Induction lift flying saucer

• US 4,824,048 A
• Filed: 03/16/1987
• Issued: 04/25/1989
• Est. Priority Date: 03/05/1981
• Status: Expired due to Fees

• Current Assignee: Kyusik Kim
• Original Assignee: Kyusik Kim
• Inventors: Kim, Kyusik
• Primary Examiner(s): BAREFOOT, GALEN L
• Application Number:
  US07/027,174
• Time in Patent Office: 771 Days
• Field of Search: 244/12.1, 244/12.2, 244/23 C, 244/23 R, 244/23 D, 244/12.5, 244/15, 244/12.6, 244/36, 244/207, 244/62, 244/53 R, 244/73 R, 244/74
• US Class Current: 244/12.2
• CPC Class Codes: B64D 27/20 within, or attached to, fuselages
• CPC Class Codes: F02K 3/08 with supplementary heating of the working fluid; Control thereof control of fuel supply therefor F02C9/26

Abstract

An induction lift flying saucer having a circular shaped air frame which houses a vacuum cell induction lift wing adapted to be used in an aerodynamic generating channel wherein the lift wing includes an airfoil having a leading edge and a trailing edge, a top panel and an acoustically treated hollow interior, and wherein the airfoil includes airtight partitions forming individual cells within the hollow interior and the airfoil has inclined slots extending from the top panel into each of the individual cells wherein the inclined slots extend at an angle from each of the individual cells toward the trailing edge of the airfoil and wherein the airfoil is adapted to be positioned within an aerodynamic generating channel with the top panel of the airfoil being adapted to form a lower boundary of the aerodynamic generating channel and to define a slip thereacross from an airstream passing through the aerodynamic generating channel, a bearing support operatively coupled to the airfoil adjacent the trailing edge to enable the airfoil to be rotated therearound to change the angle of incidence of the top panel to an airstream passing thereacross and a pivot support operatively couples to the airfoil adjacent the leading edge for moving the airfoil leading edge relative to an airstream by rotating the airfoil around the support member to change the angle on incidence of a top panel relative to an airstream enabling the airflow thereof to generate a vacuum within the individual cells is shown. A jet thrust peripheral flow recycling system and induction lift aerodynamic generating channel using the vacuum cell induction lift wing is also shown.

Claims

1. An inductive lift flying saucer comprising:

a circular airframe having an aerodynamic outer surface and a central power plant housing section;

an aerodynamic generating channel having an elongated main generating channel located in the central power plant housing section and defined by an inlet adjacent a jet engine which communicates with the main generating channel, an upper portion defining a reverse flow channel and wherein the lower portion and outlet of the main generating channel is opened and is part of said main generating channel;

a vacuum cell induction lift wing airfoil including a leading edge and a trailing edge and having a top panel and an acoustically treated hollow interior, said airfoil including airtight partitions forming individual cells within said hollow interior and having inclined slots which extend from the top panel of said airfoil into each of said individual cells, said inclined slots extending at an angle from each of said individual cells toward the trailing edge of said airfoil, said airfoil being adapted to be positioned within an aerodynamic generating channel in the lower portion thereof and spaced from the upper portion forming said elongated channel with the top panel of the airfoil being adapted to form a lower boundary of a said aerodynamic generating and forming an outlet for the main generating generating channel between the trailing edge of the airfoil and the rearward section of the upper portion forming the reverse flow channel and being adapted to define a slipflow thereacross from an airstream passing through a said aerodynamic generating channel;

support means operatively coupled to said airfoil adjacent the trailing edge for enabling said airfoil to be rotated therearound to change the angle of incidence of the top panel to a said airstream passing thereacross; and

pivoting means actuators operatively coupled to said airfoil adjacent the leading edge for moving said airfoil leading edge relative to a said airstream by rotating said airfoil around said support means to change the angle of incidence of said top panel relative a said airstream enabling a said airflow to generate a vacuum within said individual cells having a pressure which is determined by the angle of incidence of the top panel of the airfoil to the said airstream and by the shearing stress of a said airstream passing over said inclined slots in the top panel of said airfoil.

