# US 4,397,367 A · Lift and propulsion unit of air-cushion transport vehicle

> Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt

- Number: US 4,397,367 A
- Document ID: US4397367A
- Status: Granted
- Kind: A
- Application number: 06/265,584
- Filed: 1981-05-20
- Granted: 1983-08-09
- Earliest claimed: 1981-05-20
- Inventors: Sergei K. Ivanov; Viktor E. Dudkin; Iosif A. Raskin; Valery P. Peredery; Jury M. Mokhov; Vladimir K. Dyachenko; Evgenia G. Finkelshtein; Igor A. Martynov; Alexandr S. Kudryavtsev; Valery V. Protsenko; Gennady G. Filipchenko
- Web page: https://patentgrep.com/patent/US4397367A

## CPC

- B60V 1/14: Propulsion; Control thereof (B60V1/11 takes precedence)
- B60V: AIR-CUSHION VEHICLES

## Abstract

There is proposed a lift and propulsion unit for an air-cushion transport vehicle, with an axial fan installed at the entrance portion of an annular duct and at the exit of said annular duct is disposed a thrust nozzle comprising a reversing-and-steering device with independently rotatable rudder blades and reversing vanes installed in the walls of said thrust nozzle after said axial fan; said rudder blades close the exit section of said thrust nozzle during reversal of the thrust and make with each other an obtuse angle whose apex is directed toward said axial fan, and the side walls of said reversing-and-steering device are made in the form of a polyhedral vaned surface each facet of which is comprised by a cascade of bow-shaped reversing vanes. The invention may be used in the development of air-cushion transport vehicles, self-propelled transport platforms and apparatus in which the translatory motion is effected due to a reactive thrust provided by the ejected air stream.

## Claims

### Claim 1

A lift and propulsion unit of an air-cushion transport vehicle, comprising: an annular duct; an axial fan, for conveying air through said annular duct, arranged at the entrance portion of said annular duct; a thrust nozzle arranged at the exit of said annular duct; said thrust nozzle having a reversing-and-steering device having side walls, which comprises; a plurality of independently rotatable rudder blades, and reversing vanes installed in the side walls of said reversing-and-steering device after said axial fan, said rudder blades closing the exit section of said thrust nozzle during reversal of the thrust by making with each other an obtuse angle whose apex is directed toward said axial fan to divert air to said reversing vanes, said side walls of said reversing-and-steering device comprising a polyhedral vaned surface, each facet of said polyhedral vaned surface comprising a cascade of bow-shaped reversing vanes.

### Claim 2 (depends on 1)

A lift and propulsion unit of an air-cushion transport vehicle according to claim 1, in which leading edges of said bow-shaped reversing vanes are directed toward said rudder blades and kept perpendicular to the longitudinal axis of said thrust nozzle, and trailing edges thereof are inclined at an acute angle to said side walls of said thrust nozzle and directed toward the entrance portion of said annular duct.

### Claim 3 (depends on 1)

A lift and propulsion unit of an air-cushion transport vehicle according to claim 1, in which said rudder blades comprise two streamlined airfoils.

### Claim 4 (depends on 2)

A lift and propulsion unit of an air-cushion transport vehicle according to claim 2, in which said rudder blades comprise two streamlined airfoils.

### Claim 5 (depends on 1)

A lift and propulsion unit of an air-cushion transport vehicle according to claim 1, in which said rudder blades comprise more than two streamlined airfoils making up, in the closed position, guiding surfaces which close the exit section of said thrust nozzle.

### Claim 6 (depends on 2)

A lift and propulsion unit of an air-cushion transport vehicle according to claim 2, in which said rudder blades comprise more than two streamlined airfoils making up, in the closed position, guiding surfaces which close the exit section of said thrust nozzle.