US4962641A — Pulse jet engine

Claim 1

Independent Claim 143 words

In a reaction thrust propulsion engine having a forward end combustion chamber section, a rear end afterbody and a resonator tube extending rearwardly from the combustion chamber section to the afterbody, a tail section operatively interconnecting the resonator tube and the afterbody, comprising passage means establishing fluid communication between the resonator tube and the afterbody for cyclically pressurizing the afterbody with combustion supporting air compressed within the resonator tube in response to generation of combustion products within the combustion chamber section, nozzle means for sequentially discharging the combustion products from the resonator tube and conducting an inflow of external reentry air to the resonator tube and ram-air intake means responsive to forward movement of the engine for regulating said pressurization of the afterbody and refill of the resonator tube by inflow of the compressed air from the pressurized afterbody and the reentry air.

Claim 2

Dependent Claim 143 words

In a reaction thrust propulsion engine having a forward end combustion chamber section, a rear end afterbody and a resonator tube extending rearwardly from the combustion chamber section to the afterbody, a tail section operatively interconnecting the resonator tube and the afterbody, comprising passage means establishing fluid communication between the resonator tube and the afterbody for cyclically pressurizing the afterbody with combustion supporting air compressed within the resonator tube in response to generation of combustion products within the combustion chamber section, nozzle means for sequentially discharging the combustion products from the resonator tube and conducting an inflow of external reentry air to the resonator tube and ram-air intake means responsive to forward movement of the engine for regulating said pressurization of the afterbody and refill of the resonator tube by inflow of the compressed air from the pressurized afterbody and the reentry air.

Claim 3

Dependent Claim 63 words

The combination of claim 1 wherein said passage means includes a flow diffusing section having opposite ends respectively spaced from the resonator tube and connected to the afterbody and wall means interconnecting the resonator tube and the flow diffusing section for separating said fluid communication between the resonator tube and the flow diffusing section from the ram-air intake means within the tail section.

Claim 4

Dependent Claim 38 words

The combination of claim 2 wherein said ram-air intake means includes an external casing from which the nozzle means projects and a rear end portion of the flow diffusing section enclosed within the casing having inflow orifice openings.

Claim 5

Dependent Claim 51 words

The combination of claim 3 wherein said nozzle means includes a plurality of rearwardly diverging nozzle formations interconnected by the wall means and projecting radially outward from the casing, each of said nozzle formations having a rearwardly opening port and a nozzle passage extending between the port and the passage means.

Claim 6

Dependent Claim 63 words

The combination of claim 2 wherein said nozzle means includes a plurality of rearwardly diverging nozzle formations interconnected by the wall means and projecting radially outward therefrom to act as ram air intake vanes guiding airflow along the wall means, each of said nozzle formations having a rearwardly opening port and a nozzle passage extending forwardly from the port to the passage means.

Claim 7

Dependent Claim 35 words

The combination of claim 5 wherein said ram-air intake means comprises a rear end portion of the flow diffusing section having inflow orifice openings in operative alignment with said guided airflow between the nozzle formations.

Claim 8

Dependent Claim 132 words

In a pulse-jet engine having a resonator tube from which an air column is rearwardly displaced under compression by heated and expanding combustion products in cyclic relation to refill thereof with combustion supporting air, a tail section connected to the resonator tube comprising a flow diffusing section, passage enclosing wall means interconnecting the resonator tube and the flow diffusing section for decelerated outflow of the rearwardly displaced air column from the resonator tube through the flow diffusing section, nozzle means mounted on the wall means for externally discharging the combustion products from the resonator tube following said decelerated outflow of the air column through the flow diffusing section and orifice means mounted on the flow diffusing section for regulating said refill of the resonator tube following said discharge of the combustion products.

Claim 9

Dependent Claim 132 words

In a pulse-jet engine having a resonator tube from which an air column is rearwardly displaced under compression by heated and expanding combustion products in cyclic relation to refill thereof with combustion supporting air, a tail section connected to the resonator tube comprising a flow diffusing section, passage enclosing wall means interconnecting the resonator tube and the flow diffusing section for decelerated outflow of the rearwardly displaced air column from the resonator tube through the flow diffusing section, nozzle means mounted on the wall means for externally discharging the combustion products from the resonator tube following said decelerated outflow of the air column through the flow diffusing section and orifice means mounted on the flow diffusing section for regulating said refill of the resonator tube following said discharge of the combustion products.

