IP Library Patent Application 18892157
Patent Application
App. No. 18/892,157

Methods and Apparatuses Related to Payload Launch Vehicles

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Quick Facts
Patent No.
US None
App. No.
18/892,157
Abstract

Systems and methods for additive layer manufacturing of metallic components, such as rocket engines and propellant supply systems, are provided. Methods include melting the surface of a work piece to form a weld pool; adding wire to the weld pool and moving a heat source relative to the work piece to progressively form a new layer of metallic material on the work piece; cooling the formed layer; stress relieving (e.g., peening) the cooled layer; applying a secondary operations either sequentially or simultaneously; and repeating the above steps as required to form components layer by layer. Systems and methods of supplying a first propellant to the rocket engine of a launch vehicle are also provided, where the first propellant is supplied through a heat exchanger for generating mechanical energy to pump the first propellant into the rocket engine, and electrical energy to pump a second propellant into the rocket engine.

Claims (32)

1 . An apparatus, comprising:

an applicator configured to deposit a feed wire comprising a metallic deposition material onto a melted portion of a workpiece to form a layer of metallic deposition material on the workpiece;

an inductive heater configured to heat the feed wire prior to deposition of the feed wire onto the melted portion of the workpiece;

a wire feed system configured to feed the feed wire to the inductive heater and the applicator, and

at least one power supply configured to supply power to the inductive heater.

2 . The apparatus of claim 1 , further comprising an optic device configured to focus an energy beam onto a layer of the workpiece such that an amount of heat from the energy beam is sufficient to form the melted portion of the workpiece.

3 . The apparatus of claim 1 , further comprising a cooling apparatus configured to cool the layer of metallic deposition material on the workpiece to solidify the layer of deposition material.

4 . The apparatus of claim 3 , further comprising a stress-relieving apparatus configured to apply a stress-relieving process on the cooled layer of metallic deposition material on the workpiece.

5 . The apparatus of claim 1 , further comprising a wire straightening apparatus that includes the inductive heater.

6 . The apparatus of claim 2 , wherein the inductive heater raises a temperature of the feed wire sufficiently to allow energy beam coupling.

7 . The apparatus of claim 1 , wherein the inductive heater raises a temperature of the feed wire thereby reducing conduction from the melted portion into the feed wire.

8 . The apparatus of claim 1 , wherein the metallic deposition material comprises at least one alloy selected from the group consisting of: an aluminum (Al) alloy, an aluminum scandium (Al—Sc) alloy, an aluminum titanium boron (Al—Ti—B) alloy, an aluminum titanium carbon (Al—Ti—C) alloy, and an aluminum niobium boron (Al—Nb—B) alloy.

9 . The apparatus of claim 1 , further comprising a monitor and controller configured to monitor and control at least one of: a wire temperature, a workpiece temperature, a temperature surrounding the workpiece, a module location with reference to the workpiece, and a real time location and temperature of a surface of the workpiece.

10 . The apparatus of claim 1 , further comprising a trowel device, wherein the trowel device is configured to provide a force on the melted portion of the workpiece via magnetic induction.

11 . A method, comprising:

inductively heating a feed wire comprising a metallic deposition material; and

depositing the feed wire onto a portion of a workpiece to form a layer of metallic deposition material on the workpiece.

12 . The method of claim 11 , further comprising cooling the layer of metallic deposition material on the workpiece.

13 . The method of claim 12 , further comprising stress-relieving the cooled layer of metallic deposition material on the workpiece.

14 . The method of claim 11 , further comprising straightening the feed wire.

15 . The method of claim 11 , further comprising heating a layer of the workpiece via an optic device to melt the portion of the workpiece.

16 . The method of claim 15 , further comprising automatically controlling an amount of heat to the layer of the workpiece using a closed loop control system.

17 . The method of claim 15 , wherein the optic device comprises a laser beam or an electron beam.

18 . A method, comprising:

depositing a plurality of layers of a metallic deposition material to form a metal body, wherein depositing a layer of the plurality of layers comprises:

inductively heating a feed wire of the metallic deposition material;

directing the feed wire of the metallic deposition material onto a portion of the metal body while moving the feed wire and the metallic workpiece relative to each other thereby depositing the metallic deposition material to form a deposited layer of the metallic deposition material;

cooling the deposited layer to solidify the deposited layer;

monitoring the melt pool throughout the deposition to provide a real-time measurement of at least one of melt pool intensity, size, and location relative to the metallic workpiece; and

controlling the applying, directing and cooling based on the real-time measurement in a closed feedback loop.

19 . The method of claim 18 , wherein at least one deposition parameter is selected from the group consisting of: layer orientation, deposition direction, melt pool width, melt pool thickness, grain solidification, heat input, and alloy gradient.

20 . The method of claim 19 , further comprising applying an amount of heat to a portion of one or more underlying layers of the metal body sufficient to melt the portion of one or more underlying layers thereby forming a melt pool.

Assignments (4)
RELEASE OF SECURITY INTEREST Recorded Jun 12, 2025
From: SPACE LENDER, LLC
To: RELATIVITY SPACE, INC.
Reel/Frame 071574/0331 →
SECURITY INTEREST Recorded Mar 21, 2025
From: RELATIVITY SPACE, INC.
To: SPACE LENDER, LLC
Reel/Frame 070586/0861 →
SECURITY INTEREST Recorded Nov 19, 2024
From: RELATIVITY SPACE, INC.
To: SPACE LENDER, LLC
Reel/Frame 069391/0664 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 24, 2024
From: NOONE, JORDAN; ELLIS, TIMOTHY A.; RISING, JOHN
To: RELATIVITY SPACE, INC.
Reel/Frame 068684/0248 →