicle of claim 20, further comprising: a labyrinth member formed on the periphery of said first discoidal member for restricting the clearance between said discoidal member and the wall of said cylindrical well, said labyrinth member positioned on the end of said blade at the rim of said discoidal member, said labyrinth member sealing the area between said nether surface and the floor of said well, said second discoidal member having a labyrinth on the periphery of said second discoidal member for restricting the clearance between said second discoidal member and the wall of said fluid passageway, said labyrinth of said second discoidal member for sealing the area between said nether surface of said first discoidal member and the floor of said well from said fluid passageway.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1992-12-11 | 1993-06-12 | 1993-12-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-12-11 | 1997-06-12 | 1997-12-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-12-11 | 2001-06-12 | 2001-12-12 | $7700.00 | Window Closed / Lapsed |