2. An inductive lift flying saucer comprising:

a circular airframe having an aerodynamic outer surface and a central power plant housing section;

a jet engine producing a jet thrust stream having a thrust nozzle located in the central power plant section;

a jet thrust peripheral flow recycling system located rearward of and adjacent to the thrust nozzle, said jet thrust peripheral flow recycling system comprising;

a housing defining an aerodynamic generating channel adapted to pass a jet thrust stream from the thrust nozzle of said jet engine therethrough, said housing including a main generating channel having an inlet and an outlet and a reverse flow channel located in the upper portion of the main generating channel channel and separated from the main generating channel by an acoustically treated panel having inclined orifices which are directed towards this outlet, said reverse flow channel having an inlet opening located at the outlet of the main generating channel and an outlet opening located adjacent the inlet of the main generating channel, said inclined orifices being operative to provide a slipflow for a said jet thrust stream passing through the main channel;

a vacuum induction lift wing airfoil including a leading edge and a trailing edge and having a top panel and an acoustically treated hollow interior, said airfoil including airtight partitions forming individual cells within said hollow interior and having inclined slots which extend from the top panel of said airfoil into each of said individual cells, said inclined slots extending at an angle from each of said individual cells toward the trailing edge of said airfoil, said airfoil being positioned within an aerodynamic generating channel with the top panel of the airfoil being adapted to form a lower boundary of a said aerodynamic generating channel and being adapted to define a slipflow thereacross from an airstream passing through a said aerodynamic generating channel;

support means operatively coupled to said airfoil adjacent the trailing edge for enabling said airfoil to be rotated therearound to change the angle of incidence of the top panel to a said airstream passing thereacross; and

pivoting means actuators operatively coupled to said airfoil adjacent the leading edge for moving said airfoil leading edge relative to a said airstream by rotating said airfoil around said support means to change the angle of incidence of said top panel relative a said airstream enabling a said airflow to generate a vacuum within said individual cells having a pressure which is determined by the angle of incidence of the top panel of the airfoil to the said airstream and by the shearing stress of a said airstream passing over said inclined slots in the top panel of said airfoil;

reverse flow turning vanes located in the inlet of the reverse flow channel and being adapted to divert a portion of a said jet thrust stream passing through said reverse flow channel back into the main generating channel; and

actuators operatively coupled to said reverse flow vanes for controlling the position of the reverse flow turning vanes relative to a said jet thrust stream passing through the main generating channel to regulate the volume of a said jet thrust stream being diverted into and passing through said reverse flow channel.

3. An inductive lift flying saucer comprising:

a circular airframe having an aerodynamic outer surface and a central power plant housing section;

a jet engine producing a jet thrust stream having a thrust nozzle located in the central power plant section;

an induction aerodynamic lift generating appararus located rearward of and adjacent to the thrust nozzle of the jet engine producing a jet thrust stream comprising;

a housing defining an aerodynamic generating channel having an elongated main generating channel defined by an inlet adjacent a jet engine which communicates with the main generating channel, an upper portion defining a reverse flow channel and wherein the lower portion and outlet of the main generating channel is opened and is part of said main generating channel adapted to pass a jet thrust stream through including said main generating channel having said inlet and an outlet and said reverse flow channel located in the upper portion of the main generating channel channel and separated from the main generating channel by a panel, said reverse flow channel having an inlet opening located at the outlet of the main generating channel and an outlet opening located adjacent the inlet of the main generating channel;

an airfoil including a leading edge and a trailing edge and having a top panel and an acoustically treated hollow interior, said airfoil including airtight partitions forming individual cells within said hollow interior and having inclined slots which extend from the top panel of said airfoil into each of said individual cells, said inclined slots extending at an angle from each of said individual cells toward the trailing edge of said airfoil, said airfoil being adapted to be positioned within said aerodynamic generating channel in the lower portion thereof and spaced from the upper portion forming said elongated channel with the top panel of the airfoil being adapted to form a lower boundary of a said aerodynamic generating and forming an outlet for the main generating generating channel between the trailing edge of the airfoil and the rearward section of the upper portion forming the reverse flow channel and being adapted to define a slipflow thereacross from a jet thrust stream passing through a said aerodynamic generating channel;

support means operatively coupled to said airfoil adjacent the trailing edge for enabling said airfoil to be rotated therearound to change the angle of incidence of the top panel to a said jet thrust stream passing thereacross; and

pivoting means actuators operatively coupled to said airfoil adjacent the leading edge for moving said airfoil leading edge relative to a said jet thrust stream by rotating said airfoil around said support means to change the angle of incidence of said top panel relative a said jet thrust stream causing a said airflow to generate a vacuum within said individual cells having a pressure which is determined by the angle of incidence of the top panel of the airfoil to the said jet thrust stream and by the shearing stress of a said jet thrust stream passing over said inclined slots in the top panel of said airfoil, said jet thrust stream being adapted to pass through the aerodynamic generating channel and over the top surface of the vacuum cell induction lift wing for producing thermal aerodynamic lift and drag forces which are determined by the angle of incidence of said vacuum cell induction lift wing and that portion of said jet thrust stream being diverted into and passing through said jet thrust stream being diverted into and passing through the reverse flow channel and back into the main generating channel.