Claim 10

Dependent Claim 48 words

The combination of claim 7 wherein said nozzle means comprises a plurality of angularly spaced vane formations through which nozzle passages extend, respectively, in fluid communication with the resonator tube, said vane formations having rearwardly opening ports terminating the nozzle passages in non-interfering relation to the orifice means.

Claim 11

Dependent Claim 36 words

The combination of claim 8 wherein said orifice means comprises a plurality of flow restricting openings angularly spaced between the vane formations in a surface portion of the flow diffusing section rearwardly of the nozzle means.

Claim 12

Dependent Claim 30 words

The combination of claim 7 wherein said orifice means comprises a plurality of flow restricting openings in a surface portion of the flow diffusing section rearwardly of the nozzle means.

Claim 13

Dependent Claim 21 words

The combination of claim 10 including ram-air intake means for guiding airflow along the wall means into the flow restricting openings.

Claim 14

Dependent Claim 25 words

The combination of claim 7 including ram-air intake means mounted on the nozzle means for guiding airflow along the wall means into the orifice means.

Claim 15

Dependent Claim 142 words

In a reaction thrust propulsion engine having a forward end combustion chamber section, a rear end afterbody and a resonator tube extending rearwardly from the combustion chamber section to the afterbody, a tail section operatively interconnecting the resonator tube and the afterbody, comprising passage means establishing fluid communication between the resonator tube and the afterbody for cyclically pressurizing the afterbody with combustion supporting air compressed within the resonator tube in response to generation of combustion products within the combustion chamber section, nozzle means for sequentially discharging the combustion products from the resonator tube and conducting an inflow of external reentry air to the resonator tube and intake means through which an inflow of pressurized air is conducted for regulating said pressurization of the afterbody and refill of the resonator tube by the compressed air from the pressurized afterbody and the reentry air.

Claim 16

Dependent Claim 142 words

In a reaction thrust propulsion engine having a forward end combustion chamber section, a rear end afterbody and a resonator tube extending rearwardly from the combustion chamber section to the afterbody, a tail section operatively interconnecting the resonator tube and the afterbody, comprising passage means establishing fluid communication between the resonator tube and the afterbody for cyclically pressurizing the afterbody with combustion supporting air compressed within the resonator tube in response to generation of combustion products within the combustion chamber section, nozzle means for sequentially discharging the combustion products from the resonator tube and conducting an inflow of external reentry air to the resonator tube and intake means through which an inflow of pressurized air is conducted for regulating said pressurization of the afterbody and refill of the resonator tube by the compressed air from the pressurized afterbody and the reentry air.

Claim 17

Dependent Claim 63 words

The combination of claim 13 wherein said passage means includes a flow diffusing section having opposite ends respectively spaced from the resonator tube and connected to the afterbody and wall means interconnecting the resonator tube and the flow diffusing section for separating said fluid communication between the resonator tube and the flow diffusing section from the ram-air intake means within the tail section.

Claim 18

Dependent Claim 45 words

The combination of claim 13 wherein said flow diffusing section has inflow orifice openings and said intake means includes an external casing having a forward inlet end portion and a rear end portion connected to the afterbody in enclosing relation to the inflow orifice openings.

Claim 19

Dependent Claim 35 words

The combination of claim 15 including ram-air inlet valve means mounted within the inlet end portion of the casing for receiving said inflow of the pressurized air in response to forward movement of the engine.

Claim 20

Dependent Claim 36 words

The combination of claim 15 including a source of pressurized air mounted adjacent the inlet end portion of the casing for receiving said inflow of the pressurized air during start-up operation of the engine at standstill.

Claim 21

Dependent Claim 27 words

The combination of claim 17 wherein said source of pressurized air is a bleed valve through which atmospheric air is received within the casing at low altitudes.

Annuity Stage	Window Opens	Payment Deadline	Surcharge Period Until	Estimated Fee	Status
3.5 Years (Year 4)	1993-10-15	1994-04-16	1994-10-16	$2000.00	Window Closed / Lapsed
7.5 Years (Year 8)	1997-10-15	1998-04-16	1998-10-16	$3760.00	Window Closed / Lapsed
11.5 Years (Year 12)	2001-10-15	2002-04-16	2002-10-16	$7700.00	Window Closed / Lapsed

Pulse jet engine

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