Arrangements of or to propellers to improve the capabilities of propeller-driven craft

Claim 2

A vehicle capable of travel in air, comprising, in combination, a body with at least two wings whereof one of said wings extends laterally leftwards from said body and the other of said wings extends laterally rightwards from said body while said wings are provided with propeller holding sections which are distanced equally laterally from said body; wherein each of said holding sections is provided with a streamlined sectional configuration of said section with a longitudinal span and a relatively thereto normal chord, a fluid motor associated to said section to carry and to revolve by fluid which flows from a fluid supply source through the rotor of said motor a propeller which is fastened to said rotor wherein said motor is connected to said section by a structure, wherein said structure includes means to swing said motor upwards and downwards in normal direction relative to said span and parallel to said chord of said section wherein said structure is provided with means to keep the axes of said rotor and propeller at all times substantially parallel to said chord and, wherein fluid line portions which include rigid pipes and moveable fluid line portions are provided in said structure and between the ports of said motor and said supply source to permit the flow of fluid to and from different locations of said ports of said motor.

Claim 3

The wing of claim 1, wherein said fluid motor and said propeller are swung vertically down relative to said section in order to temporarily let said propeller work effectively in air in flight of said section and said motor and propeller are swung vertically up relative to said wing temporarily at other times when said section is close to the surface of the earth.

Claim 4

The vehicle of claim 1, wherein said structure includes pivot arms with inner and outer ends, wherein said section is provided with pivot bars to bear pivotably thereon said inner ends of said arms, wherein pivot portions are provided on said motor to bear pivotably thereon said outer ends of said arms, wherein said arms are provided parallely relatively to each other, wherein said arms have equal lengths and equal distances of the centers of said inner ends and outer ends from each other, and, wherein an actuator means is provided to pivot said arms around said pivot bars of said section, whereby said motor and said propeller are pivoted from an upper location to a lower location relatively to said section.

Claim 5

The vehicle of claim 1, wherein said section is a portion of an aircraft, wherein said actuator is a fluid cylinder with a therein reciprocating piston, wherein said cylinder is connected to said section and said piston is connected at least indirectly to at least one of said arms, wherein a control means is provided to said cylinder to actuate and control the movement of said piston and thereby the said pivotion of said motor and propeller from said upper location to said lower location and vice versa, and, wherein said pivotion is exercised under maintenance of the direction of the axes of said motor and of said propeller, whereby said axes are parallel to their different locations at other times.

Claim 6

The vehicle of claim 1, wherein said body carries a power plant which operates a proportionate delivery double flow pump with two separate outlets to pass from said outlets separately two individual drive fluid flows or equal rates of flow by individual fluid lines to the drive fluid entrance ports of said motors, wherein return fluid lines are set from the outlet ports of said motors to the entrance ports of said double flow pumps at least indirectly, wherein a second double flow pump is provided in said body and attached to a coupling means of said power plant, wherein said second double flow pump is able to supply two individual control fluid flows of equal rate of flow to individual control flow fluid lines which are communicated from separate outlets of said second double flow pump to the individual entrance ports of individual control cylinders while respective return flow fluid lines are set from the outlet ports of said cylinders to respective inlet ports of said second double flow pump, wherein said cylinders contain therein reciprocable pistons which are connected to the said structure to swing said motors up and down in unison when said second double flow pump delivers said control flows, while during the said up and down swing of said motors said control flow fluid lines and said return flow fluid lines which are connected to said second double flow pump operate vice versa, whereby said equal rates of flow in said control flow fluid lines secure equalness of operation at equal times of said swing up and swing down of said motors and said equalness of rate of flow in said drive fluid flows secures equal rotary speeds of said propellers.

Claim 7

The vehicle of claim 5, wherein said double flow pumps are four flow pumps, wherein four of said propellers and motors are provided with two thereof on said leftward extending wing and two on said rightward extending wing, while each of said motors and each of said cylinders is communicated separately to said four flow pumps to secure by said equalness of rates of flows equal rotary speeds of said four propellers and equalness of operation at equal times of said swing up and swing down of said motors.