Boeing Ace Collateral Agent, LLC
Held is read from USPTO's recorded assignments; a transfer never recorded there does not appear.
6
Ending by 2030
Apr 2028
Next term end
When these terms end
Held patents by the year their term ends
20262027202820292030203120322033203420352036203720382039204020412042204320442045
Fee deadlines
Maintenance fees fall due 3.5, 7.5 and 11.5 years after grant. A missed fee ends a patent at the end of the six month grace period that follows, not on the due date.
- 1 fee due Nov 21, 2026The maintenance fee for Generating inviscid and viscous fluid-flow simulations over an aircraft surface using a fluid-flow mesh (US 10,296,672) comes due Nov 21, 2026. Unpaid by May 21, 2027, it lapses early.
- 2 fees due Jul 12 to 16, 2027 · next Jul 12
- 1 fee due Oct 28, 2027The maintenance fee for Predicting transition from laminar to turbulent flow over a surface using mode-shape parameters (US 10,634,581) comes due Oct 28, 2027. Unpaid by Apr 28, 2028, it lapses early.
- 1 fee due Nov 7, 2027The maintenance fee for System and method to actively morph an aircraft while in flight for sonic boom suppression and drag minimization (US 11,975,814) comes due Nov 7, 2027. Unpaid by May 8, 2028, it lapses early.
Recent changes
- 1 of the patents on this record was granted since Aug 16, 2026
Patents held now
Soonest term end first. Each date below is computed on that patent's own page, which shows the rule, the adjustments and the fee history it was derived from.
| Patent | Title | Status | Expires | Confidence |
|---|---|---|---|---|
| US 7,837,142 | Supersonic aircraft jet engine In force (reinstated) · From the USPTO record | In force (reinstated) | From the USPTO record | |
| US 9,233,755 | Highly efficient supersonic laminar flow wing structure In force (reinstated) · From the USPTO record | In force (reinstated) | From the USPTO record | |
| US 7,946,535 | Highly efficient supersonic laminar flow wing In force · From the USPTO record | In force | From the USPTO record | |
| US 8,991,768 | Highly Efficient Transonic Laminar Flow Wing In force · Medium confidence | In force | Medium confidence | |
| US 7,967,241 | Supersonic aircraft jet engine installation In force · From the USPTO record | In force | From the USPTO record | |
| US 8,935,140 | Generating Inviscid and Viscous Fluid-Flow Simulations Over a Surface Using a Fluid-Flow Mesh In force · Low confidence | In force | Low confidence | |
| US 8,371,124 | Jet nozzle plug with varying, non-circular cross sections In force · From the USPTO record | In force | From the USPTO record | |
| US 9,348,956 | Generating a simulated fluid flow over a surface using anisotropic diffusion In force · From the USPTO record | In force | From the USPTO record | |
| US 8,882,028 | Aircraft emergency and backup secondary power apparatus In force (reinstated) · From the USPTO record | In force (reinstated) | From the USPTO record | |
| US 8,538,738 | Predicting transition from laminar to turbulent flow over a surface In force · From the USPTO record | In force | From the USPTO record |
Also on record, not counted in the 29: 7 lapsed for an unpaid fee · 2 ended at full term. List them
Sources and methods
Compiled from the USPTO record, grants, published applications and recorded assignments, not yet reviewed by hand.
How this record was built
Computed patent terms end on the dates shown. Related patents and pending applications may cover overlapping subject matter.